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Agenda 05/22/2018 Item #11B
05/22/2018 EXECUTIVE SUMMARY Recommendation to authorize Single-Source Waivers for Airbus and Metro Aviation for a one-time purchase of an Airbus helicopter equipped with medical interior for the EMS program to replace the current 1999 Airbus EC 135T1 helicopter and to negotiate a contract for final pricing, subject to Board approval. OBJECTIVE: To enable the Med Flight helicopter program to accomplish all assigned missions with quick and efficient transport of patients to definitive specialty care, to provide additional work space in the cabin in the patient compartment, and to meet current recommended safety standards. CONSIDERATIONS: The Collier County MedFlight program was started in 1975 and currently uses a 1999 Eurocopter EC135T1 twin-engine turbine helicopter to provide airborne EMS services, covering 2,000 square miles, stretching Interstate 75 from Naples to Ft. Lauderdale and Highway 41 to Miami. This service is nationally accredited and is integrated with the ground-based ambulance EMS service and both are operated by the Collier County Emergency Medical Services. This year, the Collier County Med Flight helicopter is projected to carry approximately 300 residents and visitors from the site of their accident or medical emergency to the nearest trauma receiving facilities, which are in Lee and Dade counties. Collier County does not have a trauma receiving facility and the availability of air ambulance transport is critical for improved patient outcome following injury. The number of patients transporte d by EMS is growing by 15 to 20 per year and the population is projected to grow by 1.75% per year. The current helicopter has served the county and its residents and visitors well; but it has many significant shortfalls that impact the quality of service provided to the county’s residents and visitors. With increased years in service, the following additional factors negatively affect the in -service time and general availability of MedFlight: As the aircraft ages, an increase in unscheduled maintenance in addition to the scheduled inspections, represents an increase in maintenance down time. The current helicopter is almost 20 years old. Available data suggests that helicopters over 20 years old start experiencing more unscheduled maintenance and thus less availability. This increase in down time has been observed for MedFlight over the last several years. The availability of spare parts also plays a greater role in the aircraft availability equation. At some point, the fleet, due to aircraft replacements, will be too small to warrant extensive support. This will result in lack of suppliers for critical components. Collier County’s EC 135 represents a first-generation aircraft model, and the industry is currently in the third-generation aircraft produced by Eurocopter. The current helicopter does not have an autopilot and is equipped for VFR (Visual Flight Rules) flight only. This is inadequate for dealing with inadvertent entry into IMC (Instrument Meteorological Conditions) weather. In addition, the National Transportation Safety Board recognizes an autopilot feature as a major factor in relieving pilot workload in high stress flight environments. For the last 25 years, Collier County MedFlight has operated aircraft manufactured by Airbus Helicopters and medical interiors manufactured by Metro Aviation. Prior to the current EC-135, Collier County operated an A-Star, which is also an Airbus product. This 25-year relationship would be difficult to replace or match; from aircraft part supply and maintenance to pilot training. Maintaining the same aircraft and manufacturer will reduce the cost of technician and pilot training. The pilots and maintenance technicians are currently trained in Airbus/Turbomeca engines and minimal training would be required for the upgraded avionics and auto-pilot systems. Collier County is also in possession of approximately 11.B Packet Pg. 453 05/22/2018 $1,000,000 in parts and approximately $350,000 in tools, which can only be utilized on an Airbus. Additionally, Airbus offers an enclosed Fenestron tail rotor for enhanced safety of patient and crew when loading/unloading the aircraft with rotors turning. Airbus accounts for around 25 percent of the global helicopter EMS fleet, with over 600 units in service, making it the worldwide leader in helicopter EMS. On January 29, 2018, the Procurement Services Division released notices of Request for Information No. 18-7291 to 1,779 vendors for Collier County Medflight Aircraft. Thirty-six (36) solicitation packages were downloaded, and the County received three (3) replies from Apollo Medflight, Bell Helicopter, and Airbus by February 19, 2018. Staff concluded after its review that Apollo Medflight and Bell Helicopter could not offer the safety features of the enclosed Fenestron, manufactured by Airbus. Apollo Medflight proposed an outsourced service model that would maintain current service levels; however, the earliest availability offered was between six and twelve months. This would cause a detrimental gap in service as there would be no way to offer life-saving med flights to patients. Apollo’s proposal produced an undesirable service cost because it included use of their pilots and mechanics as opposed to our current in-house service model. Bell Helicopter proposed the Bell 429 helicopter, which is used in the EMS industry; however, that model aircraft does not offer the enclosed Fenestron as a safety feature. The Procurement Director reviewed and approved staff’s request to waive formal competition and approve single source waivers for the purchase of a helicopter and medical interior from Airbus Helicopters and Metro Aviation based on the attached Waiver Request Forms and the facts provided in this Executive Summary, which demonstrate that it is in the best interest of the County to invoke the single source procurement method provided in Section Eleven of the Collier County Procurement Ordinance. Approval of the helicopter purchase will be presented to the Board in a two-step process. This Executive Summary represents the first step, by approving the single source waivers, and authorizes staff to begin contract negotiation with Airbus. Staff has obtained the services of Aviation Consultants Conklin & de Decker to assist in negotiating with Airbus and evaluating the most cost effective solution for the County. Once negotiated, the contract will be brought to the Board for final approval. FISCAL IMPACT: Once a contract is negotiated, staff will bring the contract to the Board for approval. Airbus will require a down payment, which will be negotiated, and the final amount will be due upon delivery and acceptance of the aircraft. The estimated cost for the helicopter and medical interior is between $7,500,000 and $10,000,000 (Fund 491) depending upon the model. After setting aside the first $2 million in FY 2015, a total of $7,250,000 is currently available to acquire the new helicopter. Any additional General Fund dollars required for this acquisition will be determined upon the final negotiated price. When the order is placed and the down payment made, it is estimated to take 9 months for the completion of the helicopter. Projected life of this asset is 15 to 20 years. It is also anticipated that the County will keep in service both the new and old helicopters for a period of time probably no more that 6-8 months and after that time the old helicopter will be sold and the proceeds will be used for future EMS capital equipment. GROWTH MANAGEMENT IMPACT: There are no Growth Management Impacts associated with this action. LEGAL CONSIDERATIONS: This item is approved as to form and legality, and requires majority vote for Board approval. -SRT 11.B Packet Pg. 454 05/22/2018 RECOMMENDATION: To waive formal competition and approve single source waivers for the purchase of a helicopter and medical interior from Airbus Helicopters and Metro Aviation and to authorize staff to negotiate a tentative purchase contract to be presented at a later Board meeting for review and final approval. Prepared by: Tabatha Butcher, Chief, Emergency Medical Services ATTACHMENT(S) 1. Bell RFI_Response (PDF) 2. [Linked] CC18_PD_Airbus-Helicopters-Solicitation-18-7291-Response (PDF) 3. Apollo_MedFlight_Response_to_Collier_County_RFI (PDF) 4. Metro Aviation Waiver (PDF) 5. Waiver Request 265 - Airbus (PDF) 11.B Packet Pg. 455 05/22/2018 COLLIER COUNTY Board of County Commissioners Item Number: 11.B Doc ID: 5588 Item Summary: Recommendation to authorize Single-Source Waivers for Airbus and Metro Aviation for a one-time purchase of an Airbus helicopter equipped with medical interior for the EMS program to replace the current 1999 Airbus EC 135T1 helicopter and to negotiate a contract for final pricing, subject to Board approval. (Tabatha Butcher, EMS Chief) Meeting Date: 05/22/2018 Prepared by: Title: Division Director - EMS Operations – Emergency Medical Services Name: Tabatha Butcher 05/09/2018 12:10 PM Submitted by: Title: Division Director - EMS Operations – Emergency Medical Services Name: Tabatha Butcher 05/09/2018 12:10 PM Approved By: Review: Administrative Services Department Paula Brethauer Level 1 Division Reviewer Completed 05/09/2018 4:10 PM Procurement Services Opal Vann Level 1 Purchasing Gatekeeper Completed 05/09/2018 4:49 PM Procurement Services Ted Coyman Additional Reviewer Completed 05/09/2018 5:17 PM Procurement Services Sara Schneeberger Additional Reviewer Completed 05/10/2018 1:17 PM Procurement Services Catherine Bigelow Additional Reviewer Completed 05/10/2018 3:39 PM Administrative Services Department Len Price Level 2 Division Administrator Review Completed 05/11/2018 1:25 PM County Attorney's Office Scott Teach Level 2 Attorney Review Completed 05/11/2018 4:31 PM Office of Management and Budget Valerie Fleming Level 3 OMB Gatekeeper Review Completed 05/14/2018 8:10 AM County Attorney's Office Jeffrey A. Klatzkow Level 3 County Attorney's Office Review Completed 05/14/2018 8:17 AM Office of Management and Budget Susan Usher Additional Reviewer Completed 05/14/2018 12:10 PM County Manager's Office Nick Casalanguida Level 4 County Manager Review Completed 05/16/2018 1:51 PM Board of County Commissioners MaryJo Brock Meeting Pending 05/22/2018 9:00 AM 11.B Packet Pg. 456 Post Office Box 482 ▪ Fort Worth, Texas 76101 ▪ Telephone: (817) 280-1290 ▪ Fax: (817) 278-1290 19 February 2018 X7:VR-002-0285 Collier County Board of County Commissioners Procurement Services Division 3295 Tamiami Trail East, Naples, Florida 34112 Attention: Swainson Hall, Procurement Manager - Acquisitions Subject: Bell Helicopter Textron Inc. Response to Request for Information #18-7291 for Collier County Med Flight Aircraft Reference: Request for Information #18-7291 Collier County Med Flight Aircraft Enclosure (1): Bell Helicopter Textron Inc. Executive Summary Dear Ms. Hall: Please find attached our solution for a Light Twin Med Flight helicopter. We would welcome the opportunity to speak directly with your flight department to develop a customized platform. Please contact our Regional Sale Manager, Bill Hein, at 850-797-5843. Sincerely, Veronica Rojas Manager of Contracts Commercial Business Operations Bell Helicopter Textron Inc. 11.B.1 Packet Pg. 457 Attachment: Bell RFI_Response (5588 : Single Source Approval for EMS Helicopter Purchase) Collier County Med Flight Aircraft 1.0 – EXECUTIVE SUMMARY Submittal Date: February 2018 Use of data contained on this sheet is subject to the restriction on page i of this document. 1-1 1.0 EXECUTIVE SUMMARY Emergency Medical Services (EMS) organizations have many factors critical to the success of their missions. Safety, speed, ride quality with low vibration, cabin size and patient access are paramount as lives, literally, are at stake. Bell Helicopter is pleased to offer Collier County the Bell 429 as the complete EMS solution. 1.1 The Bell Helicopter Advantage The Bell 429 is a light twin-engine, Single Pilot IFR (SPIFR) and Dual Pilot IFR (DPIFR) aircraft built to the latest Federal Aviation Regulations (FAR)/Joint Aviation Requirements (JAR) Part 27 safety amendments. It offers the latest in technology to provide one of the best combinations of speed, payload, range and cabin size, coupled with the latest in safety improvements for redundancy, crashworthiness and a rotary manufacturer that offers avionics with integrated performance calculations for fingertip access to critical flight parameters. With more than 80 years of aviation experience and expertise in providing one of the safest and most reliable helicopters in the industry, Bell Helicopter’s firm commitment to customer satisfaction and continuing product improvements is represented in the Bell 429. Customer support representatives are available 24 hours a day, 7 days a week, 365 days a year. The Bell 429 Figure 1-1, can play the vital role in ensuring the gap between patient and advanced medical care covers the shortest possible time. The Bell 429 provides a number of features that translate to better medical care during patient transports: • Cabin Volume - Featuring one of the largest cabin in its class, the Bell 429 with an open design and flat floor easily fits two litters, two attendants, and required specialty equipment. The aircraft offers ample room for hospital transport teams to have full body access needed in critical care. The deck height matches litter height and allows one-man litter loading with less lifting or back strain through either side or optional aft clamshell doors. The Bell 429 is the total package solution for EMS operators. Certified to the latest Airworthiness Requirements (Category A), SPIFR on all profiles for increased occupant safety Largest Cabin in Class allowing for two patient litters and two crew members Backed by the #1 ranked Customer Support for the 23rd year in a row Figure 1-1. Bell 429 EMS. The Bell 429 offers customers a superior aircraft highly specialized to perform EMS operations. 11.B.1 Packet Pg. 458 Attachment: Bell RFI_Response (5588 : Single Source Approval for EMS Helicopter Purchase) Collier County Med Flight Aircraft 1.0 – EXECUTIVE SUMMARY Submittal Date: February 2018 Use of data contained on this sheet is subject to the restriction on page i of this document. 1-2 • Loading Flexibility - Equipped with 62-inch side entrances, and rear loading capability, the Bell 429 design simplifies the most difficult loading challenges (Figure 1-2). Note: Graphics represent door opening only – not vendor specific equipment. Figure 1-2. EMS Loading & Comfort. The Bell 429 is one of the largest cabin in its class and flexible loading options provide the highest level of comfort for crew and passengers. • 150 Knot Maximum Cruise Speed - The Bell 429 moves patients quicker than competing aircraft. The Vh cruise speed of 150 knots or maximum sustainable cruise is 13 knots is faster than its closest competitor in its class at 137 knots in the EMS field, those 13 knots are critical during “the golden hour”. • High Output Air -Conditioning - Enhances patient comfort, and minimizes thermal stress. • Smooth/Stable/Low Vibration Ride - Reduces the difficulty of pulse detection, in transit, and patient airsickness is minimized by Bell 429’s advanced longitudinal and pitch stability. An added benefit is improved medical equipment health due to reduced vibration exposure. 11.B.1 Packet Pg. 459 Attachment: Bell RFI_Response (5588 : Single Source Approval for EMS Helicopter Purchase) Collier County Med Flight Aircraft 1.0 – EXECUTIVE SUMMARY Submittal Date: February 2018 Use of data contained on this sheet is subject to the restriction on page i of this document. 1-3 • Excellent High/Hot Performance - The Bell 429 demonstrates outstanding high/hot performance including Category A Single Engine performance, providing Bell 429 operators greater lift capabilities across the spectrum of hot temperatures and higher altitudes. 1.2 Crew and Patient Safety The Bell 429 (Figure 1-3) incorporates redundant systems in the avionics, hydraulics and power- plant systems providing increased safety and is compliant and certified to the latest standards for crashworthiness (FAR 27 Amendment 44, dated 2008) and meets all applicable crash protection requirements specified in the ADF’s Airworthiness Design Requirements Manual. In addition, the Bell 429 is configured with a BasiX-Pro Integrated Avionics and Flight Control System which has been specifically designed to meet the requirements of twin engine helicopters and is optimized for IFR, Category A (CAT A), and EU-OPS compliant operations. BELL 429 SAFETY FEATURES (AIRFRAME) Wire Strike Protection Dual Hydraulics Excellent Main Rotor Clearance FADEC with Engine Exceedance Monitoring Crash Attenuating Seats Large Doors for Better Egress 30-Minute Dry Run Transmission Damage Tolerant Rotor Blades Fire Extinguisher Rupture Resistant Fuel Tanks Roll-over Bulkheads Certified for Ditching BELL 429 SAFETY FEATURES (COCKPIT) Single Pilot IFR Certified Superior CAT A Performance Performance and Automatic CG Calculator Terrain Avoidance Warning Systems (TAWS) Real-time Satellite Weather in the Cockpit (Optional) 3rd Axis Autopilot (standard). 4th Axis Autopilot( kit) Figure 1-3. Safety is Designed into the Aircraft. The Bell 429 includes numerous safety features to provide the highest level of safety for our customers. 1.3 Maintenance Efficiency The Bell 429 is engineered for reliability and ease of maintenance, as such it is the first helicopter certified through the Maintenance Steering Group-3 (MSG-3). MSG-3 is a process for enhanced maintenance efficiency and safety and requires 35% less maintenance man-hours per flying versus a comparable aircraft. Primary components and systems are designed for routine servicing while installed on the aircraft. Major service intervals are among the longest in the rotorcraft industry due to Bell Helicopter’s traditionally long Time Between Overhaul/Retirement Life components. Steps and work platforms, along with plentiful access panels, doors and inspection windows provide for quick and thorough preflight checks and servicing. Bell Helicopter is 11.B.1 Packet Pg. 460 Attachment: Bell RFI_Response (5588 : Single Source Approval for EMS Helicopter Purchase) Collier County Med Flight Aircraft 1.0 – EXECUTIVE SUMMARY Submittal Date: February 2018 Use of data contained on this sheet is subject to the restriction on page i of this document. 1-4 committed to safety, low cost of operations and reliable, responsive helicopters that are supportable and economic through their lifetime. 1.4 Bell Helicopter Product Support With a keen focus on customer satisfaction and impeccable service, Bell Helicopter has surpassed its competitors. For this reason, Bell Helicopter has been named as the Best Customer Support and Service provider by Pro Pilot magazine for 23 years in a row. Bell Helicopter’s extensive and responsive support organization supports every aircraft model ever built by Bell Helicopter. Bell Helicopter’s unmatched worldwide spares and warranty support plays a huge role in achieving excellence in customer service. Bell Helicopter’s factory supported Repair and Overhaul capabilities, combined with its globally dispersed Customer Service Facilities are the perfect ingredients to respond promptly to customer issues. 1.5 Bell 429 Training In addition to designing and certifying the most recent air medical helicopter, Bell Helicopter is also recognized around the world as the premier helicopter training organization. The Bell Training Academy (BTA) has trained over 200,000 pilots and maintenance personnel, and has invested significantly in the infrastructure required to conduct initial and recurrent pilot or mechanic training. 1.6 Bell 429 Summary The Bell 429 EMS solution (Figure 1-5), certified to the most demanding airworthiness standards in existence, provides one of the best combinations of performance, mission readiness, comfort, safety, customer support and training for Collier County. Figure 1-4. Customer Support You Can Count On. Bell Helicopter’s #1 rated Customer Support ensures EMS operators spend their time in the air and not on the ground. 11.B.1 Packet Pg. 461 Attachment: Bell RFI_Response (5588 : Single Source Approval for EMS Helicopter Purchase) Collier County Med Flight Aircraft 1.0 – EXECUTIVE SUMMARY Submittal Date: February 2018 Use of data contained on this sheet is subject to the restriction on page i of this document. 1-5 Figure 1-5. The Light Twin Choice for EMS Operations. The high performance Bell 429, filled with the latest technology, and backed by #1 ranked customer support is the optimal aircraft for EMS operators. 11.B.1 Packet Pg. 462 Attachment: Bell RFI_Response (5588 : Single Source Approval for EMS Helicopter Purchase) Collier County Med Flight Aircraft 1.0 – EXECUTIVE SUMMARY Submittal Date: February 2018 Use of data contained on this sheet is subject to the restriction on page i of this document. 1-6 1.7 Bell 429 Best In-Class Performance Bell 429 H135T Max Gross Weight 7,000 lbs 6,504 lbs HIGE Altitude Performance (Maximum GW, ISA) 14,130 ft 6,000 ft HOGE Altitude Performance (Maximum GW, ISA) 11,290 ft 5,600 ft Altitude Performance (Service Ceiling) 18,710 ft 8,000 ft Useful Load (Internal, Std. Config.) 2,072 lbs. 1,912 lbs. Demonstrated Functional Speed 155+ knots 150 knots Maximum Cruise Speed (MGW, Sea Level, ISA) 150 knots 137 knots 11.B.1 Packet Pg. 463 Attachment: Bell RFI_Response (5588 : Single Source Approval for EMS Helicopter Purchase) Apollo MedFlight, LLC 5600 Bell St. Amarillo, TX 79109 USA 806-322-4448 www.apollomedflight.com February 19, 2018 Swainson Hall Procurement Manager – Acquisitions Collier County Board of County Commissioners 3295 Tamiami Trail East Naples, FL 34112 Dear Mr. Hall: On behalf of Apollo MedFlight, I am pleased to present the Collier County Board of Commissioners with our response to the Collier County Medflight Aircraft Request for Information (RFI). We request an opportunity to participate in any future Request for Proposals. Apollo Medflight Apollo MedFlight is a privately-held corporation headquartered in Amarillo, Texas with aviation operations in Texas, Oklahoma and North Carolina. Our organization is led by recognized air medical industry veterans who utilize best practices in our operations. We are financially sound, CAMTS accredited, have a strong safety culture, and have a focus on customer service. Apollo was founded in 2011 by three partners with a strong track record of establishing service-oriented businesses focused on performance, strong partnerships, strategic growth and prioritizing consumers and business in rural communities. Apollo is a provider of rotor-wing, fixed-wing and ground medical transport services in the Texas, Oklahoma, New Mexico and North Carolina markets. Apollo’s flexibility to create service models tailored to the specific needs of its healthcare provider and community constituents, combined with the delivery of superior service, has enabled the company to rapidly gain market share from the large industry competitors and form strong relationships with healthcare providers and community leaders within its markets. Apollo operates its own part 135 certificate under the name of Integra Aviation with King Air fixed-wing aircraft and EC 135 rotor-wing aircraft. Apollo is adding additional EC 135 and EC 145 bases in May 2018. Apollo Leadership Apollo’s people are its most valuable resource. The following personnel are experienced industry leaders in rotor- wing and fixed-wing air medical transport operations: Lehmer Dunn, CEO, is a licensed pilot with 22 years of experience in leading the growth of entrepreneurial service organizations. In 1999, he co-founded and served as CEO of AMA Communications, going from a start- up to $8M in EBITDA while also acquiring seven similar businesses. He also was an owner and senior leader at Attebury Grain with annual revenues of $400M. His success has resulted from his enthusiasm for customer service. 11.B.3 Packet Pg. 464 Attachment: Apollo_MedFlight_Response_to_Collier_County_RFI (5588 : Single Source Approval for EMS Helicopter Purchase) 2 Jonathan Collier, Chief Strategy Officer, has 17 years of senior and executive leadership roles in the air medical industry with Air Methods, PHI, Summit Air Ambulance and Rocky Mountain Helicopters. He is a former board member for the Association of Air Medical Services (AAMS). He worked directly with Dennis Cochran and other Mercy leadership to build a strong partnership and develop an ADM program focused on safety, customer service and high quality patient care. He is passionate about bringing back a focus on customer service to the air medical industry. Tom Klassen, Director of Operations, has 35 years of aviation experience and leadership. When Mr. Dunn desired to bring on an experienced Director of Operations, he called the FAA for recommendations; the FAA strongly recommended Mr. Klassen as an ideal candidate and his skills along with the FAA relationship have been instrumental in Apollo’s ongoing success. He is the Past President of the Texas Association of Air Medical Services, Chairman for the Director of Operations section of AAMS, and is a Board Member of the Air Medical Operator’s Association. Michael Benton, Director of Safety and Quality, has 21 years in aviation operations and safety. He was instrumental in his previous role at Air Methods in managing FAA compliance, safety and in developing the Operational Control Center. As an independent consultant, he worked with organizations to to improve communication, safety and general operations. Most recently, he has been a leader in the Line Operations Safety Audit (LOSA) initiative and has managed projects worldwide for PHI, Air Methods, Metro Aviation, CHC Helicopters, Babcock, and the US Air Force (along with many others). He has increased the expertise at Apollo and is implementing Flight Operational Quality Assurance (FOQA) and engaging Apollo in the FAA Safety Management System Voluntary Program. Howard Ragsdale, SVP of Strategic Alliances, has had a major impact on the air medical and aviation industries in his 40+ year career. Former roles include Senior Vice President of Business Development at Air Methods, Director of the PHI Air Medical Division and VP of Operations at Omniflight. He has also served as President of the Air Medical Operators Association (AMOA), on the board of The Commission on Accreditation of Medical Transport Services (CAMTS) and multiple industry committees. Travis Lamance, Director of Maintenance, has 20 years A&P/IA technician experience in addition to being a licensed pilot. He is the previous owner and operator of a part 145 repair station (FAA approved repair facility); he has a strong relationship with the FAA and is known for his hands-on approach to working with his team and ensuring compliance on each of the aircraft under his responsibility. Financial Strength and Partners Since its inception, Apollo has shown continued growth in revenue and financial performance. The organization has a strong financial foundation and is performing with its current cash flows. Apollo has ready access to capital 11.B.3 Packet Pg. 465 Attachment: Apollo_MedFlight_Response_to_Collier_County_RFI (5588 : Single Source Approval for EMS Helicopter Purchase) 3 to provide needed cash, equipment and aircraft for growth. Apollo abides by GAAP for producing financial statements and has audited financials prepared by an independent third party accounting firm. Safety Focus Safety is a cultural imperative throughout the Apollo organization from the CEO to the flight personnel. Michael Benton, Director of Safety and Quality, and the aviation leadership team have implemented FAA recommended safety best practices including a defined safety management system. The safety management system is an integrated program that drives decision making, operations and all other aspects of the company’s business and how those elements correlate to one another. Apollo meets all FAA and Helicopter Emergency Medical Services (HEMS) operational and safety requirements. Contact—I will serve as the primary contact for all RFI or RFP related communications, including any requests for clarification or other communication. Thank you for your consideration of our organization as a potential partner for Collier County Medflight. Regards, Jonathan Collier Chief Strategy Officer Apollo MedFlight jcollier@apollomedflight.com (208) 515-6470 (cell) 5600 Bell St. Amarillo, TX 79109 11.B.3 Packet Pg. 466 Attachment: Apollo_MedFlight_Response_to_Collier_County_RFI (5588 : Single Source Approval for EMS Helicopter Purchase) 1 II. Description of Proposed Helicopter Model and Services Aircraft Model—Apollo and its leadership team have operated the majority of available twin engine and single engine air medical aircraft. Apollo currently operates multiple model H135s and will begin operations in an H145 in May. We recommend Collier County consider other aircraft models in addition to the H135 T3. There are currently no H135 T3s in operation in the United States. Apollo is able to source a T3 but the response time to availability will be more than six-twelve months upon selection as a partner to Collier County. Being the first operator of an aircraft model, especially with only one of the aircraft, is not always a desirable situation based on parts and support. The predominant variant of the H135 in operation in the United States is the Pratt & Whitney model H135 (P1, P2, P2+ and P3). Aircraft currently available include a 2016 P2e and a P3 in the short term for the right contract. If an H135 is the desired airframe for consistency of operations, Apollo proposes a used P2e, the new 2016 P2e or the new P3—Apollo will provide pricing and contract considerations for each of these models to Collier County as desired. One additional aircraft for consideration is a used H145. There are multiple used H145s available on the market, with newer used models to soon go on the market. The H145 introduces a larger, cabin-class aircraft with increased speed and other capabilities. The hourly cost of operation is reasonable and not tremendously different than the H135. With each of these models, the aircraft will be single pilot instrument flight rules (SPIFR) capable. One of the considerations for Collier County with its contract is the decision to fly SPIFR or to only have SPIFR capable aircraft for its operations. Another key focus for consideration is discussion about a spare aircraft. Apollo operates programs in which there is a dedicated spare to the program; Apollo also covers spare needs from other regions. We recommend consideration of a dedicated spare for the program to ensure complete availability. Service Model—Apollo and its leadership team have operated many service models in the air medical industry and considers the following options as viable for contract discussions with Collier County. 1. Traditional/Hospital Based Services (HBS) ◦ Apollo provides aviation services only Pilots Mechanics Aircraft (can be provided by Apollo or owned by the County) ◦ Collier County provides Clinicians Billing and collections Branding Dispatch (can be provided by Apollo or the County) ◦ Long term contract with County Apollo reimbursed on a fixed monthly and an hourly flight rate 2. Hybrid/Alternative Delivery Model (ADM) ◦ Apollo provides 11.B.3 Packet Pg. 467 Attachment: Apollo_MedFlight_Response_to_Collier_County_RFI (5588 : Single Source Approval for EMS Helicopter Purchase) 2 Aviation services Aircraft Billing and collections Reimbursement to County for medical staffing, medical direction and branding ◦ Collier County provides Clinicians Branding Medical Direction Dispatch (can also be provided by Apollo) No contractual reimbursement to Apollo for aviation services 3. Community Based Services (CBS) ◦ Apollo provides Aviation services Medical staffing Dispatch and communications Billing and collections All costs carried by Apollo Each of these models can be adapted to fit the needs of Collier County MedFlight. Apollo would be interested in operating each of these models but recommends looking at the Traditional or Hybrid models as having the greatest potential for long-term success. With each of these models, Apollo will work directly with Collier County to select and employ pilots and mechanics. Pilots—Apollo will hire and assign four pilots to the base. One of the pilots will be designated as the Lead Pilot at the base. Tom Klassen and his Chief Pilots will recruit and retain pilots based on higher than average industry pay with retention bonuses, off-duty housing, benefits and a strong safety culture. The Apollo aviation team’s leadership, relationship with the FAA, focus on training, and the use of quality equipment are additional incentives to attract candidates for the open positions. Apollo will work with Collier County to determine the best candidates for the pilot positions. Apollo leadership will seek Medflight input in regards to current program pilots and candidates to retain at the bases. All pilots will, at a minimum, (i) be licensed by the FAA (ii) satisfy Apollo’s qualifications and standards and (iii) meet or exceed the applicable standards set forth by the Commission on Accreditation of Medical Transport Systems (CAMTS) and the State of Iowa Office of Emergency Medical Services air ambulance regulations and rules. Subject to applicable FAA regulations, pilots will work rotating schedules so that one pilot is available twenty-four (24) hours a day, twelve (12) hour work shifts, 365 days per year. 11.B.3 Packet Pg. 468 Attachment: Apollo_MedFlight_Response_to_Collier_County_RFI (5588 : Single Source Approval for EMS Helicopter Purchase) 3 Apollo will ensure that qualified annual recurrent training occurs either with internal aircraft or through FlightSafety and flight simulation. Pilots will fulfill assignments within the FAA, CAMTS and Apollo rest and duty time requirements. Mechanics—Apollo will hire two mechanics for the base. By having the mechanics regionally based, they will be available to complete daily maintenance or work together to efficiently complete more significant maintenance events. Apollo will perform routine maintenance on the aircraft at off-peak hours and other times determined by Apollo and Medflight as those least likely to interfere with the readiness of the aircraft. Each mechanic will meet or exceed applicable CAMTS requirements and will have completed the factory approved airframe and engine school relative to the aircraft within one year of their hire date. Mechanic training will be performed at Flight Safety International or an approved manufacturer’s training facility. Mechanics will fulfill assignments within the FAA, CAMTS and Apollo rest and duty time requirements. III. Additional Information Apollo’s primary differentiator in the air medical industry is its ability focus completely on the success of our partner. The majority of air medical providers in the industry have been consolidated and are part of massive companies who have significant conflicts and a lack of customer service. We have built our success through safety in operations and customer service. We set up each of our operations with the ability to stand alone—we look forward to extending operations into Florida. Apollo has other value added services and strengths that may appeal to Collier County, including the following: • No contractual or relationship conflicts with hospital systems or adjacent air medical programs—Apollo has the ability to focus solely on Collier County Medflight’s success • Progressive culture focused on its safety management system (SMS) with evolving safety programs like Baldwin SMS, FDM and the FOQA initiative • A strong, positive relationship with the FAA • CAMTS accreditation and operations with industry best practices • A high functioning app for customers to request and track dispatched aircraft • Ability to establish a membership program to cover air medical transports for the communities Medflight serves 11.B.3 Packet Pg. 469 Attachment: Apollo_MedFlight_Response_to_Collier_County_RFI (5588 : Single Source Approval for EMS Helicopter Purchase) 11.B.4Packet Pg. 470Attachment: Metro Aviation Waiver (5588 : Single Source Approval for EMS Helicopter Purchase) Instructions Completed waiver requests accompanied by any associated backup documentation (sole source letter, business case, etc.) must be submitted to the division’s Procurement Strategist for any procurement, without competition, in excess of $3,000. Waiver requests greater than $50,000 will require approval by the Board of County Commissioners. Sole source refers to a procurement where the selection of one particular supplier to the exclusion of all others may be based on a lack of competition, proprietary technology, copyright, warranty or a supplier’s unique capability. Single source refers to a procurement directed to one source because of standardization, warranty, or other factors, even though other competitive sources may be available. Requester Name: Division: Item/Service:Vendor Name: Fiscal Year: Requested Date Range:Anticipated Cost per Fiscal Year: Sole Source: Single Source: One Time Purchase: Multiple Purchases: Description of Purchase:Enter a description of the item(s) items that will be purchased under this waiver. Purpose:Describe in detail, the purpose of the requested item(s) and why it is essential to County operations. Explanation: Why is this a single or sole source? Date of BCC standardization (if applicable): BCC Item number: It is a felony to knowingly circumvent a competitive process for commodities or services by fraudulently specifying sole source. Florida Statute 838.22(2). Requested by: Signature: Date: Division Director: Signature:Date: Procurement Strategist: Signature:Date: Procurement Director: Signature:Date: For Procurement Use Only: FY18 Approval: FY19 Approval: Multi-Year Approval: Start ____________ End ____________ Collier County Waiver Request Form Waiver Form Ver. 1 - 8/25/2017 Tabatha Butcher EMS Airbus Helicopter with Turbomeca Engine Airbus FY18 $7 to $10 million ✔✔ Medical Helicopter with engine (Part 1 of 2 Helicopter package) To quickly and efficiently respond to serious medical emergencies when ambulance travel is not possible or more definitive specialty care is warranted. Since the purchase of the AStar in 1992, Collier County Medflight has operated aircraft manufactured by Airbus Helicopters. This 25 year relationship would be difficult to replace or match; from aircraft part supply and aircraft maintenance and pilot training. Maintaining the same aircraft and manufacturer will reduce the cost of maintenance technician and pilot training. The pilots and maintenance technicians are currently trained in Airbus/Turbomeca engines and minimal training would be required for the upgraded avionics and auto-pilot systems. CCHO is in possession of approximately $1,000,000.00 in Airbus parts and $300,000 in Airbus tools. Airbus offers the same unique cockpit design and layout and enclosed Fenestron tail rotor for safety of patient and crew when loading/unloading the aircraft with the rotors turning. Tabatha Butcher Tabatha Butcher Digitally signed by Tabatha Butcher Date: 2017.11.21 08:47:27 -05'00' Tabatha Butcher Tabatha Butcher Digitally signed by Tabatha Butcher Date: 2017.11.21 08:47:41 -05'00' Adam Northrup cn=adamnorthrup@colliergo v.net '00'05- 08:51:32 2017.11.21 Edward F. Coyman Jr. CoymanTed Digitally signed by CoymanTed DN: dc=net, dc=colliergov, dc=bcc, ou=Divisions, ou=ASD, ou=ASD Purchasing, ou=Purchasing User Accounts, cn=CoymanTed, email=TedCoyman@colliergov.net Date: 2018.05.09 16:35:35 -04'00' ✔ 11.B.5 Packet Pg. 471 Attachment: Waiver Request 265 - Airbus (5588 : Single Source Approval for EMS Helicopter Purchase) Collier County MedFlight Aircraft RFI Solicitation 18-7291 February 14, 2018 Submitted To Submitted By Swainson Hall Airbus Helicopters, Inc. Procurement Manager - Acquisitions 2701 North Forum Drive Collier County Board of County Commissioners Grand Prairie, Texas 75052 Procurement Services Division 3295 Tamiami Trail East Naples, Florida 34112 Company Points of Contact Contracts POC Christie White-Mays Contract Administration Manager Email: christie.white@airbus.com Phone: 972-641-3455 Sales POC Jennifer Hardcastle Air Medical Sales Manager Email: jennifer.hardcastle@airbus.com Phone: 214-846-1373 Glenn Murray Regional Sales Manager Email: glenn.murray@airbus.com Phone: 817-600-1672 Airbus Helicopters, Inc. Proprietary Information Disclosure Restriction Notice This document contains proprietary information belonging to Airbus Helicopters, Inc., and its Affiliates. This information is commercially sensitive in nature, is not made available for public review, and is submitted to Collier County on a confidential basis for evaluation and planning purposes only. No other use of the information is permitted without the express written permission of Airbus Helicopters, Inc. Note: Airbus Helicopters logo, AS365N3+®, AS565MBe®, H120®, H125®, H125M®, H130®, H130M®, H135®, H135M®, H145®, H145M®, H155®, H160®, H175®, H215®, H215M®, H225®, H225M®, Helionix®, and Fenestron® are registered trademarks of Airbus Helicopters, Inc. 02/14/18 2 / 22 This document is the property of Airbus Helicopters, Inc. (AHI), and should be handled in accordance with the Disclosure Restriction Notice on the front cover of the document. This document, as well as the information and/or data it contains, shall not be disclosed without express written authorization of AHI. All rights reserved. 02/14/18 3 / 22 This document is the property of Airbus Helicopters, Inc. (AHI), and should be handled in accordance with the Disclosure Restriction Notice on the front cover of the document. This document, as well as the information and/or data it contains, shall not be disclosed without express written authorization of AHI. All rights reserved. Transmittal Letter I. Swainson Hall February 14, 2018 Procurement Manager - Acquisitions Collier County Board of County Commissioners Procurement Services Division 3295 Tamiami Trail East Naples, Florida 34112 RE: Collier County MedFlight Aircraft RFI Solicitation 18-7291 Dear Mr. Hall, Airbus Helicopters, Inc. (AHI), is a world class helicopter manufacturer and is the leading provider of commercial helicopters in North America. We appreciate the opportunity to present our proposed air medical transportation services and patient care solution to Collier County MedFlight. We believe our H135 model, as described more fully below, offers a superior solution capable of meeting and/or exceeding all mission requirements defined in Collier County’s RFI Solicitation 18-7291. Airbus Helicopters sells and supports the broadest range of civil and para-public helicopters offered by any helicopter manufacturer in the world. Over the last ten years, AHI has provided helicopter solutions for more than half of all emergency medical service (EMS) needs in the United States. Our headquarters is located in Grand Prairie, Texas, where we provide engineering, new production helicopters, completion services, maintenance, repairs, and overhaul services. Airbus Helicopters also has a manufacturing facility in Fort Erie, Ontario (Canada), which provides similar services to those provided in Grand Prairie. AHI’s production center of excellence in Columbus, Mississippi, provides the H125 for commercial customers and the UH-72A Lakota for the U.S. Army. AHI is proud to have delivered more than 400 UH-72A’s to the U.S. Army from Columbus (current contract of record is for 427), all of them on time and on budget. Our heritage in the United States dates back over 40 years. Our roots began in 1969 when Aerospatiale and LTV Aerospace formed Vought Helicopter. Airbus Helicopters, Inc., formerly American Eurocopter, was formed in 1992 when Aerospatiale Helicopter, Inc., and MBB USA merged. Today, AHI has more than 600 customers, and we support over 1900 aircraft operating throughout the nation. From our humble beginnings, we have grown to a U.S. footprint of over 860,000 square feet with more than 700 employees, and we are the market leader in five out of six helicopter segments. AHI is the U.S. affiliate of Airbus Helicopters, the largest helicopter manufacturer in the world, and a subsidiary of Airbus Group, Inc. 02/14/18 4 / 22 This document is the property of Airbus Helicopters, Inc. (AHI), and should be handled in accordance with the Disclosure Restriction Notice on the front cover of the document. This document, as well as the information and/or data it contains, shall not be disclosed without express written authorization of AHI. All rights reserved. AHI company and contact information, along with identification of the primary AHI points of contact (POC) supporting Collier County, are defined below: Christie White-Mays Contract Administration Manager Email: christie.white@airbus.com Phone: 972-641-3455 Jennifer Hardcastle Air Medical Sales Manager Email: jennifer.hardcastle@airbus.com Phone: 214-846-1373 Glenn Murray Regional Sales Manager Email: glenn.murray@airbus.com Phone: 817-600-1672 Collier County MedFlight’s helicopter EMS program operations call for a helicopter that is safe, mission-capable, operationally available, competitively priced, and cost-effective to purchase and operate. AHI is proud to offer our H135 model helicopter, AHI’s premier three ton class helicopter for North American and worldwide operations, as an exceptional solution to fulfill the key requirements of Collier County MedFlight’s EMS program. The Airbus H135 is a proven solution for critical EMS mission requirements throughout the world, and AHI is eager to support Collier County MedFlight’s fleet upgrade efforts. Our Sales, Marketing, and Support Teams at Airbus Helicopters are fully committed to providing a new H135 light twin-turbine helicopter to Collier County MedFlight that meets and exceeds your critical mission requirements. We look forward to the next steps in the acquisition process. Sincerely, Brian K. Reid Senior Director, Commercial Sales Airbus Helicopters North America Airbus Helicopters, Inc. 2701 North Forum Drive Grand Prairie, Texas 75052 02/14/18 5 / 22 This document is the property of Airbus Helicopters, Inc. (AHI), and should be handled in accordance with the Disclosure Restriction Notice on the front cover of the document. This document, as well as the information and/or data it contains, shall not be disclosed without express written authorization of AHI. All rights reserved. Table of Contents Transmittal Letter ................................................................................................................ 3 I. Proposed Helicopter ........................................................................................................... 7 II. II.A. H135 Platform Overview ........................................................................................... 7 II.A.1. Advanced Technology ................................................................................. 9 II.B. H135 in Emergency Medical Services Missions ......................................................12 II.B.1. Air Ambulance Capabilities and Configuration ............................................12 II.B.2. EMS Interior Completion .............................................................................13 II.C. H135 Performance ...................................................................................................14 II.C.1. H135 Maintenance......................................................................................15 Support and Services.........................................................................................................16 III. III.A. Customer Support....................................................................................................16 III.A.1. Technical Support .......................................................................................17 III.A.2. Spare Parts.................................................................................................17 III.B. Aircraft Support ........................................................................................................19 III.B.1. Warranty .....................................................................................................19 III.B.2. HCare .........................................................................................................19 III.C. Pilot and Technician Training ...................................................................................20 III.C.1. Pilot Training ...............................................................................................20 III.C.2. Technician Training ....................................................................................21 Project Approach ...............................................................................................................22 IV. 02/14/18 6 / 22 This document is the property of Airbus Helicopters, Inc. (AHI), and should be handled in accordance with the Disclosure Restriction Notice on the front cover of the document. This document, as well as the information and/or data it contains, shall not be disclosed without express written authorization of AHI. All rights reserved. 02/14/18 7 / 22 This document is the property of Airbus Helicopters, Inc. (AHI), and should be handled in accordance with the Disclosure Restriction Notice on the front cover of the document. This document, as well as the information and/or data it contains, shall not be disclosed without express written authorization of AHI. All rights reserved. Proposed Helicopter II. II.A. H135 Platform Overview Categorized as a light twin, the H135 is the latest progressive variant of the well-known EC135 that has maintained its reputation as the most popular aircraft for air medical providers over the last 20 years. The unrivalled, mission-fit patient care area offers over 130 cubic feet of cabin space, allowing excellent patient access for critical interventions while in flight. The large cabin area accommodates up to three (3) medical crew and two (2) patients. The rear-loading clamshell doors ensure ergonomic loading and unloading of the patient via a wheeled stretcher solution and contribute to the safe and efficient transport of the patient through all phases of the transport evolution. The H135’s high endurance and extended range enable this helicopter to perform a wide range of missions while carrying more payload over longer distances than any other aircraft in its class. The exceptional payload of the H135 is the result of modern technology fabrication in conjunction with an extensive use of composite materials. The high degree of composite structure results in a low empty weight and provides increased safety and resistance against corrosive operating environments. These attributes distinguish the H135 as the most popular twin-engine choice for U.S. air medical providers. The H135’s simple design allows fast, easy maintenance, ensuring optimal dispatch reliability and lower operating costs. The evolved maintenance plan, extended scheduled inspection intervals, and high dispatch rates make the H135 the world’s most reliable light twin helicopter. Airbus Helicopters is the Market Leader in EMS Helicopters in the U.S. 63% of all new EMS helicopters sold in the U.S. in the last 10 years have been produced by Airbus Helicopters Over 220 EMS-configured H135 helicopters are in service in the U.S. The H135 family makes up 25% of the entire worldwide fleet of EMS helicopters The H135 is the most cost-effective helicopter in the light twin-engine 3 ton class Figure 1: The latest evolution of the H135 platform offers many new innovations to improve mission performance, increase operational safety, and provide an efficient EMS system. 02/14/18 8 / 22 This document is the property of Airbus Helicopters, Inc. (AHI), and should be handled in accordance with the Disclosure Restriction Notice on the front cover of the document. This document, as well as the information and/or data it contains, shall not be disclosed without express written authorization of AHI. All rights reserved. The H135 is certified to the latest CS 27/FAR 27 crashworthiness standards, including energy- absorbing fuselage and seats and rupture-resistant fuel cells. The H135’s safety is enhanced by its dual-system architecture and the aircraft’s options of single- or dual-pilot Instrument Flight Rules (IFR) avionics for all-weather operations. The Fenestron® shrouded tail rotor further ensures maximum safety for both man and machine on the ground and in flight. The Appareo Vision 1000 is a factory-installed cockpit camera and voice recorder that assists in the identification of operational risks before they can lead to incidents and accidents. This system also enables CFR Part 135 air medical operators to comply with the most recent FAA regulations for operational risk management. The H135’s noise emissions are lower than any other helicopter in its class, more than 7 dB below International Civil Aviation Organization (ICAO) standards. This low sound level is approximately 50% that of other aircraft in its class. The built-in Anti Resonance Isolation System (ARIS) reduces rotor-induced vibrations and enhances flying comfort to a maximum for both the crew and the patient. The H135 now offers the most modern avionics solution with Helionix®, designed by Airbus. Airbus Helicopters’ unique First Limit Indicator (FLI) is embedded in the Helionix® displays and considerably simplifies engine and torque monitoring. With the FLI, pilots can easily scan performance indications and can therefore dedicate more attention to safe mission execution. The 4-axis dual duplex Automatic Flight Control System (AFCS) is the first autopilot designed specifically for helicopters, providing unique control laws that dramatically reduce pilot workload and increase safety. Since its introduction in 1995, the H135 fleet has accumulated over 4.5 million total flight hours, with more than 1,200 units in service across the globe. It has proven itself as a reliable and affordable workhorse in even the most demanding of missions. Figure 2: The H135 was designed in close cooperation with medical professionals and rescue experts. 02/14/18 9 / 22 This document is the property of Airbus Helicopters, Inc. (AHI), and should be handled in accordance with the Disclosure Restriction Notice on the front cover of the document. This document, as well as the information and/or data it contains, shall not be disclosed without express written authorization of AHI. All rights reserved. II.A.1. Advanced Technology Fenestron® The Fenestron® shrouded tail rotor provides the safest ground and flight operations, enhanced anti- torque control efficiency, reduced power demand in forward flight, and lower noise and vibration levels. On the H135, the Fenestron® has a new-design tail gearbox with lower maintenance costs and incorporates a duplex tail rotor actuator and dual hydraulic circuits installed in a new, damage- tolerant all-composite tail boom. The composite Fenestron® rotor blades are damage-tolerant and reduce the risk of corrosion and exposure to foreign object damage. In the unlikely event of a loss of tail rotor drive or pitch control, the Fenestron® design allows for continuous flight at speeds of 50-60 knots. Helionix® Helionix® is Airbus Helicopters’ advanced, innovative avionics system, now operating in the H135, H145, H160, and H175. This avionics system delivers the latest in human-machine interface technology and has been optimized to provide clear and easily understandable information. Helionix® meets the latest international avionics standards and provides unrivalled in-flight envelope protection, pilot assistance, and situational awareness. These features result in dramatically reduced pilot workload and increased safety levels. The Helionix® installation incorporates the most innovative alerting and self-monitoring system. Additionally, the system has open architecture and a modular design with very high redundancy (dual-duplex). It is also capable of embedding future mission functions. The most significant embedded function is the advanced dual-duplex 4-axis autopilot specifically designed for helicopters. This offers high flight stability and precision, unique flight envelope and over-limit protection, automated takeoff, and fully-coupled approaches to hover, among other benefits. Examples of the functionality delivered by Helionix® include: Enhanced pilot assistance provided by the 4-axis digital AFCS that includes new upper modes which expand the aircraft capabilities for both day and night missions, particularly in low visibility conditions and over water, such as in a Search and Rescue environment Best in class Satellite Based Augmentation System (SBAS) navigation to execute fully coupled WAAS LPV and LNAV/VNAV approaches up to and including 10° glide path angle at speeds down to 30 KIAS Figure 3: The Fenestron® tail rotor enhances safety and performance while reducing noise. 02/14/18 10 / 22 This document is the property of Airbus Helicopters, Inc. (AHI), and should be handled in accordance with the Disclosure Restriction Notice on the front cover of the document. This document, as well as the information and/or data it contains, shall not be disclosed without express written authorization of AHI. All rights reserved. Enhanced situational awareness with integrated optional equipment, such as Automatic Dependent Surveillance-Broadcast (ADS-B) out, Moving Map, Helicopter Terrain Awareness System (HTAWS), and Synthetic Vision System (SVS) Reduced pilot workload with an innovative crew alerting concept, including the one hundred feet Above Ground Level (AGL) alert and on demand Vehicle Management System (VMS) Reduced pilot workload by intuitive determination of All Engines Operating (AEO) and One Engine Inoperative (OEI) power available by combining the power limit and FLI in one indication Reduced pilot workload with an intuitive Human Machine Interface (HMI) Unrivalled level of redundancy resulting from all functions embedded in each Multi- Function Display (MFD), dual-duplex aircraft management computers, and 2 Attitude and Heading Reference Sensors (in IFR configuration), plus an Integrated Electr onic Stand-by Instrument (IESI) Full Usage Monitoring System (UMS) included in the basic Helionix® package; a health monitoring option is available to provide HUMS® Figure 4: The Helionix® cockpit system with 4-axis autopilot significantly reduces the workload of the pilot and brings the H135 to an unrivalled level of safety. 02/14/18 11 / 22 This document is the property of Airbus Helicopters, Inc. (AHI), and should be handled in accordance with the Disclosure Restriction Notice on the front cover of the document. This document, as well as the information and/or data it contains, shall not be disclosed without express written authorization of AHI. All rights reserved. Helionix® provides enhanced safety with failure analysis and automatic reconfiguration performed by the system (no pilot action required). The incorrect management of failures is therefore averted. The Helionix® provides clear displays of failure, and the systems status facilitates the decision-making process. The Vehicle and Engine Multifunction Display (VEMD) Monitoring System page is automatically displayed during start-up and at the pilot’s command any time during flight. The 4-axis AFCS dual-duplex design provides for high redundancy, automatic take-off procedure, automatic cyclic trim below 30 kts, and automatic engine management in the event of FADEC malfunction. The system provides flight envelope protection and displays the AEO/OEI available power to the pilot via the VMS Full Authority Digital Engine Control (FADEC). The new priority management between collective and pitch axes (high speed/ economic mode) enables Engine and MGB protection, with permanent power limited to MTOP below Vy and Vne in 3-axis mode. The system has features that actively monitor and prevent Controlled Flight into Terrain (CFIT) settling with power. There are 130 Airbus helicopters in service with Helionix® avionics. The successful entry into service started with the H175 in 2014, followed by the H145 in 2015 and the H135 in 2017. The H160 will be the next to implement Helionix®, anticipated in 2019. The rapid adoption of this technology is a testimony to the reliability of the Airbus advanced glass cockpit solution. This shows the level of maturity of new platforms being used every day by our customers. Helionix® implementation is supported by the Helionix® Advanced Training Simulator (HATS). This desktop training system provides specialized functions for cockpit, operational procedure, and emergency procedure training. Additionally, the HATS simulator provides a Safety Management System Function and Troubleshooting Function as well as performs the operate training function. The system uses real flight control grips and Xplane® database customization. Figure 5: The HATS training system provides a smooth transition to the Helionix® avionics system with rapid pilot orientation and operational experience. 02/14/18 12 / 22 This document is the property of Airbus Helicopters, Inc. (AHI), and should be handled in accordance with the Disclosure Restriction Notice on the front cover of the document. This document, as well as the information and/or data it contains, shall not be disclosed without express written authorization of AHI. All rights reserved. II.B. H135 in Emergency Medical Services Missions The H135 brings added confidence during the rapid deployment of personnel, offering superior capability and the versatility to meet time-critical operational requirements. Its design incorporates a lightweight cockpit layout, compact dimensions, and remarkable performance with excellent outside visibility, as well as a modular, flexible cabin arrangement. Quick and easy patient loading is ensured via the rear clamshell doors, even when rotors are running. The H135’s external sound signature, far below the strictest regulatory specifications, allows operations in close approach to hospitals, often situated in urban areas. The H135 is equipped with durable high skid landing gear. The skids, combined with the H135’s compact design, allow touchdowns in very confined areas or on unprepared terrain. The helicopter can make pinpoint landings close to the patient with optimum safety as a result of its high mounted main rotor and protected Fenestron® tail rotor. II.B.1. Air Ambulance Capabilities and Configuration The H135 is a mission-fit platform for Emergency Medical Services, offering maximum mission flexibility and supporting the ability to accommodate multiple EMS interior solutions. With a combined cabin and cargo volume of more than 173 cubic feet, patient care in the H135 accommodates advanced life support, critical care, and specialty team transports. The spacious cabin can fit up to three (3) clinical crew members and the required specialty team equipment. Similar to a ground ambulance orientation, the longitudinal placement of the patient(s) enables optimum, ergonomic patient-to-crew alignment for performance of critical, life-saving, advanced interventions while in a secure, belted position during flight. Multiple EMS interior options exist for the H135. This versatile cabin environment lends itself to Collier County MedFlight’s ongoing requirements of each and every patient served. Combined with the flat floor, the use of the seat rails to secure crew, equipment, and patients provides maximum access as well as the highest level of safety for patients and medical crew. The flat floor design allows for accommodation of crash-resistant crew seats as well as maximum Figure 6: The configuration of the H135 and custom options have been carefully considered in the performance of the EMS mission, providing critical patient access while ensuring enhanced crew safety. 02/14/18 13 / 22 This document is the property of Airbus Helicopters, Inc. (AHI), and should be handled in accordance with the Disclosure Restriction Notice on the front cover of the document. This document, as well as the information and/or data it contains, shall not be disclosed without express written authorization of AHI. All rights reserved. flexibility and versatility to meet Collier County MedFlight’s current and future mission needs. The H135 offers ample room for up to either three (3) medical seats and one (1) stretcher, or two (2) medical seats and two (2) stretchers. II.B.2. EMS Interior Completion AHI has a long-standing partnership for EMS helicopter completions with Metro Aviation, the largest rotorcraft completion center in the United States. FAA- and FAR-certified, Metro Aviation is well-equipped to provide EMS interior solutions to Collier County. Metro Aviation’s 160,000 sqft comprehensive completion facility is based in Shreveport, Louisiana, where they provide services for painting, avionics, machining, production, and maintenance. Their completion capabilities include in-house engineering, 2D and 3D services, and in-house FAA maintenance and manufacturing DAR support. Metro Aviation has performed completion services for over 200 EC135/H135 aircraft , more than any other completion center in the world, as well as completions for all of the nation’s major air medical operators. Metro Aviation’s fully vetted, FAA-certified EMS interior will enable Collier County MedFlight to continue to provide the broad spectrum of clinical care the citizens of Collier County have come to rely on. Figure 7: The H135 cabin features a modular design easily adaptable to different users’ needs. 02/14/18 14 / 22 This document is the property of Airbus Helicopters, Inc. (AHI), and should be handled in accordance with the Disclosure Restriction Notice on the front cover of the document. This document, as well as the information and/or data it contains, shall not be disclosed without express written authorization of AHI. All rights reserved. II.C. H135 Performance The H135 delivers exceptional power reserves, enhanced safety margins, and best-in-class payload. This results from the hinge-less and bearing-less main rotor system. Our H135 offer to you comes outfitted with Turbomeca’s Arrius 2B2Plus engine, which is FADEC controlled and provides efficient fuel burn characteristics. This reliable turboshaft engine delivers outstanding performance and vital reserves, even in OEI scenarios. The H135’s performance increased in 2015 with the introduction of this latest variant, adding over 440 pounds of payload at 7000 feet. Its maximum take-off weight (6,570 pounds) enables the fully configured H135 (EMS interior, one pilot, two crew, 100 pound carry-on medical equipment, 250 pound patient, and 20 minute reserve fuel) to meet an impressive range of 285 nautical miles (SL, ISA +20). Pictured below is a map depicting the “radius” from Naples in Collier County. The H135 in EMS configuration with standard payload can fly up to 143 nautical miles from Naples and return without refueling. Figure 8: Radius from Collier County - EMS Configuration at max cruise speed - SL, ISA+20 conditions. The full range of the H135 in EMS configuration with standard payload (i.e., the farthest the helicopter can fly before it has to refuel) is 285 nautical miles. The map below shows the exceptional full range of this aircraft from Naples. 02/14/18 15 / 22 This document is the property of Airbus Helicopters, Inc. (AHI), and should be handled in accordance with the Disclosure Restriction Notice on the front cover of the document. This document, as well as the information and/or data it contains, shall not be disclosed without express written authorization of AHI. All rights reserved. Figure 9: Range from Collier County - EMS configuration at max cruise speed - SL, ISA+20 conditions. II.C.1. H135 Maintenance Because Collier County is currently operating the EC135T1 aircraft, the addition of a new H135 will allow for a relatively seamless induction effort with minimal impact to Collier County’s existing maintenance processes and procedures. Maintenance intervals will remain unchanged with no additional manual subscription requirements due to the evolution of the maintenance plan and extended scheduled inspection intervals. In most cases the airframe and engine tooling will be common, reducing any non-recurring investments required to support the new model H135. Relative to training, only a differences course will be required for the Collier County Maintenance Technicians to be certified to support the new H135 aircraft. The benefits resulting from these commonalities make the H135 a logical and cost effective solution for Collier County. Major Maintenance Intervals The H135 benefits from the experience of its extensive in-service fleet of over 1,200 helicopters with more than 4,405,500 accumulated flight hours. This experience has encouraged continuous maintenance improvement and has enabled the extension of scheduled inspection timeframes, as shown in the table below. 02/14/18 16 / 22 This document is the property of Airbus Helicopters, Inc. (AHI), and should be handled in accordance with the Disclosure Restriction Notice on the front cover of the document. This document, as well as the information and/or data it contains, shall not be disclosed without express written authorization of AHI. All rights reserved. Inspection Previous New Intermediate Inspection Schedule 400 FH 500 FH Exceedance Tolerance 40 FH 50 FH Periodical Inspection Schedule 800 FH / 3 years 1,000 FH / 3 years Exceedance Tolerance 80 FH / 3 months 100 FH / 3 months The Turbomeca Arrius 2B2Plus engine inspection schedule is as follows: Arrius 2B2Plus Inspections 200 FH 400 FH 500 FH 800 FH 1000 FH 15 Years Support and Services III. III.A. Customer Support The moment an Airbus Helicopters aircraft is delivered, one of our primary missions begins: providing our customer with the necessary support and services to carry out their operations as efficiently, safely, and cost-effectively as possible. Airbus Helicopters’ global Customer Service network works around the clock to fulfill this mission, bringing tailor-made and competitive solutions to our customers' doorsteps. As operators’ requirements evolve and their missions become more demanding, we at Airbus Helicopters continuously adapt our service portfolio to fit our customers’ needs. Airbus Helicopters supports more than 600 customers operating over 1900 aircraft throughout the nation, and we are committed to supporting your Airbus Helicopters product with the same level of excellence that you have come to expect from our aircraft. We are dedicated to looking out for the best interests of our customers, whether this be maximizing flight revenues, ensuring public safety, or saving lives, and our Customer Support team is at your service 24/7 to keep you flying. Our customer support offerings include everything you need to minimize downtime and maximize efficiency: logistics services, with a dedicated logistics warehouse located at Dallas/Fort Worth International Airport; technical support, provided by a dedicated team of highly experienced Technical Representatives based at our headquarters and Regional Technical Representatives located in the field; technical publications, including manuals, bulletins, and a growing range of electronic publications; and aftermarket services, which offer you a wide range of ways to enhance the performance of your Airbus Helicopters aircraft while minimizing operational costs. The Customer Support Manager (CSM) works closely with our Sales and Marketing team to address all customer support concerns. The Customer Support Manager is the focal point for 02/14/18 17 / 22 This document is the property of Airbus Helicopters, Inc. (AHI), and should be handled in accordance with the Disclosure Restriction Notice on the front cover of the document. This document, as well as the information and/or data it contains, shall not be disclosed without express written authorization of AHI. All rights reserved. our customers regarding support and services. The CSM is accountable for customer satisfaction and loyalty and will monitor the continuous improvement of the relationship. Each customer is also assigned a Customer Support Representative in our Spares Command Center; this person works closely with the CSM on the resolution of any customer needs. It is our mission that you enjoy a seamless transition from the acquisition of your helicopter to years of hassle-free flying. We are always here to help you, and hope to make the operation of your Airbus Helicopters product as simple and reliable as flying it. III.A.1. Technical Support Airbus Helicopters’ Technical Services team is optimized and prepared to support our U.S. customers who depend on our expertise for routine and unplanned technical events. Located in- house in Grand Prairie, Texas, as well as in the field throughout the U.S., this team’s primary focus is to deliver response-appropriate and expert technical knowledge whenever needed, maximizing our customers’ aircraft dispatch availability. These dedicated professionals provide a full spectrum of services, from answering the simplest technical inquiries about routine operation and maintenance of the aircraft to solving the most complex troubleshooting of any technical needs that may arise. Airbus Helicopters’ Technical Services are AS9100 and ISO:9001 certified, and our Technical Team members are licensed aircraft and power plant technicians. Additionally, the Technical Team undergoes Airbus-specific airframe initial training and participates in extensive ongoing education to establish and advance their knowledge of the Airbus Helicopter product line. Team members are further specialized by airframe, ensuring our customers are connected with a qualified, expert technical representative for every Airbus aircraft they fly. Additional expertise on the team is focused on the technical support of avionics systems. We close 85% of technical support inquiries in one (1) day or less, and 100% within t hree (3) days. Our satisfaction rate on technical support responses is at 99%. III.A.2. Spare Parts Our commercial spares inventory now averages $183 million, a 123% increase since 2013. More than 60,000 unique part numbers are in stock at our 80,000 square foot logistics warehouse, located at the Dallas/Fort Worth International Airport to ensure efficient movement of parts from Airbus to you. Spare parts are delivered by the date requested more than 96% of Figure 10: AHI’s Customer Support team is dedicated to providing the best support in the industry. 02/14/18 18 / 22 This document is the property of Airbus Helicopters, Inc. (AHI), and should be handled in accordance with the Disclosure Restriction Notice on the front cover of the document. This document, as well as the information and/or data it contains, shall not be disclosed without express written authorization of AHI. All rights reserved. the time. Our performance is at 100% for planned spares orders. Our Aircraft on Ground (AOG) performance continues to improve; 98% of needed parts are ready for shipment with an air waybill within 4 hours. We have implemented numerous changes and new functionalities to our Keycopter e- commerce customer service portal system for online ordering and product support. The Webtek function is a means to easily communicate with a technical support adviser. eBook repair is now available on ORION (Optimized Reader for Internet and Other Networks) in Keycopter; this manual contains some of the more common repairs and reduces time in generating customized repair requests. Built up from operators’ return on experience from the field, a comprehensive material management offer is at your disposal from Airbus Helicopters. HCare Material Management offerings provide firm commitments and operational cost-reduction for better competitiveness, including: Committed performance on Smart plans Secured performance on Easy Repair and Easy Exchange services 2 lines of service package answering customers’ mission specifics Our services include: Easy Part o Spare Parts o Repair and Overhaul o Standard Exchange Easy Rental o Rent a tool or a Ground Support Equipment (GSE) when it is needed, and for the period you define o Applicable to a growing list of part numbers available within the group Easy Repair o A new standard for Repair and Overhaul services offering more service for the same price o Short and fixed repair turnaround times secured by a dedicated pool o Applicable to the whole Airbus Helicopters range o A catalogue of part numbers eligible for this solution is available on Keycopter and covers all of our helicopter types Easy Exchange o This solution entails the replacement of parts that have reached the end of their life expectancies o Parts availability is secured by a dedicated pool, prices are fixed with no exclusions on most part numbers, and delivery is timely o A catalogue of part numbers eligible for this solution is available on Keycopter and covers all of our helicopter types 02/14/18 19 / 22 This document is the property of Airbus Helicopters, Inc. (AHI), and should be handled in accordance with the Disclosure Restriction Notice on the front cover of the document. This document, as well as the information and/or data it contains, shall not be disclosed without express written authorization of AHI. All rights reserved. III.B. Aircraft Support III.B.1. Warranty Airbus Helicopters offers exceptional airframe warranty coverage for the H135: three (3) years or 2,000 flight hours (whichever comes first). The airframe warranty labor coverage is provided for one (1) year or 1,000 hours (whichever comes first); for the first year, warranty repair labor conducted by Collier County’s maintenance staff will be credited to your trade account at a rate of $190/hour. Turbomeca’s engine warranty covers two (2) years or 1,000 hours (whichever comes first). The table below outlines the specific warranty coverages offered. Warranty Coverage Flight Hours Year 1 Year 2 Year 3 Airframe 2,000 Covered Covered Covered Airframe Labor 1,000 Covered Engine 1,000 Covered Covered III.B.2. HCare Airbus Smart programs offer flexible coverage options to best suit each customer’s particular operational needs. The options we offer range from support of primary cost drivers to comprehensive nose to tail coverage. Parts by the Hour (PBH): coverage of scheduled and unscheduled component repairs Exchange by the Hour (EBH): reduced cost, no buy-in, standard exchange for unscheduled events Full by the Hour (FBH): nose to tail coverage, including standard PBH coverage plus consumable parts with either a $0 or $250 deductible Repair by the Hour (RBH): reduced cost, with secured repair Turn Around Time (TAT) for customers who prefer to own and control their inventory The benefits of a Smart support program extend beyond keeping your Airbus Helicopter in the air. Other HCare benefits extend beyond keeping your Airbus helicopter in the air: Increased aircraft residual value Leveling aircraft operating expense Reducing aircraft spare inventory cost Lower aircraft spares management expenses Improved aircraft availability New in 2018, we have reduced hourly rates during the warranty period (40% discount) and fewer excluded items. For Collier County, we are offering a 3% discount on HCare rates. The estimated buy-in to the PBH program for Collier County is $92,921 at 1,000 hours in 2021. This calculation is based on 02/14/18 20 / 22 This document is the property of Airbus Helicopters, Inc. (AHI), and should be handled in accordance with the Disclosure Restriction Notice on the front cover of the document. This document, as well as the information and/or data it contains, shall not be disclosed without express written authorization of AHI. All rights reserved. components that have service life limits or an overhaul interval, which are contained in dynamics, blades, and avionics in the list of parts defined in the attached HCare presentation. The estimate for the Turbomeca engines at the end of the second year is $104,009, assuming 600 TTAF after two (2) years. III.C. Pilot and Technician Training The AHI Training Center offers turnkey pilot and technician training services included in every aircraft sale. Emphasis is placed on a blended learning approach in small classes, with hands - on learning utilizing computer-based simulation tools to practice failures, troubleshooting, and emergency procedures, as well as component location and virtual maintenance tasks. Customer aircraft is used for all pilot training, so that pilots can train on the exact configuration that they will be flying. Figure 11: Airbus Helicopters blended training approach and associated tools and methods. III.C.1. Pilot Training The H135 Helionix® Pilot Transition VFR class is a three (3) week blended training course that includes ten (10) days of theoretical instruction and seven (7) to eight (8) hours of flight on the 02/14/18 21 / 22 This document is the property of Airbus Helicopters, Inc. (AHI), and should be handled in accordance with the Disclosure Restriction Notice on the front cover of the document. This document, as well as the information and/or data it contains, shall not be disclosed without express written authorization of AHI. All rights reserved. customer’s aircraft. Use of the Helionix® Advanced Training System (HATS), a multi-screen computer-based simulator, allows student pilots to practice after each section of theory. The HATS was developed using real aircraft flight loops and can simulate all aircraft systems (navigation, hydraulic, fuel, electrical), as well as over 300 aircraft malfunctions. Both technician and pilot students use the HATS to practice troubleshooting, normal and emergency procedures, and cockpit orientation. Pilot recurrency classes are available to support the continuing education of pilots 12 months or more after completion of an initial transition class. Figure 12: Helionix® Advanced Training System (HATS) multi-screen display. III.C.2. Technician Training Technician training on the H135 Helionix® is a robust program of courses covering airframe maintenance, avionics, and engine. Airframe and avionics courses are three (3) weeks each of classroom and hands-on practical exercises. In addition to utilizing the HATS, airframe and avionics courses also utilize physical aircraft component mock -ups and the Virtual Maintenance Trainer (VMT), a computer-based tool that allows students to explore a 3D aircraft, locate components, and simulate maintenance tasks. Engine maintenance courses are provided through Turbomeca USA, located in a neighboring facility to Airbus Helicopters, Inc., in Grand Prairie, Texas. Engine courses are typically one (1) week in duration and can be scheduled through AHI. Technician refresher classes are available to support the continuing education of technicians who have completed initial airframe or avionics courses. 02/14/18 22 / 22 This document is the property of Airbus Helicopters, Inc. (AHI), and should be handled in accordance with the Disclosure Restriction Notice on the front cover of the document. This document, as well as the information and/or data it contains, shall not be disclosed without express written authorization of AHI. All rights reserved. Project Approach IV. Airbus Helicopters offers support to Collier County MedFlight from order to delivery and beyond. Our market share standing within the Emergency Medical Services segment positions us as the best qualified manufacturer and support services provider to offer the right mission-fit helicopter for Collier County. With 40+ years of U.S.-based operations, we possess the necessary collective experience to support the vital missions you serve. The following outlines our approach to this project. 1. Program Management a. Regular updates on aircraft production and delivery timing from Airbus Helicopters (Donauwörth, Germany) and Metro Aviation 2. Training a. Tailored pilot training program that includes: i. Ground instruction in the classroom and utilizing the Helionix® Avionics Training System ii. Flight training instruction in Collier County MedFlight aircraft after its delivery in Grand Prairie, Texas b. Tailored maintenance technician training program that includes: i. Ground instruction in the classroom and utilizing the Helionix® Avionics Training System and H135 maintenance training aids ii. Turbomeca Arrius 2B2Plus engine training at Turbomeca USA facility in Grand Prairie, Texas 3. Support and Services a. Coordinated and aligned technical support from Airbus Helicopters and Turbomeca USA technical representatives that will begin prior to delivery b. Logistics support from Airbus Helicopters’ Customer Support Manager to assist with management of warranty and/or HCare (and Turbomeca SBH), if selected We are fully committed to our relationship with Collier County MedFlight and to the continued safe and successful execution of your mission. Adding an H135 with Helionix® to your fleet represents a significant increase in capability and technology for Collier County MedFlight, and we look forward to providing all of the necessary assistance to ensure a seamless transition into this aircraft. Exhibits A Declaration Statement & Conflict of Interest Affidavit B H135 2018 Technical Data Book C Collier County HCare Presentation This Page Intentionally Left Blank Exhibits A Declaration Statement & Conflict of Interest Affidavit B H135 2018 Technical Data Book C Collier County HCare Presentation This Page Intentionally Left Blank Exhibits A Declaration Statement & Conflict of Interest Affidavit B H135 2018 Technical Data Book C Collier County HCare Presentation This Page Intentionally Left Blank H135 Technical Data 2018 HELICOPTERS 135 T3H/P3H 18.101.01 E 1 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data Contents 1 Foreword...................................................................................................................................................... 3 1.1 Baseline Aircraft Highlights and Main Improvements ........................................................................... 6 2 General Characteristics............................................................................................................................ 19 2.1 Cockpit and Cabin Layouts ................................................................................................................ 19 2.2 Weight................................................................................................................................................. 19 2.3 Power Ratings..................................................................................................................................... 19 2.4 Fuel Capacities................................................................................................................................... 20 2.5 External Dimensions........................................................................................................................... 21 2.6 Internal Dimensions............................................................................................................................ 22 2.7 External Sound Levels........................................................................................................................ 22 2.8 Touch Down Forces............................................................................................................................ 23 3 Baseline Aircraft Definition...................................................................................................................... 25 4 Mission Configurations............................................................................................................................ 27 4.1 Emergency Medical Services (EMS) Mission..................................................................................... 28 4.2 Law Enforcement Mission................................................................................................................... 37 4.3 Offshore Transportation Mission......................................................................................................... 45 4.4 Aerial Work Mission............................................................................................................................ 52 5 Further Equipment Information............................................................................................................... 59 5.1 General Available Equipment ............................................................................................................. 59 5.2 Avionics Layout................................................................................................................................... 66 5.3 Antenna Layout................................................................................................................................... 68 5.4 NVG friendly & NVIS Certification....................................................................................................... 69 5.5 Disclaimers ......................................................................................................................................... 70 6 Main Performance..................................................................................................................................... 71 6.1 Performance Summary Tables........................................................................................................... 71 6.2 Operating Limitations.......................................................................................................................... 83 6.3 Performance Charts............................................................................................................................ 84 7 Service and Support Information ............................................................................................................ 97 7.1 Assets................................................................................................................................................. 97 7.2 H135 Inspection Programs ................................................................................................................. 97 7.3 Main Components Limitations............................................................................................................. 99 7.4 HCare - Material Management ......................................................................................................... 101 7.5 Engine Service and Support Programs............................................................................................. 104 7.6 HCare - Helicopter Maintenance....................................................................................................... 107 7.7 HCare - Technical Support ............................................................................................................... 108 7.8 HCare - Training & Flight Ops........................................................................................................... 110 7.9 Flight Operations Services................................................................................................................ 112 7.10 HCare - Connected Services.......................................................................................................... 113 8 Abbreviations.......................................................................................................................................... 115 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 2 135 T3H/P3H 18.101.01 E Technical Data Preliminary Data The data provided in this document is under validation. Final confirmation of the data after finalization of flight test program. 135 T3H/P3H 18.101.01 E 3 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 1Foreword The H135 equipped with Helionix® is Airbus‘® light twin-engine multi-purpose helicopter in the 3 ton class, with up to 8 seats for pilots and passengers. The H135 delivers exceptional power reserves including full class 1 & class 2 performances, enhanced safety margins, best-in-class payload and the industry benchmark for control response and precision flying thanks to the hinge and bearing less main rotor system. All composite main rotor blades, with an advanced tip geometry design, in combination with the Fenestron® anti-torque system make the H135 the quietest helicopter in its class, with certified sound levels well below the ultra-stringent ICAO limit. The built-in Anti Resonance Isolation System (ARIS) reduces rotor-induced vibrations and enhances flying comfort to a maximum. The H135 combines Airbus latest Helionix technologies, including an advanced cockpit design with the most modern Human Machine Interface (HMI). The innovative Helionix avionics system has an open architecture and modular design with very high redundancy (dual duplex) incorporating embedded functions as well as the capability for further integration of mission functions. The most significant embedded function is the 4-axis dual duplex AFCS which is a further evolution of the H225 autopilot. The functionalities, level of safety and the mission capability enhancements offered by this autopilot are currently the benchmark in the helicopter industry. The H135 is certified to the latest CS 27/FAR 27 crashworthiness standards, including energy absorbing fuselage, seats and crash resistant fuel cells. The safety of twin engine performance is complemented with redundancy incorporated in the hydraulics, electrics, main transmission oil cooling and lubrication systems. In addition, the H135 features the best cockpit field of view and unmatched HMI, granting the lowest pilot workload and therefore minimizing pilot fatigue and increasing mission capability. The H135 can be powered by either Safran Helicopter Engines Arrius 2B2plus or Pratt & Whitney Canada PW206B3 engines - both are FADEC controlled and provide efficient fuel burn characteristics. These powerful and reliable engines, combined with the improved dynamic lifting system components, provide outstanding performance and vital power reserves especially in One Engine Inoperative (OEI) scenarios and in all flight regimes including demanding High & Hot conditions. Figure 1.1: Example of the H135® The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 4 135 T3H/P3H 18.101.01 E Technical Data A main rotor design, which does not require a main rotor head and associated components, contributes to the highest safety standards, the lowest maintenance costs and an outstanding control response for precision flying. The extensive fleet experience and high level of product maturity has enabled the H135's maintenance scheme to be 'trimmed to perfection' delivering H135 operators with high intervals for the scheduled inspections, excellent maintainability, high TBO times, outstanding reliability and availability. To optimize aircraft availability even further, the Continuous Maintenance Program (CMP) allows customers to perform the scheduled inspections easily, step by step at any time the aircraft is not operationally required, for example in evenings or during periods of poor weather. The enormous flexibility offered by the CMP results in the maximum of aircraft operational availability. The exceptional payload of the H135 is the result of modern technology fabrication in conjunction with an extensive use of composite materials. The high degree of composite usage in the fuselage does not only result in a low empty weight but it also provides a high degree of safety and resistance against corrosive operating environments. For training purposes, an OEI training mode is integrated in the basic aircraft which provides, by simulation, a very realistic single engine emergency procedures training environment while maintaining optimum safety for the crew and aircraft. A wide range of quickly interchangeable optional equipment is available for the H135 and with the most versatile cabin layout the H135 is readily able to operate in different mission configurations, including EMS, Law Enforcement, Aerial Work, Offshore Transportation, Training and other specialized applications. The H135 offers a spacious cabin, featuring: • Excellent outside visibility for pilots and passengers • Unrivalled side loading (no door posts) and rear loading capability (even with rotors turning) • Cabin area with unobstructed flat floor and integrated seat / mounting rails The Helionix avionics system installed in the H135 is born from the latest generation of Airbus avionics family, integrated also in the H145®, H160® and H175®, designed to provide enhanced safety and mission capability along with simplified maintainability. Helionix benefits from the long experience accumulated by Airbus in the development of innovative avionics. The H135 Helionix installation includes a glass cockpit with a highly efficient HMI designed to reduce the pilot workload and increase the flight safety while enabling more concentration on the mission at hand. The Helionix Flight Display Subsystem (FDS) is composed of smart Multifunction Displays (MFD) providing state-of-the-art quality and precise imaging of flight parameters. The Active Matrix Liquid Crystal Displays (AMLCD) feature perfect readability from any angle and in any light condition. The Figure 1.2: View from rear into the empty cabin 135 T3H/P3H 18.101.01 E 5 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data pilot display offers all the flight, navigation and vehicle relevant data while the remaining displays are configurable for flight, vehicle or mission data, and offer an exceptional display platform for mission equipment including for example, Moving map and High Definition (HD) Electro Optical Systems. Maintenance crews will benefit from the new concept for enhanced maintainability with user-friendly software management, failure codes recording and trouble-shooting algorithm. With Helionix, the flight crew will experience: • Enhanced pilot assistance provided by the most advanced 4-axis digital AFCS including innovative upper modes which expand the aircraft capabilities for both day and night missions, particularly in low visibility conditions and over water. For example, in the SAR environment. • Best in class SBAS navigation to execute fully coupled 4-axis AFCS LPV and LNAV/VNAV approaches up to and including 10° glide path angle at speeds down to 30 KIAS. • Enhanced situation awareness with integrated optional equipment such as Automatic Dependent Surveillance-Broadcast (ADS-B) out, Moving map, Helicopter Terrain Awareness and Warning System (H-TAWS) and Synthetic Vision System (SVS). • Reduced pilot workload with innovative crew alerting concept including the one hundred feet AGL alert (required by EASA OPS) and on demand Vehicle Management Subsystem (VMS). • Reduced pilot workload by intuitive determination of AEO and OEI power available by combining the power limit & FLI in one indication. • Reduced pilot workload with an intuitive Human Machine Interface (HMI). • Unrivalled level of redundancy resulting from all functions embedded in each MFD, dual duplex aircraft management computers and 2 Attitude and Heading Reference Systems (in IFR configuration), plus an Integrated Electronic Stand-by Instrument (IESI). • Full Usage Monitoring System (UMS) included in the basic Helionix package. Health monitoring option is available to provide HUMS®. The unique color coding, warning and information concept helps the pilot(s) to identify vital information instantaneously while suppressing presentation of non-relevant parameters. Additionally, the H135's unique First Limit Indicator (FLI) considerably simplifies engine and torque monitoring. The pilot(s) workload is minimized and thus allowing more attention to be safely dedicated to the mission at hand. Airbus has built and delivered H135/H135M helicopters since 1996. More than 1,250 aircraft are in service worldwide. The total flight hours accumulated at the end of August 2017 were approximately 4,440,000 Fh. The fleet leading aircraft has accumulated approximately 15,000 Fh. Figure 1.3: Typical instrument panel (single / dual pilot) The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 6 135 T3H/P3H 18.101.01 E Technical Data 1.1 Baseline Aircraft Highlights and Main Improvements Maintenance Reduction Benefitting from the experience of more than 1,250 aircraft in service and over 4.4 million flight hours, Airbus has further streamlined the H135 maintenance requirements to ensure lowest Direct Maintenance Costs (DMC) and lowest Direct Operating Costs (DOC) in the light twin helicopter class without compromising safety. Thanks to the extensive experience in close collaboration with Airbus customers overhaul times and/or Service Life Limits (SLL) of the following components were increased: By streamlining the scheduled inspection tasks also the required mean man hours could be reduced: Pratt & Whitney Canada has extended the previous 800 Fh inspection to 1,000 Fh for the PW206B3 engine, thus now aligning with the airframe inspection interval schedule. Flight Data Continuous Recorder (FDCR) The Flight Data Continuous Recorder (FDCR), built into the Helionix avionics, collects vehicle and engine parameters, records the data continuously and downloads the data onto the Compact Flash card in the Data Transfer Device (DTD). Analysis of the recorded data post flights supports operator programs, including Helicopter Flight Data Monitoring (HFDM) and maintenance activities. Airframe main components TBO /SLL Old value New value Control rod SLL 19,200 Fh on condition Hinged support SLL 12,300 Fh 30,000 Fh Main rotor blade SLL 12,400 Fh on condition Main rotor blade damper SLL 4,800 Fh or 10 years 12 years Main transmission housing SLL 7,000 Fh on condition Mixing lever gear unit forked lever SLL 11,500 Fh 30,000 Fh Swash plate bearing & control ring SLL 6,700 Fh on condition Starter / generator TBO 1,000 Fh usage based Main transmission TBO 4,000 Fh 5,000 Fh Tail rotor transmission TBO 3,600 Fh 5,000 Fh Scheduled airframe inspections Old estimated mean man hours New estimated mean man hours 12-month inspection 20 19 Intermediated inspection every 500 Fh 28 26 Periodical inspection every 1,000 Fh or 3 years 111 80 Engine Arrius 2B2plus 500 Fh inspection 4 2.5 135 T3H/P3H 18.101.01 E 7 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data Fleet Keeper® Fleet Keeper is a user-friendly electronic Technical LogBook (TLB) application, completely replacing the paper TLB and improving the process by delivering a cockpit view of customers' fleet status. It enables real-time data exchange between pilots, line mechanics and airworthiness managers. Fleet Keeper is a secured cloud-based solution in combination with a user-friendly web and mobile application. It handles pilot tasks like pre- and post-flight checks, recording of flight data and events as well as line maintenance and airworthiness duties, including management of line maintenance, events and discrepancies or electronic signatures. Data download from Fleet Keeper enables easy and quick transfer into Maintenance Information Systems (e.g. CAMO tools). It is compatible with all Airbus helicopter models, as well as those of other manufacturers. Fleet Keeper is a deployable tool ready to replace operators' paper technical logbooks, by meeting EASA M.A.306 & FAA Part 135 regulations. Figure 1.4: Fleet keeper example The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 8 135 T3H/P3H 18.101.01 E Technical Data Flight Planner® Flight Planner is Airbus' comprehensive application for helicopter portable Electronic Flight Bag (EFB). This software, running on mobile devices, is dedicated to flight crews, and is fully adapted for an efficient mission preparation. The all-in-one application provides useful features reducing significantly crew workload such as: • Interactive flight & mission planning with feasibility check, • Helicopter performance and weight & balance calculation, • Maps and terrain display, navigation data, airport charts, • Electronic documents display (eTechPub…), • Weather and NOTAM access and consultation. Figure 1.5: Flight Planner mission computation example 135 T3H/P3H 18.101.01 E 9 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data Optimized aerodynamic Airbus developed new, optimized aerodynamic elements for H135 granting optimal mission capability. More in detail: • The vertical fin is extended in its upper section to extend the envelope of the autopilot • The oil cooler cowling and the engine exhaust pipes are tailored to the specific characteristics of each engine, with shorter shapes for Safran Helicopter Engines and extended geometries for Pratt & Whitney Canada engines Figure 1.6: Example of H135 equipped with Pratt & Whitney Canada engines Figure 1.7: Example of H135 equipped with Safran Helicopter engines The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 10 135 T3H/P3H 18.101.01 E Technical Data Optional Equipment Highlights and Main Improvements Wireless connectivity Connext (Garmin) Garmin's Connext is based on Garmin's Flight Stream 210 using Bluetooth technology. The option enables wireless data exchange between the helicopters built-in GTN 750 and electronic devices, such as: • Flight plan up-/download and synchronization • GPS position transmission EMS floor The EMS floor is a lightweight, ruggedized floor that is available as optional equipment and replaces the standard cabin floor. The airline-style rail location is optimized for EMS missions in terms of cabin arrangement and access to the patient. Beside the standard rails, e.g. for stretcher installation, it provides also 12" track rails to enable the installation of 12" medical seats without requiring additional seat adapters. The floor has a fully flat, hard anodized surface, which improves the corrosion and scratch resistance and the cleaning and disinfection capability. Anti-slip-stripes are integrated in the forward cabin part. The main floor is machined out of one piece of rigid aluminum alloy. Reinforced, machined solid side channel covers allow maintenance access without removing the floor. An enhanced floor sealing concept avoids moisture ingress to the helicopter structure. A bumper edge at the aft end protects the H/C structure against damaging while loading from the aft. The EMS floor is designed for primary stretcher installation on the LH side. Bucher Leichtbau is the first EMS supplier offering an EMS kit adapted to the new EMS floor and benefitting from considerable weight savings. Figure 1.8: EMS floor for primary stretcher installation on LH side - typical 135 T3H/P3H 18.101.01 E 11 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data Professional Ground Station (PGS) Vision System and Helicopter Flight Data Monitoring (HFDM) Modular ground tools are available, enabling download of helicopter data and their visualization and analysis on ground: 1. Professional Ground Station (PGS) Vision System: PGS Vision System is the software, enabling users to turn raw binary data into readable charts and graphs. PGS Vision also converts CVR audio encoded data to standard Microsoft WAV file format and synchronize audio records to the flight data. PGS Vision System is typically used to visualize CVFDR data on ground. 2. Helicopter Flight Data Monitoring (HFDM): HFDM is the process of a systematic, pro-active analyzing of recorded flight data to enhance aviation safety, enabled by means of the Professional Ground Station (PGS) Analysis System. The software facilitates flight analysis and detection of events to identify and address operational risks before they can lead to incidents and accidents. Data recorded during the flight can then be used for in-depth analysis and subsequent implementation of corrective actions through training programs or changes to operational procedures. This process is assisted by presenting 3D replay of high fidelity aircraft models fully animated and synchronized to flight data enabled by the PGS Replay 3D module. The software enables data visualization, analysis and 3D replay of flight data recorded by • The Flight Data Continuous Recorder (FDCR), included in the H135 Baseline and/or, • The optional Cockpit Voice and Flight Data Recorder (CVFDR). Figure 1.9: PGS Replay 3D: Example of 3D flight replay The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 12 135 T3H/P3H 18.101.01 E Technical Data External cameras External cameras can be mounted on the helicopter, e.g. to monitor external loads or helicopter loading observation by the crew or to support identification of obstacles behind the helicopter. The color camera provides a picture with a horizontal and vertical field of view of approx. 70° x 120°, which can be indicated on the center and/or LH MFD in the cockpit. Two different camera installations are offered: • External multi-purpose camera on tail boom The camera is installed at the lower rear cover of tail boom vertical fin and features observation of the cargo hook, hoist or rope down missions and helicopter rear loading. The camera angle is pre- adjusted by means of three adjustment screws. • External rear-view camera on landing gear The camera is installed at the RH aft landing gear cross tube and features observation of the area behind the helicopter which may be beneficial for rearward takeoffs. Figure 1.10: External camera pictures displayed on Multi-Functional Display 135 T3H/P3H 18.101.01 E 13 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data Offshore The H135 offers several options to increase safety and reliability during offshore missions, or to comply with customers' or regulations' requirements. Between others: • Emergency float system with auto-activation and floatation demonstrated up to sea state 6 • Automatic Deployable Emergency Locator Transmitter (ADELT) • Emergency Life Raft System (ELRS) certified up to sea state 6 with optionally available survivor Emergency Locator Transmitter (ELT) • Helicopter Emergency Egress Lighting System (HEELS) • Search and rescue weather radar RDR-1600 by Telephonics • Lashing points for ship landings • Corrosion protection for high corrosive environment • Main rotor blade folding Figure 1.11: HEEL installation for crew and sliding doors (typical) The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 14 135 T3H/P3H 18.101.01 E Technical Data Digital Voice Control System DVCS 6100 (Becker) Alternatively to the Digital Audio Control System (DACS) from Cobham, the Digital Voice Control System DVCS 6100 from Becker is available. The DVCS 6100 allows the complete handling of intercommunication, voice communication and alert monitoring. The system also provides the following modes of operation / features: • Intercommunication between pilot, copilot and the passengers • Handling of up to 8 transceivers and 8 receivers (2 for ACU 6101) with a capability of individual volume control • Monitoring of up to 6 fixed inputs • Main volume control for receiver and intercom audio • Aircraft intercommunication in either "voice operated exchange" (VOX) or "push to talk" (PTT) controlled mode (VOX setting via individual potentiometer) • Up to 3 intercom circuits to separate cockpit and cabin communication • Optical call indication for intercom request plus aural call alert • Indication of transmission via status lights • Built in test functionality with optical indication of test status/result • In case of system failure reduced operation via "SLAVED" or "BACK-UP" mode possible • Configuration capability for system integration or maintenance shops to configure and adapt the system to the individual aircraft requirements, stored in the external memory module. The system includes two Audio Control Units (ACUs) in the cockpit, and one Remote Electronic Unit (REU). The REU also provides the possibility of communication with a winch operator as well as with the ground crew (via ground crew connector), if required. When external communication capability from the cabin is required, additional passenger audio control units ACU 6100 or ACU 6101 can be installed Figure 1.12: Audio Control Unit (ACU) 6100 pilot, copilot or pax (Becker) 135 T3H/P3H 18.101.01 E 15 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data Single pilot IFR cockpit The flexibility of H135 is underlined by the different avionic solutions available. The instrument panel can be freely configured for single or single/dual pilot operations. All solutions are offered with IFR certification: • Three flight displays can be installed in the extended instrument panel, providing the highest mission capability for single or dual pilot operations. • The Extended instrument panel in combination with two displays provides plenty of space for the customization with STC equipment. • The installation of two displays on the standard instrument panel offers the lightest possible solution, combined with extraordinary external field of view. Figure 1.13: Example of extended instrument panel with two MFD Figure 1.14: Example of standard single pilot instrument panel with two MFD The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 16 135 T3H/P3H 18.101.01 E Technical Data Enhanced rope down device The enhanced rope down device provides the capability to release the ropes attached to the external rope down device beam, using a switch panel in the cockpit area or a hand controller connected to the rear end of the center console. The beam is provided with an electrical release instead of the mechanic release lever. The control panel in the cockpit or the hand controller in the cabin will release all ropes (LH and RH) at the same time, using dual action switches to increase the safety. The release of the ropes from the cockpit may allow performing missions without need for an operator in the cabin, increasing the available payload. Enhanced Reality System (ERS) The ERS greatly enhances the images provided by an electro-optical system (EOS) by blending them with data layers or synthetic pictures. The ERS also incorporates a high performance video management system which has the ability to connect multiple video sources and to distribute those in the desired video standard, resolution and aspect ratio. Additionally up-to four full HD video tracks can be recorded in parallel. Additional options provide communication capabilities by supporting LAN applications, voice communication or server access based on VPN connections over LTE/4G network. Customer specific data formats can be used for secured data transmission. Figure 1.15: Cockpit control panel (left) and hand controller (right) 135 T3H/P3H 18.101.01 E 17 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data Figure 1.16: Example of ERS data overlay on real time camera imagery Figure 1.17: Example of screen split with ERS data overlay on real time camera and on satellite picture 18 135 T3H/P3H 18.101.01 E Blank The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 135 T3H/P3H 18.101.01 E 19 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 2 General Characteristics 2.1 Cockpit and Cabin Layouts 2.2 Weight 2.3 Power Ratings Engine Ratings (Uninstalled)1 The H135 can be equipped with either two Pratt & Whitney Canada PW206B3 or two Safran Helicopter Engines ARRIUS 2B2plus turboshaft engines. Values are per engine manufacturer specification. Pratt & Whitney Canada PW206B3 turboshaft engines Seats & equipment as option Aerial Work 1 pilot + copilot + up to 6 passengers Emergency Medical Services (EMS) 1 or 2 pilots + up to 2 stretcher patients + up to 3 HEMS crew Law Enforcement / Offshore Transportation 1 or 2 pilots + up to 6 passengers Passenger Transportation 1 or 2 pilots + up to 6 passengers kg lb • Empty weight, Baseline Aircraft Definition a 1,563 3,446 • Useful load, Baseline Aircraft Definition 1,417 3,124 • Pilot 85 187 • Payload and / or fuel 1,332 2,937 • Maximum Takeoff Weight (MTOW) 2,980 6,570 • Maximum Takeoff Weight (MTOW) with external load 2,980 6,570 • Maximum taxi weight 3,000 6,614 • Maximum cargo-sling load (single hook) 1,200 2,646 a. Margin ±1.5 %. 1. Thermodynamic values per engine, in standard atmosphere, at sea level All Engines Operative (AEO) kW shp • Takeoff-Power (TOP) 528 708 • Maximum Continuous Power (MCP) 457 613 One Engine Inoperative (OEI) kW shp • OEI 30 s 610 818 • OEI 2 min 582 780 • OEI MCP 528 708 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 20 135 T3H/P3H 18.101.01 E Technical Data Safran Helicopter Engines ARRIUS 2B2plus turboshaft engines Main Transmission Ratings 2.4 Fuel Capacities Note: Tolerance of fuel figures: ±2 %; fuel density used is 0.8 kg/liter. All Engines Operative (AEO) kW shp • Takeoff-Power (TOP) 492 660 • Maximum Continuous Power (MCP) 464 622 One Engine Inoperative (OEI) kW shp • OEI 30 s 606 812 • OEI 2 min 589 790 •OEI MCP 538 721 All Engines Operative (AEO) kW shp • Takeoff Power (TOP) 2 x 320 2 x 429 • Maximum Continuous Power (MCP) 2 x 283 2 x 380 One Engine Inoperative (OEI) kW shp • OEI 30 s 1 x 526 1 x 705 • OEI 2 min 1 x 513 1 x 687 • OEI MCP 1 x 368 1 x 493 Usable fuel liters US gal kg lb • Standard fuel tanks 700.5 185.1 560.4 1,235.4 • Internal long range fuel tank (option) 212.7 56.2 170.2 375.2 135 T3H/P3H 18.101.01 E 21 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 2.5 External Dimensions Figure 2.1: External dimensions The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 22 135 T3H/P3H 18.101.01 E Technical Data 2.6 Internal Dimensions 2.7 External Sound Levels Figure 2.2: Internal dimensions Floor area Volume Cabin & cargo compartment 4.35 m² 46.83 ft² 4.90 m³ 173.04 ft³ Cockpit (pilot side) 1.15 m² 12.38 ft² 1.00 m³ 35.31 ft³ Total (undivided) 5.50 m² 59.21 ft² 5.90 m³ 208.35 ft³ Flight phase Certified Sound Levels ICAO Annex 16, Chapter 8.4.1 & FAR 36 H, Stage 2 limits at 2,980 kg ICAO Annex 16, Chapter 8.4.2 & FAR 36 H, Stage 3 limits at 2,980 kg [EPNdB] [EPNdB] [EPNdB] Takeoff [EPNL] 86.1 94.8 91.8 Overflight [EPNL] 82.7 93.8 89.8 Approach [EPNL] 90.3 95.8 94.8 135 T3H/P3H 18.101.01 E 23 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 2.8 Touch Down Forces The touch down forces will be mainly transferred to a solid landing site via the four skid shoes on the landing gear. Figure 2.3: Touch down forces Skid shoe position FWD LH FWD RH AFT LH AFT RH Max. occurring force 17 kN 17 kN 24 kN 24 kN 24 135 T3H/P3H 18.101.01 E Blank The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 135 T3H/P3H 18.100.01 E 25 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 3 Baseline Aircraft Definition GENERAL • Energy absorbing fuselage • Tail boom with fixed horizontal stabilizer • Vertical fin with faired-in Fenestron • Upper deck with fittings for main gearbox, engines, hydraulic and cooling system • Cowlings for main transmission and engine • Skid-type landing gear with skid protectors, capable of taking ground-handling wheels • Long boarding steps, LH and RH • Maintenance built-in steps and grips • Exterior painting (single color) COCKPIT, CABIN AND CARGO COMPARTMENT • One-level cabin and cargo compartment floor with integrated rails • Glazed canopy • Two hinged cockpit doors with sliding window • Map case in pilot's door • Two wide passenger sliding doors • Two rear hinged clam-shell doors • Longitudinally adjustable energy absorbing pilot and copilot seats with head rest and 4-point safety belts with automatic locking system • Cabin boarding grips LH and RH • Interior paneling with integrated basic sound insulation • Flight controls for pilot side; fixed provisions of flight controls for copilot side • Covers for copilot collective lever & cyclic stick • Engine controls with manual engine back-up system at pilot's collective pitch lever • Single pilot instrument panel with glare shield and slant console • Ram-air and electrical ventilating system for cockpit and cabin • Helmet holder in the cockpit • Headset holder in the cabin • Portable fire extinguisher • Stowage net for first aid kit at the LH rear clam-shell door • Flash light (torch) for pilot side INSTRUMENTS • Flight Display Subsystem (FDS) composed of 2 smart multifunction displays (6 x 8 inch) providing the following functions: • Flight and Navigation Display (FND) format (incl. PFD, FLI, Master List, NAV, RPM, mast moment & fuel indication) • Vehicle Management System (VMS) format (incl. engine, gearbox, fuel, electrical system, RPM & clock indication) • Vehicle Management System (VMS) including: • 2 duplex Aircraft Management Computer (AMC) • Reference sensors: • 1 Attitude and Heading Reference System • Air Data sensor pilot side (electrically heated pitot tube and static port) • 1 Magnetometer • Standby instruments: • Integrated Electronic Standby Instrument (IESI) • Standby compass • Usage Monitoring System (UMS) - Helionix • Flight Data Continuous Recorder (FDCR) - Helionix • "One hundred feet" alert • Directional Gyro Free Steering Mode • Warning unit: • Engine fire warning with fuel emergency shut-off • Warning lights • Fire extinguishing system warning • Cockpit Control Panel (CCP) for FDS • Data Transfer Device (DTD) • Engine switch panel POWER PLANT • Two Pratt & Whitney Canada PW206B3 turbine engines or two Safran Helicopter Engines ARRIUS 2B2plus turbine engines These two engines are equipped with: • Fire detectors • Full Authority Digital Engine Control (FADEC) • Chip detectors with quick-disconnect plugs • Overspeed protection system • Cycle indication on FDS • Twin-engine OEI-training mode • Oil cooling and lubricating system with thermostatic valve • Crash resistant fuel system with a flexible bladder-type main tank and supply tank (split into two sections) • Automatically controlled variable rotor speed system • Fuel tank filler flap, lockable • Drain system •Fire walls TRANSMISSION SYSTEM • Flat-shaped main gearbox with two stages • Chip detector system with quick-disconnect plug (main gearbox) • Redundant oil cooling and lubrication system • Main gearbox attachment with Anti-Resonance Isolation System (ARIS) • Free wheel assemblies in the engine input drives • Tail rotor drive shaft • Tail rotor gearbox with splash lubrication and oil level sight gauge • Chip detector system with quick-disconnect plug (tail rotor gearbox) The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 26 135 T3H/P3H 18.100.01 E Technical Data ROTOR AND FLIGHT CONTROLS • Bearingless Main Rotor system (BMR) with improved dynamic characteristics, consisting of: • Rotor head / mast in one piece • Four fiber-reinforced composite main rotor blades with anti-erosion strips, control cuff, elastomeric lead-lag dampers and special blade tip painting • Main rotor control system with dual hydraulic boost system • Electrical trim system • Basic provisions for an easy integration of a track and balance system • Fenestron-type tail rotor with ten metal blades (asymmetric blade spacing) and stator • Tail rotor gearbox cover • Tail rotor control system with flexball cable and single hydraulic booster • Digital 3-axis SAS (Stability Augmentation System) • Mast moment system ELECTRICAL INSTALLATION • Two starter / generators (2x200 A, 28 VDC) • Nickel-Cadmium battery, (24 VDC, 27 Ah) • External power connector (STANAG 3302, LN9064, SAE AS 25018, SAE AS 35061) • Power distribution system: • Two primary busbars • Two shedding busbars • Two essential busbars • Two high load busbars (80 A) - for optional equipment only • Two high power busbars (200 A) • Battery bus • One utility receptacle in LH side of cargo compartment (28 VDC, 10 A) • Lighting: • Anti-collision warning light (red flashing), LED • Fixed, nose-mounted landing light • Three position lights (red, green, white), LED • Adjustable instrument lighting • One utility light in the cockpit • 5 spot-lights in the cabin • One light in cargo compartment RH side • Radio: • Two radio master switches GROUND HANDLING KITa • Two ground-handling wheels • Basic aircraft covers (short term) • Main rotor blade tie-down lash bags • Oil drain kit • Fuel tank drain device • Keys for cockpit doors, cabin doors, baggage compartment doors and tank flap (one-key system) • Battery key • Lifting points • Maintenance Ground Station (MGS) software • Airbus Helicopters Data Loader (AHDL) • Flight Data Continuous Recorder (FDCR) converter • Fleet keeper ® applicationb • Flight Planner application c a. Weight not included in the standard helicopter empty weight. b. Licence for one year and one helicopter included. c. Two licenses for one year and one helicopter included. Availability date to be confirmed. DOCUMENTATION (in English) • One Flight Manual ab (on paper) • One Pilots Checklist c (on paper) • One Master Minimum Equipment List (MMEL) a online via T.I.P.I. • One Logbook (on paper, CD-ROM on demand) • One Historical Record (on paper, CD-ROM on demand) • Technical Documentation a incl. AMM, SDS, WDM, IPC, MSM, CECG, SRM online via Keycopter® portal • Service Bulletin Catalogue (SB) online via T.I.P.I. • List of Applicable Publications (LOAP) a online via Keycopter portal • One Avionics Manual d (for avionics installed by Airbus) (on CD-ROM) • One ECMM c (Electronic Component Maintenance Manuals) for vendor manuals • One Engine Documentation e (format depends on engine manufacturer), furnished by supplier, including: • Maintenance Manual • Illustrated Parts Catalogue a. Revision service included as long as the aircraft is operational b. One Flight Manual included in the standard helicopter empty weight c. Revision service for 3 years d. Customized documentation e. Revision service for 3 years for Safran HE, 2 years for PWC 135 T3H/P3H 18.101.01 E 27 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 4 Mission Configurations Airbus offers the following mission configurations for specific H135 missions. The created mission configurations should be regarded as a first proposal for customers to evaluate the suitability of the H135 for their operational fields. The shown mission configurations comprise a list of Baseline Aircraft and Mission Package which can be complemented by additional equipment from the Further Available Equipment of the respective mission configuration. The General Available Equipment (chapter 5.1) shows all available optional items for all mission configurations. The following mission configurations are available: • Emergency Medical Services (EMS) • Law Enforcement • Offshore Transportation • Aerial Work Please note that some mission configurations include equipment requested by EASA-OPS. They do not cover oxygen equipment and the entire equipment required for extended over water or offshore operations. The operator shall contact his national authority for the approval of the planned aircraft mission configuration. General rules for adding options to the mission configurations The following rules must be considered when adding options from the respective Further Available Equipment to the mission configurations: • Only options from the respective Further Available Equipment list may be added to the mission configuration. Mixing options of different Further Available Equipment lists could lead to product incompatibilities. • Detachable parts require always the relevant fixed provisions. • Simultaneous installation of Interior Layout options from Further Available Equipment together with options of the mission configuration may not always be possible. Please contact an Airbus helicopter sales representative for further information. Performance calculation All data used for mission performance calculations in this document are for information purpose only and Airbus takes no responsibility for the correctness of this information as far as the applicability to the receiving party's individual case is concerned. The present use of the named data shall not be construed as expressly or impliedly granting the receiving party any rights nor be deemed to constitute any kind of obligation or commitment of Airbus. Further individual configurations General Available Equipment can be added by considering the rules provided in chapter 5.1. The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 28 135 T3H/P3H 18.101.01 E Technical Data 4.1 Emergency Medical Services (EMS) Mission The H135 is the most successful EMS helicopter on the market, with approximately 50% market share in the light twin helicopter segment worldwide and 25% of the entire EMS fleet worldwide. The H135 is designed to land almost anywhere and offers best-in-class outside visibility, Night Vision Goggle (NVG) friendly cockpit and cabin, compact overall external dimensions, high set main rotor, Fenestron, rugged skid landing gear, and the lowest external sound levels. Solutions for all primary mission configurations including, Helicopter Emergency Medical Service (HEMS) or mountain rescue and conversion to secondary missions, such as Helicopter Intensive CAre Medical Service (HICAMS), are possible due to the modular and flexible solution concept. Loading and unloading of patients and equipment, with rotors turning, can be carried out safely, quickly and easily from either side of the cabin or the rear. The extra-large sliding doors and the clam-shell doors can all be operated by one hand. During winching operations, patients can easily be transferred into the hovering helicopter. The H135 and medical equipment installations are designed to the stringent EMS standard EN13718. The EMS configuration is available with ergonomic solutions provided by AAT or Bucher Leichtbau. EMS interiors include state-of-the-art medical devices and other typical accessories for EMS missions and are designed to provide the best treatment for the patient. The newly designed EMS floor in combination with the adapted Bucher Leichtbau EMS kit provides considerable weight savings while optimizing cabin arrangement and patient access. Additional options required for customizing the mission configuration to the operators specific needs and requirements are detailed in the sections Further Available Equipment or General Available Equipment (chapter 5.1). Specific aircraft equipment including additional flight safety devices or specialized EMS equipment, for example, twin stretcher disaster management kits, Search And Rescue (SAR) equipment or incubators are available on request. Figure 4.1: EMS configuration - external view 135 T3H/P3H 18.101.01 E 29 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 4.1.1 Mission Parameter 4.1.2 EMS Configuration Baseline Aircraft Mission Equipment • Flight Rules Single / Dual Pilot IFR Night •Cat. A Yes • Instrumentation Glass Cockpit • NVG friendly Yes • EASA OPS Yes a a. Please refer to chapter 5.4 Figure 4.2: EMS configuration - cabin layout Qty Document Reference Commercial Reference Description kg lb Baseline Aircraft 1 00-10048-A E0000-001-00 H135 Baseline Aircraft 135 T3H/P3H 18.100.01 E 1563.0 3445.8 1 00-10048-A E0000-003-01 Safran Helicopter Engines ARRIUS 2B2plus turbine engines (2 engines) 0.0 0.0 1 00-10048-A E0000-003-02 Pratt & Whitney Canada PW206B3 turbine engines (2 engines) 0.0 0.0 Subtotal Weight: 1,563.0 3,445.8 1.5 % Weight margin: 23.4 51.7 Subtotal Weight (incl. margin): 1,586.4 3,497.5 Qty Document Reference Commercial Reference Description kg lb Mandatory Equipment General Equipment 1 05-03018-B E2561-000-00 First aid kita 1.2 2.6 1 05-22030-B E2621-000-00 Engine fire extinguishing system 4.0 8.8 1 05-22031-A E7924-000-00 Fuzz burners for engines 1.0 2.2 1 05-22032-B E7111-000-00 Engine cowling heat protection 1.8 4.0 1 05-23009-B E7165-000-00 Engine compressor wash kit 2.0 4.4 1 05-30004-C E3310-001-00 Flashlight for copilot side 0.3 0.7 1 05-32014-A E3042-000-00 Windshield wiper system 4.9 10.8 1 05-33007-B E3113-000-00 Center console 1.4 3.1 1 05-34012-B E2570-000-00 Avionics compartment 4.6 10.1 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 30 135 T3H/P3H 18.101.01 E Technical Data 1 05-37030-B E6700-000-20 Copilot flight controls, detachable parts 6.1 13.4 1 05-38025-B E3111-000-00 Instrument panel extension on copilot side 1.5 3.3 1 05-39021-A E2513-001-00 Map case in copilot door 0.4 0.9 1 05-39022-A E2514-000-00 Map cases on instrument panel glare shield 0.6 1.3 1 05-39023-A E3315-102-00 Illuminated chart holder, pilot 0.9 2.0 1 05-41013-B E2142-200-00 Bleed air heating system with additional air outlets in cargo compartment 6.8 15.0 1 05-61026-A E2433-100-00 Battery (40 Ah, 24 VDC) ULM (Saft) instead of standard battery 8.3 18.3 1 05-71003-A E6350-000-00 Rotor brake system 5.7 12.6 Specific Mission Equipment 1 06-45082-B E3343-200-10 Search & landing light, fixed provisions 1.2 2.6 1 06-45082-B E3343-200-20 Search & landing light, detachable parts 3.3 7.3 1 06-67081-A E2562-000-00 Emergency Locator Transmitter (ELT) 1.7 3.7 1 06-71010-B E1150-200-00 Standard cockpit, cabin and cargo compartment - NVG 0.0 0.0 1 06-71011-B E2521-500-10 Separation curtain for cockpit / cabin, fixed provisions 0.3 0.7 1 06-71011-B E2521-500-20 Separation curtain for cockpit / cabin, detachable parts 0.3 0.7 Interior Layout 1 07-15035-A E2512-102-00 Height adjustable pilot seat instead of standard pilot seat 1.3 2.9 07-15035-A E2512-101-00 Height adjustable copilot seat instead of standard copilot seat 1.3 2.9 Avionics 1 08-00447-B E2300-120-00 Avionics Package DP IFR GC GTN 750 0.0 0.0 1 08-16164-C E2341-000-00 Digital Audio Control System (DACS), incl. ACP53 (Cobham), pilot + copilot 5.8 12.8 1 08-22083-A E3451-000-00 Transponder GTX 335R (Garmin)b 2.4 5.3 1 08-25519-A E3455-000-00 Distance Measuring Equipment (DME) DME-4000 (Rockwell Collins) 2.6 5.7 1 08-26063-A E3431-000-00 Marker beacon receiver MKR3300-1 (Becker) 1.2 2.6 1 08-43077-C E3463-001-00 GPS/NAV/COM GTN 750 (Garmin), copilotc 6.9 15.2 1 08-43077-C E3463-002-00 GPS/NAV/COM GTN 750 (Garmin), pilotc 8.2 18.1 1 08-65054-A E3161-001-00 Flight Display Subsystem (FDS), copilot 5.5 12.1 1 08-99005-B E0000-151-00 Avionics Package DP IFR GTN Series interconnection / wiring 23.5 51.8 1 08-21036-A E3441-000-00 Radar altimeter KRA 405B (Honeywell) 3.3 7.3 1 08-35068-B E3446-000-00 Helicopter Terrain Awareness and Warning System (H-TAWS) - Helionixd 0.1 0.2 1 08-35069-B E3446-100-00 Synthetic Vision System (SVS) - Helionixd 0.0 0.0 1 08-53010-B E2213-000-00 Additional Attitude and Heading Reference System (AHRS) & magnetometer 5.4 11.9 1 08-54004-B E3411-000-00 Copilot pitot static system 2.9 6.4 1 08-72007-A E2212-100-00 4-axis Automatic Flight Control System (AFCS) 17.6 38.8 1 08-81045-A E3139-000-00 Lightweight Aircraft Recording System (LARS) Alerts Vision 1000 (Appareo) 0.7 1.5 Qty Document Reference Commercial Reference Description kg lb 135 T3H/P3H 18.101.01 E 31 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data Reference Equipment General Equipment 1 05-02084-A E1111-100-00 Enhanced exterior painting instead of standard painting 2.0 4.4 1 05-31148-A E5633-001-00 Window in clam-shell door LH 0.3 0.7 Specific Mission Equipment 1 06-11044-A E3274-000-10 Settling protectors, fixed provisions 0.1 0.2 1 06-11044-A E3274-000-20 Settling protectors, detachable parts 8.1 17.9 1 06-66025-B E3342-400-00 Boarding step illuminations 0.3 0.7 Interior Layout 1 07-40036-B E2515-100-00 Washable floor covering for cockpit 3.6 7.9 1 07-50082-B E5231-000-00 One-hand latching system for clam-shell doors 1.4 3.1 1 07-50083-A E5231-100-00 Extended opening fasteners for clam-shell doors 0.1 0.2 Interior Layout - AAT EMS Solution 1 07-70081-B AAT-35100-002-2 EMS Package (AAT - STC), 2018e 0.0 0.0 1 07-73095-A AAT-35110-007-2 Medical floor (AAT - STC)f 44.2 97.4 1 07-74109-A AAT-35120-007-2 Stretcher "Rescue" foldable for Medical Floor (AAT-STC), LH 13.0 28.7 1 07-73086-A AAT-35130-006-2 Medical seat slidable (AAT - STC), fwd RH 11.5 25.4 1 07-73087-A AAT-35130-016-2 Medical seat slidable & swiveling (AAT - STC), aft RH 16.7 36.8 1 07-76060-A AAT-35140-005-2 Medical cabinet with 3 drawers (AAT - STC), front center 11.9 26.2 1 07-72084-A AAT-35160-005-2 Oxygen station 3x3.0 l, 200 bar (AAT - STC), front RH 6.0 13.2 1 07-75182-B AAT-35140-101-2 Medical equipment carrier – NVG (AAT - STC), aft LH 29.4 64.8 3 07-75183-A AAT-35150-003-2 Infusion hook (AAT - STC), mid LH 0.3 0.7 1 07-77023-A AAT-35160-013-2 Medical power distribution unit for Corpuls C3 (AAT - STC) 1.2 2.6 1 07-75184-A AAT-35150-302-2 Retainer for monitor & defibrillator Corpuls C3 (AAT - STC) 1.7 3.7 1 07-75185-A AAT-35150-105-2 Retainer for monitor & patient box Corpuls C3 (AAT - STC) 1.3 2.9 1 07-75186-A AAT-35150-208-2 Retainer for respirator Medumat Transport (AAT - STC) 2.3 5.1 1 07-75187-A AAT-35150-203-2 Retainer for infusion system Perfusor Space (AAT - STC) 0.7 1.5 1 07-75188-A AAT-35150-310-2 Retainer for suction pump LCSU 4 (AAT - STC) 0.7 1.5 1 07-75189-A AAT-35150-002-2 Accessories (AAT - STC) 1.4 3.1 1 07-79043-A AAT-35190-100-3 Installation, certifcation & documentation (AAT - STC) 0.0 0.0 3 07-72060-A AAT-00170-910-3 Oxygen cylinder (3.0 l) aluminum (Luxfer) 9.6 21.2 1 07-72093-A AAT-00170-105-3 Monitor & defibrillator Corpuls C3 Slim (GS) 6.3 13.9 1 07-72045-A AAT-00170-404-3 Respirator Medumat Transport (Weinmann) 5.8 12.8 2 07-72044-A AAT-00170-602-3 Infusion system Perfusor Space (Braun) 2.8 6.2 1 07-72043-B AAT-00170-508-3 Suction pump LCSU 4 (Laerdal) 1.7 3.7 1 07-79008-B AAT-00170-820-3 Emergency backpack incl. DIN13232-N contents WM9062 (Weinmann) 11.1 24.5 1 07-79020-B AAT-00170-821-3 Respiration rescue bag WM9090 incl. contents (Weinmann) 13.7 30.2 1 07-79023-A AAT-00170-904-3 Cervical collar set Perfit ACE & Mini Perfit ACE (Ambu) 0.5 1.1 1 07-79007-C AAT-00170-901-3 Vacuum mattress (Tyromont) 4.3 9.5 1 05-67040-B E2460-000-00 Power sockets (2x 28 VDC, 20 A) at center console 1.1 2.4 Qty Document Reference Commercial Reference Description kg lb The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 32 135 T3H/P3H 18.101.01 E Technical Data Interior Layout - BUL EMS Solution 1 07-70083-B BUL-35100-001-2 EMS Package (Bucher Leichtbau - STC). 2018e 0.0 0.0 1 07-74108-A BUL-35120-101-2 Foldable stretcher 12-2 (BUL - STC)g 12.0 26.5 1 07-73091-B BUL-35130-102-2 Medical seat slideable & swiveling (BUL - STC)h 17.2 37.9 1 07-73092-A BUL-35130-101-2 Medical seat stationary (BUL - STC)h 11.0 24.3 1 07-76067-A BUL-35140-104-2 Modular center cabinet, (BUL - STC) 6.4 14.1 1 07-76067-A BUL-35140-106-2 Module drawers (BUL - STC) 3.5 7.7 1 07-76063-A BUL-35150-105-2 Center cabinet (BUL - STC), adapter 1.6 3.5 1 07-76064-A BUL-35140-203-1 Side cabinet (BUL - STC), RH 0.2 0.4 1 07-76065-A BUL-35140-202-1 Rear door stowage unit (BUL - STC) 3.3 7.3 1 07-76066-A BUL-35140-201-2 Stowage box (BUL - STC) 6.5 14.3 1 07-72111-A BUL-35160-301-1 Oxygen cylinder rack (BUL - STC), window RH 3.9 8.6 3 07-72111-A BUL-35160-302-2 Oxygen supply hoses (BUL - STC) 3.6 7.9 1 07-75205-A BUL-35150-100-1 Medical wall (BUL - STC) 17.9 39.5 1 07-75197-A BUL-35150-103-1 Roof rails (BUL - STC), LH 0.9 2.0 1 07-75198-A BUL-35150-107-1 Suction unit (BUL - STC), window LH, fixed provisions 1.4 3.1 1 07-75199-A BUL-35150-106-1 Infusion hook (BUL - STC), mid LH 0.2 0.4 1 07-77037-A BUL-35160-101-1 Electrical system (BUL - STC) 14.1 31.1 1 07-75200-A BUL-35150-201-2 Retainer for monitor & defibrillator Corpuls C3 (BUL - STC)i 2.6 5.7 1 07-75201-A BUL-35150-202-2 Retainer for respirator Oxylog 3000plus (BUL - STC) 1.0 2.2 1 07-75202-A BUL-35150-101-2 Retainer mounting single adapter (BUL - STC) 0.7 1.5 1 07-75206-A BUL-00170-001-2 Retainer for Braun Perfusor Space (BUL - STC) 1.9 4.2 1 07-72118-A BUL-00170-406-3 Connection cable for Braun Perfusor Space (BUL - STC) 0.2 0.4 1 07-79045-A BUL-35190-001-3 Installation, certification & documentation (BUL - STC) 0.0 0.0 3 07-72112-A BUL-00170-701-3 Oxygen cylinder 2.7 l, 300 bar 7.5 16.5 1 07-72113-A BUL-00170-101-3 Monitor & defibrillator Corpuls C3 (GS) 5.3 11.7 1 07-72114-A BUL-00170-202-3 Respirator Oxylog 3000plus (Draeger) 5.8 12.8 2 07-72119-A BUL-00170-402-3 Perfusor Space (Braun) 2.8 6.2 1 07-72116-A BUL-00170-301-3 Portable suction unit OB1000 (Boscarol) 3.3 7.3 1 07-79046-A BUL-00170-601-3 Emergency backpack incl. DIN13232-N contents WM9050 (Weinmann) 2.8 6.2 1 07-79047-B BUL-00170-603-3 Respiration backpack incl. contents WM9080 (Weinmann) 5.0 11.0 1 07-79048-A BUL-00170-901-3 Vacuum mattress (Tyromont)j 4.3 9.5 1 07-79049-B BUL-00170-902-3 Rescue bag (Tyromont) 3.7 8.2 1 07-40041-A E2531-100-00 EMS floor instead of standard cabin floork 18.4 40.6 1 07-77034-A E8522-200-00 Main switch in overhead console for Bucher Leichtbau installation 0.1 0.2 Qty Document Reference Commercial Reference Description kg lb 135 T3H/P3H 18.101.01 E 33 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data Avionics 1 08-12102-A E2317-000-00 Tactical radio, fixed provisions, incl. antenna, power supply & intercom interfacel 2.0 4.4 1 08-16164-C E2341-005-00 Digital Audio Control System (DACS), ACP53 (Cobham), pax 1.2 2.6 4 08-18078-A E2315-100-00 Headset H 10-76 (David Clark), low impedance 2.4 5.3 2 08-18079-B E2342-000-00 Headset adapter cable crew GLENAIR / U92 0.2 0.4 2 08-18079-B E2342-005-00 Headset adapter cable pax GLENAIR / U92 0.4 0.9 Weight breakdown with AAT EMS Solution Subtotal Weight: 368.3 812.0 3.0 % Weight margin: 11.0 24.3 Subtotal Weight (incl. margin): 379.3 836.2 Total Weight: 1,965.8 4,333.8 Weight breakdown with Bucher Leichtbau EMS Solution Subtotal Weight: 338.2 745.6 3.0 % Weight margin: 10.1 22.4 Subtotal Weight (incl. margin): 348.3 768.0 Total Weight: 1,934.8 4,265.5 a. Customization of first aid kit content necessary to comply with EASA OPS requirements. Medications may have to be removed for Export. b. incl. ADS-B out. c. SBAS RNP approach local service availability verification through your Airbus helicopter sales representative on request. d. The database update service is provided under a dedicated service contract. Please contact your Airbus helicopter sales representative for further information. e. This STC is only EASA certified. Prices and leadtimes for national certifications are available on request. f. Incl. recessed stretcher locking system g. incl. retainers h. incl. seat stop assy i. sea rail mount j. incl. pump k. Primary Stretcher LH side. l. Onboard HF/tact. radio transm. can influence radio nav. systems (MKR, VOR, ILS, ADF) and com systems (VHF/other tact. radio). Depending on NAA cert. requirements, such systems must either be turned off during IFR approaches/departures or deactivated. Qty Document Reference Commercial Reference Description kg lb The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 34 135 T3H/P3H 18.101.01 E Technical Data 4.1.3 Further Available Equipment 05 General Equipment Qty Document Reference Commercial Reference Description kg lb General Equipment 1 05-02087-B E6211-100-00 Main rotor blade erosion protection paint 0.1 0.2 1 05-12011-B E2516-000-00 Boarding grips for cockpit 0.1 0.2 1 05-21036-C E8541-000-10 Cable cutter system, fixed provisions 3.1 6.8 1 05-21036-C E8541-000-20 Cable cutter system, detachable parts 8.1 17.9 1 05-25037-C E7162-000-00 Inlet Barrier Filter (IBF) system 19.1 42.1 1 05-31146-A E2511-000-00 Tinted sun shades for cockpit windshield roof section 1.8 4.0 1 05-31148-A E5633-002-00 Window in clam-shell door RH 0.3 0.7 1 05-37031-B E6700-101-00 Pedal cover for copilot flight controls -4.8 -10.6 1 05-39023-A E3315-101-00 Illuminated chart holder, copilot 0.8 1.8 1 05-42051-B E2111-000-00 Air conditioning system (ACS) 49.7 109.6 1 05-85018-A E2841-000-00 Fuel management system (fuel flow meters) 1.0 2.2 Specific Mission Equipment 1 06-12028-A E3210-100-00 Medium height landing gear instead of standard landing gear 5.2 11.5 1 06-21042-D E8510-001-10 External hoist LH, fixed provisions 13.1 28.9 1 06-21042-D E8510-001-20 External hoist LH, detachable parts 2.6 5.7 1 06-21042-D E8510-100-31 External hoist (without hook and damper kit), 90 m, vendor partsa 62.4 137.6 1 06-21042-D E8510-300-30 External hoist, small hook damper kit & D-LOK hook, vendor parts 2.3 5.1 1 06-26028-A E8512-002-10 Cargo hook mirrors RH, fixed provisions 0.5 1.1 1 06-26028-A E8512-002-20 Cargo hook mirrors RH, detachable parts 4.0 8.8 1 06-26028-A E8512-002-90 Cover for cargo hook mirrors RH 0.4 0.9 1 06-26029-A E3181-000-10 External multi-purpose camera on tail boom, fixed provisions 2.0 4.4 1 06-26029-A E3181-000-20 External multi-purpose camera on tail boom, detachable parts 0.6 1.3 1 06-26029-A E3181-100-10 External rear-view camera on landing gear, fixed provisions 1.5 3.3 1 06-26029-A E3181-100-20 External rear-view camera on landing gear, detachable parts 1.4 3.1 1 06-27049-D E8511-500-10 Dual cargo hook system, fixed provisions 6.6 14.6 1 06-27049-D E8511-500-20 Dual cargo hook system, detachable parts 29.6 65.3 1 06-27049-D E8511-600-10 Cargo hook system, remote control grip, fixed provisions 0.3 0.7 1 06-27049-D E8511-600-20 Cargo hook system, remote control grip, detachable parts 0.9 2.0 1 06-27049-D E8511-700-00 Dual cargo hook system, copilot electrical release 0.3 0.7 1 06-27049-D E8511-800-10 Cargo hook weighing system, fixed provisions 0.2 0.4 1 06-27049-D E8511-800-20 Cargo hook weighing system, detachable parts 0.2 0.4 1 06-45082-B E3343-300-10 2nd Search & landing light, fixed provisions 1.7 3.7 1 06-45082-B E3343-300-20 2nd Search & landing light, detachable parts 3.1 6.8 1 06-45082-B E3343-900-00 Search & landing light, IR mode 0.1 0.2 1 06-46012-A E3344-100-00 White strobe lights 1.3 2.9 1 06-61036-B E3215-100-10 Emergency floats, fixed provisionsb 9.5 20.9 1 06-61036-B E3215-000-20 Emergency floats, detachable parts 63.4 139.8 1 06-65016-B E2625-100-00 2nd portable fire extinguisher 2.8 6.2 135 T3H/P3H 18.101.01 E 35 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data Interior Layout 1 07-50084-A E5213-101-00 Sliding door fastener, max. position, LH 0.3 0.7 1 07-50088-B E8513-000-00 Abrasion protection at sliding doors 0.2 0.4 1 07-50089-A E5211-200-00 Securing device for complete opening of cockpit doors 1.1 2.4 1 07-60049-B E2513-005-00 Map cases in sliding doors 1.4 3.1 1 07-77033-A E8521-200-00 Main switch in overhead console for Aerolite installation 0.1 0.2 Avionics 1 08-15568-B E2315-400-00 LTE phone, fixed provisions, incl. antenna, power supply (28 VDC) & intercom interfacec 1.0 2.2 1 08-15569-C E2316-000-00 Wireless intercom system PNG (Axnes), basic systemd 2.6 5.7 1 08-15569-C E2316-100-00 Wireless intercom system PNG (Axnes), cockpit control panel CP50 0.5 1.1 1 08-15569-C E2316-200-00 Wireless intercom system PNG (Axnes), mobile transceiver MP50e 1.0 2.2 1 08-15570-B E2315-000-00 Iridium satellite transceiver GSR 56 (Garmin) 4.3 9.5 1 08-35070-B E2327-000-10 Traffic Advisory System TAS620A (Avidyne), fixed provisions 3.0 6.6 1 08-35070-B E2327-000-20 Traffic Advisory System TAS620A (Avidyne), detachable parts 3.4 7.5 1 08-43078-A E3464-000-00 Wireless connectivity Connext (Garmin) 0.3 0.7 1 08-46070-A E3169-000-00 Moving map - Helionixf 0.0 0.0 1 08-81046-C E3132-000-10 Cockpit Voice and Flight Data Recorder (CVFDR), fixed provisions 3.3 7.3 1 08-81046-C E3132-000-20 Cockpit Voice and Flight Data Recorder (CVFDR), detachable partsg 4.7 10.4 1 08-83048-A E3171-200-00 Professional Ground Station (PGS) Vision Systemh GSE GSE 1 08-83049-A E3171-100-00 Helicopter Flight Data Monitoring (HFDM)i GSE GSE a. Hoist operation & maintenance training included. Details are provided in the respective documentation. b. incl. auto-activation. c. Without integration and EASA certification of LTE phone. d. Mobile transceiver and cockpit control panel not included. e. Mobile transceiver with defined frequency range between 440 - 450 MHz and in yellow color. f. The database update service is provided under a dedicated service contract. Please contact your Airbus helicopter sales representative for further information. g. Ground station not included. h. Recommended 1 per customer base if CVFDR is selected. i. Instead of PGS Vision System Qty Document Reference Commercial Reference Description kg lb The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 36 135 T3H/P3H 18.101.01 E Technical Data 4.1.4 EMS Mission Performance Weight breakdown (with payload and fuel) Mission profile • Takeoff Cat. A VTOL at SL (maximum 2,950 kg) • Climb flight AEO-MCP from SL to 5,000 ft with VY, mean 65 KIAS • Level flight in 5,000 ft with VBR (PW206B3: 132 KTAS; Arrius 2B2plus: 136 KTAS) • Descent from 5,000 ft to SL with R/D of 1,000 fpm, mean 80 KIAS • Landing Cat. A VTOL at SL Payload range diagram Relevant flight data kg lb Weight basis for Payload Range Diagram Equipped empty weight EMS Configuration (incl. engine oil, unusable fuel and weight margin) 1,780 3,924 2 pilots (2 x 85 kg) 170 375 Payload Bucher Leichtbau medical equipment (incl. stretcher; cabinet; 2 seats; oxygen; medical devices) 155 342 2 medical crew (2 x 85 kg) 170 375 1 patient on stretcher (1 x 85 kg) 85 187 Fuel Reserve fuel: 30 min in 1,500 ft with 130 KTAS 96 212 Trip fuel 464 1,023 Mission takeoff weight 2,920 6,437 Figure 4.3: EMS configuration - payload range diagram PW206B3 engines Arrius 2B2 plus engines • Calculated maximum range (without payload, with trip fuel) 316 NM (585 km) 318 NM (589 km) • Corresponding flight time (incl. 2x climb / descent phases)2 h 26 min 2 h 23 min 135 T3H/P3H 18.101.01 E 37 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 4.2 Law Enforcement Mission Whatever the Law Enforcement mission requires, the H135 offers the proven solution. The best-in- class payload, long range, high endurance, low vibration levels, ergonomic interior design and lowest sound levels combine to create an environment that minimizes crew fatigue in the demanding Law Enforcement environment. With compact overall dimensions, high set main rotor, Fenestron and rugged landing gear the H135 is able to transport law enforcement officers safely in and out of confined areas while the spacious, unobstructed cabin offers multi mission flexibility and the visibility required for special operations. Mission flexibility is expanded with an extensive range of off-the-shelf solutions. The Law Enforcement configuration offers a FLIR Systems Star Safire 380HDc Electro Optical System (EOS) solution based on a modular concept, which is a forward mounted side-by-side installation coordinated with the searchlight to ensure the maximum observation capabilities and unobstructed view. The cockpit and cabin as well as the mission equipment are Night Vision Goggle (NVG) friendly. Observation, command and control, aerial support and protection of sensitive sites are the major tasks of this mission configuration. Further Available Equipment allows for fast mission changes, for example from anti-terrorist operations, to deploying armed teams or SWAT units or disaster management, where carrying a stretcher beside the operator workstation is possible. Additional options required for customizing the mission configuration to the operators specific needs and requirements are detailed in the sections Further Available Equipment or General Available Equipment (chapter 5.1). Specific aircraft equipment including additional flight safety devices or specialized alternate state-of-the-art Electro Optical Systems (EOS), recording capabilities, Enhanced Reality System (ERS), secured data link and networking solutions, additional High Definition (HD) mission displays, various tactical radios and stowage equipment are available on request. Figure 4.4: Law Enforcement configuration - external view The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 38 135 T3H/P3H 18.101.01 E Technical Data 4.2.1 Mission Parameter 4.2.2 Law Enforcement Configuration Baseline Aircraft Mission Equipment • Flight Rules Single / Dual Pilot IFR Night •Cat. A Yes • Instrumentation Glass Cockpit • NVG friendly Yes • EASA OPS Yes a a. Please refer to chapter 5.4 Figure 4.5: Law Enforcement configuration - cabin layout Qty Document Reference Commercial Reference Description kg lb Baseline Aircraft 1 00-10048-A E0000-001-00 H135 Baseline Aircraft 135 T3H/P3H 18.100.01 E 1563.0 3445.8 1 00-10048-A E0000-003-01 Safran Helicopter Engines ARRIUS 2B2plus turbine engines (2 engines) 0.0 0.0 1 00-10048-A E0000-003-02 Pratt & Whitney Canada PW206B3 turbine engines (2 engines) 0.0 0.0 Subtotal Weight: 1,563.0 3,445.8 1.5 % Weight margin: 23.4 51.7 Subtotal Weight (incl. margin): 1,586.4 3,497.5 Qty Document Reference Commercial Reference Description kg lb Mandatory Equipment General Equipment 1 05-03018-B E2561-000-00 First aid kita 1.2 2.6 1 05-22030-B E2621-000-00 Engine fire extinguishing system 4.0 8.8 1 05-22031-A E7924-000-00 Fuzz burners for engines 1.0 2.2 1 05-22032-B E7111-000-00 Engine cowling heat protection 1.8 4.0 1 05-23009-B E7165-000-00 Engine compressor wash kit 2.0 4.4 1 05-30004-C E3310-001-00 Flashlight for copilot side 0.3 0.7 1 05-32014-A E3042-000-00 Windshield wiper system 4.9 10.8 1 05-33007-B E3113-000-00 Center console 1.4 3.1 1 05-34012-B E2570-000-00 Avionics compartment 4.6 10.1 135 T3H/P3H 18.101.01 E 39 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 1 05-37030-B E6700-000-20 Copilot flight controls, detachable parts 6.1 13.4 1 05-38025-B E3111-000-00 Instrument panel extension on copilot side 1.5 3.3 1 05-39021-A E2513-001-00 Map case in copilot door 0.4 0.9 1 05-39022-A E2514-000-00 Map cases on instrument panel glare shield 0.6 1.3 1 05-39023-A E3315-102-00 Illuminated chart holder, pilot 0.9 2.0 1 05-41013-B E2142-200-00 Bleed air heating system with additional air outlets in cargo compartment 6.8 15.0 1 05-61026-A E2433-100-00 Battery (40 Ah, 24 VDC) ULM (Saft) instead of standard battery 8.3 18.3 1 05-71003-B E6350-000-00 Rotor brake system 5.7 12.6 Specific Mission Equipment 1 06-45082-B E3343-200-10 Search & landing light, fixed provisions 1.2 2.6 1 06-45082-B E3343-200-20 Search & landing light, detachable parts 3.3 7.3 1 06-67081-A E2562-000-00 Emergency Locator Transmitter (ELT) 1.7 3.7 1 06-71010-B E1150-200-00 Standard cockpit, cabin and cargo compartment - NVG 0.0 0.0 1 06-71011-B E2521-500-10 Separation curtain for cockpit / cabin, fixed provisions 0.3 0.7 1 06-71011-B E2521-500-20 Separation curtain for cockpit / cabin, detachable parts 0.3 0.7 Interior Layout 1 07-15035-A E2512-102-00 Height adjustable pilot seat instead of standard pilot seat 1.3 2.9 1 07-15035-A E2512-101-00 Height adjustable copilot seat instead of standard copilot seat 1.3 2.9 Avionics 1 08-00447-B E2300-120-00 Avionics Package DP IFR GC GTN 750 0.0 0.0 1 08-16164-C E2341-000-00 Digital Audio Control System (DACS), incl. ACP53 (Cobham), pilot + copilot 5.8 12.8 1 08-22083-A E3451-000-00 Transponder GTX 335R (Garmin)b 2.4 5.3 1 08-25519-A E3455-000-00 Distance Measuring Equipment (DME) DME-4000 (Rockwell Collins) 2.6 5.7 1 08-26063-A E3431-000-00 Marker beacon receiver MKR3300-1 (Becker) 1.2 2.6 1 08-43077-C E3463-001-00 GPS/NAV/COM GTN 750 (Garmin), copilotc 6.9 15.2 1 08-43077-C E3463-002-00 GPS/NAV/COM GTN 750 (Garmin), pilotc 8.2 18.1 1 08-65054-A E3161-001-00 Flight Display Subsystem (FDS), copilot 5.5 12.1 1 08-99005-B E0000-151-00 Avionics Package DP IFR GTN Series interconnection / wiring 23.5 51.8 1 08-21036-A E3441-000-00 Radar altimeter KRA 405B (Honeywell) 3.3 7.3 1 08-35068-B E3446-000-00 Helicopter Terrain Awareness and Warning System (H-TAWS) - Helionixd 0.1 0.2 1 08-35069-B E3446-100-00 Synthetic Vision System (SVS) - Helionixd 0.0 0.0 1 08-53010-B E2213-000-00 Additional Attitude and Heading Reference System (AHRS) & magnetometer 5.4 11.9 1 08-54004-B E3411-000-00 Copilot pitot static system 2.9 6.4 1 08-72007-A E2212-100-00 4-axis Automatic Flight Control System (AFCS) 17.6 38.8 1 08-81045-A E3139-000-00 Lightweight Aircraft Recording System (LARS) Alerts Vision 1000 (Appareo) 0.7 1.5 Reference Equipment General Equipment 1 05-02084-A E1111-100-00 Enhanced exterior painting instead of standard painting 2.0 4.4 1 05-31147-A E5632-005-00 Sliding windows in sliding doors 1.2 2.6 1 05-36035-A E8532-001-00 Multifunction step LH instead of standard boarding step 3.9 8.6 1 05-36035-A E8532-002-00 Multifunction step RH instead of standard boarding step 3.9 8.6 Qty Document Reference Commercial Reference Description kg lb The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 40 135 T3H/P3H 18.101.01 E Technical Data 1 05-85018-A E2841-000-00 Fuel management system (fuel flow meters) 1.0 2.2 Specific Mission Equipment 1 06-12028-A E3210-100-00 Medium height landing gear instead of standard landing gear 5.2 11.5 1 06-24027-B E8534-001-10 External rope-down device, LH, fixed provisions 7.5 16.5 1 06-24027-B E8534-002-10 External rope-down device, RH, fixed provisions 7.5 16.5 1 06-31029-B E8531-000-10 External loudspeaker system with siren, fixed provisions 5.9 13.0 1 06-31029-B E8531-000-20 External loudspeaker system with siren, detachable parts 4.8 10.6 1 06-45082-B E3343-900-00 Search & landing light, IR mode 0.1 0.2 1 06-45083-B E3346-000-10 Searchlight A800 (Trakka) basic LH, fixed provisions 4.4 9.7 1 06-45083-B E3346-000-20 Searchlight A800 (Trakka) basic LH, detachable parts 23.1 50.9 1 06-45083-B E3346-000-30 Searchlight A800 (Trakka), vendor parts 18.2 40.1 1 06-45083-B E3346-100-00 Searchlight A800 (Trakka), IR filters 0.0 0.0 1 06-45083-B E3346-200-00 Searchlight A800 (Trakka), IR laser pointer 0.1 0.2 Specific Mission Equipment - EOS Star Safire 380HDc Solution 1 06-50021-A E8532-272-00 EOS Star Safire 380HDc Packagee 0.0 0.0 1 06-51231-C E8532-200-11 EOS, RH step, fixed provisions 8.7 19.2 1 06-51231-C E8532-200-21 EOS, RH step, detachable parts 7.7 17.0 1 06-51231-C E8532-200-90 EOS, safety circuit for laser 0.7 1.5 1 06-51234-A E8532-272-32 EOS, Star Safire 380HDc, basic system (MWIR, 1280) 28.0 61.7 1 06-51234-A E8532-270-82 EOS, Star Safire series, geo reference system with integrated IMU/GPS 0.0 0.0 1 06-51234-A E8532-271-71 EOS, Star Safire series, universal hand controller 1.1 2.4 1 06-51234-A E8532-271-52 EOS, Star Safire series, compact laser range finder 0.0 0.0 1 06-51234-A E8532-271-61 EOS, Star Safire series, video autotracker 0.0 0.0 1 06-51234-A E8532-271-63 EOS, Star Safire series, digital image blendinge 0.0 0.0 1 06-51234-A E8532-271-91 EOS, Star Safire series, purge kit GSE GSE 1 06-52003-B E8532-261-21 Operator workstation PD DZUS, basic 9.7 21.4 1 06-52003-B E8532-261-28 Operator workstation PD DZUS, monitor, provisions 2.9 6.4 1 06-52003-B E8532-261-26 Operator workstation PD DZUS, EOS control, holder 0.2 0.4 1 06-52003-B E8532-261-30 Operator workstation PD DZUS, table for monitor installation 8.3 18.3 1 06-52003-B E8532-261-33 Operator workstation PD DZUS, keyboard, provisions 0.4 0.9 1 06-52003-B E8532-261-41 Operator workstation PD DZUS, stowage case lateral 0.3 0.7 1 06-52003-B E8532-261-42 Operator workstation PD DZUS, searchlight control holder 0.2 0.4 1 06-52003-B E3168-200-01 Keyboard - NVG 0.9 2.0 1 06-52003-B E8532-261-63 22" Full-HD Monitor 7.6 16.8 1 06-54004-A E8532-261-34 Video recorder, provisions, operator workstation compatible 0.1 0.2 1 06-54004-A E8532-261-62 Video recorder 0.6 1.3 1 06-53005-B E8532-254-11 Downlink (BMS), operator workstation installation, fixed provisions 1.7 3.7 1 06-53005-B E8532-254-26 Downlink (BMS), operator workstation installation, detachable parts 1.2 2.6 1 06-53005-B E8532-252-56 Downlink (BMS), transmission system (Helicoder4), vendor parts 3.6 7.9 Qty Document Reference Commercial Reference Description kg lb 135 T3H/P3H 18.101.01 E 41 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data Interior Layout 1 07-27036-B E2522-405-00 Operator seat with armrests and 4-point restraint system 12.7 28.0 1 07-40036-B E2515-000-00 Washable floor covering for cockpit, cabin & cargo compartment 9.2 20.3 1 07-50084-A E5213-101-00 Sliding door fastener, max. position, LH 0.3 0.7 1 07-50084-A E5213-102-00 Sliding door fastener, max. position, RH 0.3 0.7 1 07-50086-B E5212-100-00 Spoiler position for cockpit doors 1.0 2.2 Avionics 1 08-12101-A E2312-000-00 Tactical radio VHF-FM NPX138N (Cobham)f 2.5 5.5 1 08-16164-C E2341-005-00 Digital Audio Control System (DACS), ACP53 (Cobham), pax 1.2 2.6 3 08-18078-A E2315-100-00 Headset H 10-76 (David Clark), low impedance 1.8 4.0 2 08-18079-B E2342-000-00 Headset adapter cable crew GLENAIR / U92 0.2 0.4 1 08-18079-B E2342-005-00 Headset adapter cable pax GLENAIR / U92 0.2 0.4 1 08-46068-A E3168-000-00 Moving map EuroNav VII - RN7 (EuroAvionics), basic versiong 6.3 13.9 Subtotal Weight: 355.4 783.5 3.0 % Weight margin: 10.7 23.6 Subtotal Weight (incl. margin): 366.1 807.1 Total Weight: 1,952.5 4,304.5 a. Customization of first aid kit content necessary to comply with EASA OPS requirements. Medications may have to be removed for Export. b. incl. ADS-B out. c. SBAS RNP approach local service availability verification through your Airbus helicopter sales representative on request. d. The database update service is provided under a dedicated service contract. Please contact your Airbus helicopter sales representative for further information. e. Export clearance needs to be clarified by Airbus Helicopters sales representative. f. Onboard HF/tact. radio transm. can influence radio nav. systems (MKR, VOR, ILS, ADF) and com systems (VHF/other tact. radio). Depending on NAA cert. requirements, such systems must either be turned off during IFR approaches/departures or deactivated. g. incl. 512 GB flashdisk and Global Map Package Qty Document Reference Commercial Reference Description kg lb The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 42 135 T3H/P3H 18.101.01 E Technical Data 4.2.3 Further Available Equipment Qty Document Reference Commercial Reference Description kg lb General Equipment 1 05-02087-B E6211-100-00 Main rotor blade erosion protection paint 0.1 0.2 1 05-21036-C E8541-000-10 Cable cutter system, fixed provisions 3.1 6.8 1 05-21036-C E8541-000-20 Cable cutter system, detachable parts 8.1 17.9 1 05-25037-C E7162-000-00 Inlet Barrier Filter (IBF) system 19.1 42.1 1 05-26020-A E1241-100-00 Corrosion protection for high corrosive environment 3.2 7.1 1 05-31146-A E2511-000-00 Tinted sun shades for cockpit windshield roof section 1.8 4.0 1 05-31151-A E2521-600-10 Curtains for cabin windows - NVG, fix provisions 0.2 0.4 1 05-31151-A E2521-600-20 Curtains for cabin windows - NVG, detachable parts 1.3 2.9 1 05-37031-B E6700-101-00 Pedal cover for copilot flight controls -4.8 -10.6 1 05-39023-A E3315-101-00 Illuminated chart holder, copilot 0.8 1.8 1 05-42051-B E2111-000-00 Air conditioning system (ACS) 49.7 109.6 1 05-93017-A E1021-000-10 Lashing points for wind speeds up to 40 kts, fixed provisions 1.6 3.5 1 05-93017-A E1021-000-20 Lashing points for wind speeds up to 40 kts, detachable parts 0.8 1.8 Specific Mission Equipment 1 06-11044-A E3274-000-10 Settling protectors, fixed provisions 0.1 0.2 1 06-11044-A E3274-000-20 Settling protectors, detachable parts 8.1 17.9 1 06-24027-B E8534-200-10 Enhanced external rope down device (ECMS - STC), LH & RH, electrical fixed provisionsa 3.5 7.7 1 06-24027-B E8534-300-00 Enhanced external rope down device (ECMS - STC), control panela 0.5 1.1 1 06-24027-B E8534-400-00 Enhanced external rope down device (ECMS - STC), hand controllera 2.0 4.4 1 06-24027-B E8534-601-20 Enhanced external rope down device for 2/1 persons (ECMS - STC), LH retractable, detachable partsa 19.3 42.5 1 06-24027-B E8534-602-20 Enhanced external rope down device for 2/1 persons (ECMS - STC), RH retractable, detachable partsa 19.3 42.5 1 06-26029-A E3181-000-10 External multi-purpose camera on tail boom, fixed provisions 2.0 4.4 1 06-26029-A E3181-000-20 External multi-purpose camera on tail boom, detachable parts 0.6 1.3 1 06-26029-A E3181-100-10 External rear-view camera on landing gear, fixed provisions 1.5 3.3 1 06-26029-A E3181-100-20 External rear-view camera on landing gear, detachable parts 1.4 3.1 1 06-45082-B E3343-300-10 2nd Search & landing light, fixed provisions 1.7 3.7 1 06-45082-B E3343-300-20 2nd Search & landing light, detachable parts 3.1 6.8 1 06-46012-A E3344-100-00 White strobe lights 1.3 2.9 1 06-65016-B E2625-100-00 2nd portable fire extinguisher 2.8 6.2 Interior Layout 1 07-40037-C E2532-000-00 Sealed cabin floor 0.3 0.7 1 07-50082-B E5231-000-00 One-hand latching system for clam-shell doors 1.4 3.1 1 07-50089-A E5211-200-00 Securing device for complete opening of cockpit doors 1.1 2.4 1 07-60049-B E2513-005-00 Map cases in sliding doors 1.4 3.1 1 07-60050-B E2550-000-00 Variable tie-down net 3.3 7.3 1 07-74099-B AAT-35120-006-2 Foldable stretcher Rescue (AAT - STC)a 18.7 41.2 135 T3H/P3H 18.101.01 E 43 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data Avionics 1 08-15568-B E2315-400-00 LTE phone, fixed provisions, incl. antenna, power supply (28 VDC) & intercom interfaceb 1.0 2.2 1 08-15569-C E2316-000-00 Wireless intercom system PNG (Axnes), basic systemc 2.6 5.7 1 08-15569-C E2316-100-00 Wireless intercom system PNG (Axnes), cockpit control panel CP50 0.5 1.1 1 08-15569-C E2316-200-00 Wireless intercom system PNG (Axnes), mobile transceiver MP50d 1.0 2.2 1 08-24038-A E3452-100-00 Automatic Direction Finder (ADF), control unit CDF552 (Cobham) 1.0 2.2 1 08-24038-A E3452-000-00 Automatic Direction Finder (ADF), receiver DF-431B (Cobham) 11.0 24.3 1 08-35070-B E2327-000-10 Traffic Advisory System TAS620A (Avidyne), fixed provisions 3.0 6.6 1 08-35070-B E2327-000-20 Traffic Advisory System TAS620A (Avidyne), detachable parts 3.4 7.5 1 08-43078-A E3464-000-00 Wireless connectivity Connext (Garmin) 0.3 0.7 1 08-46068-B E3168-100-00 Moving map EuroNav 7 - RN7 (EuroAvionics), Iridium satcom module 1.4 3.1 1 08-46068-B E3168-400-00 Moving map EuroNav 7 - RN7 (EuroAvionics), GSM / UMTS module 0.5 1.1 1 08-46068-B E3168-300-00 Moving map EuroNav 7 - RN7 (EuroAvionics), FLARM module 0.6 1.3 1 08-81046-C E3132-000-10 Cockpit Voice and Flight Data Recorder (CVFDR), fixed provisions 3.3 7.3 1 08-81046-C E3132-000-20 Cockpit Voice and Flight Data Recorder (CVFDR), detachable partse 4.7 10.4 1 08-83048-A E3171-200-00 Professional Ground Station (PGS) Vision Systemf GSE GSE 1 08-83049-A E3171-100-00 Helicopter Flight Data Monitoring (HFDM)g GSE GSE a. This STC is only EASA certified. Prices and leadtimes for national certifications are available on request. b. Without integration and EASA certification of LTE phone. c. Mobile transceiver and cockpit control panel not included. d. Mobile transceiver with defined frequency range between 440 - 450 MHz and in yellow color. e. Ground station not included. f. Recommended 1 per customer base if CVFDR is selected. g. Instead of PGS Vision System Qty Document Reference Commercial Reference Description kg lb The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 44 135 T3H/P3H 18.101.01 E Technical Data 4.2.4 Law Enforcement Mission Performance Weight breakdown (with payload and fuel) Mission profile • Takeoff at SL (maximum 2,980 kg) • Climb flight AEO-MCP from SL to 5,000 ft with VY, mean 65 KIAS • Level flight in 5,000 ft with VBR (PW206B3: 133 KTAS; Arrius 2B2plus: 132 KTAS) • Descent from 5,000 ft to SL with R/D of 1,000 fpm, mean 80 KIAS • Landing at SL Payload range diagram Relevant flight data kg lb Weight basis for Payload Range Diagram Equipped empty weight Law Enforcement configuration (incl. engine oil, unusable fuel and weight margin) 1,952 4,303 2 pilots (2 x 85 kg) 170 375 Payload EOS operator (1 x 85 kg) 85 187 Available remaining payload 213 470 Fuel Reserve fuel: 20 min in 1,500 ft with VY, mean 65 KIAS 50 110 Trip fuel 510 1,124 Mission takeoff weight (MTOW) 2,980 6,570 Figure 4.6: Law Enforcement configuration - payload range diagram PW206B3 engines Arrius 2B2 plus engines Calculated maximum range (without payload, with trip fuel) 320 NM (593 km) 326 NM (604 km) Corresponding flight time (incl. 2x climb / descent phases) 2 h 27 min 2 h 31 min 135 T3H/P3H 18.101.01 E 45 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 4.3 Offshore Transportation Mission Certified for offshore operations up to sea state 6 the high maneuverable H135 combines integrated system safety, efficient twin engine performance (AEO) and outstanding single engine performance (OEI) with, panoramic visibility, extended range, and a spacious cabin to make the helicopter perfectly suited for the most demanding off-shore conditions. Flight crew workload and fatigue is considerably reduced by the integrated state-of-the-art avionics, including the most advanced 4-axis autopilot and Human Machine Interface (HMI) which enables the flight crew to safely dedicate more attention to the mission and changing environments of off shore operations while remaining informed of vital aircraft information. The H135 offers exceptionally high aircraft availability with maintainability included in the aircraft design and with operator inspired flexible maintenance schemes. The H135's proven technology enables pilots to perform safe and efficient flights in the most harsh and remote offshore conditions. The Offshore Transportation configuration is equipped with a 5-passenger interior solution and special equipment for offshore operations including emergency floats, additional corrosion protection and Helicopter Emergency Egress Lighting System (HEELS). Further available items from the respective Further Available Equipment or General Available Equipment (chapter 5.1) can be added to customize the mission configuration. Additional items required for EASA OPS or specific operator requirements including External Life Raft System (ELRS) which meets the EASA OPS requirements for hostile environment, fully integrated Health & Usage Monitoring System (HUMS), Automatic Identification System (AIS), personal locator beacons, and other equipment are available on request. Figure 4.7: Offshore Transportation configuration - external view The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 46 135 T3H/P3H 18.101.01 E Technical Data 4.3.1 Mission Parameter 4.3.2 Offshore Transportation Configuration Baseline Aircraft Mission Equipment • Flight Rules Single / Dual Pilot IFR Night •Cat. A Yes • Instrumentation Glass Cockpit • NVG friendly Yes • EASA OPS No Figure 4.8: Offshore Transportation configuration - cabin layout Qty Document Reference Commercial Reference Description kg lb Baseline Aircraft 1 00-10048-A E0000-001-00 H135 Baseline Aircraft 135 T3H/P3H 18.100.01 E 1,563.0 3,445.8 1 00-10048-A E0000-003-01 Safran Helicopter Engine ARRIUS 2B2plus turbine engines (2 engines) 0.0 0.0 1 00-10048-A E0000-003-02 Pratt & Whitney Canada PW206B3 turbine engines (2 engines) 0.0 0.0 Subtotal Weight: 1,563.0 3,445.8 1.5 % Weight margin: 23.4 51.7 Subtotal Weight (incl. margin): 1,586.4 3,497.5 Qty Document Reference Commercial Reference Description kg lb Mandatory Equipment General Equipment 1 05-03018-B E2561-000-00 First aid kita 1.2 2.6 1 05-22030-B E2621-000-00 Engine fire extinguishing system 4.0 8.8 1 05-22031-A E7924-000-00 Fuzz burners for engines 1.0 2.2 1 05-22032-B E7111-000-00 Engine cowling heat protection 1.8 4.0 1 05-23009-B E7165-000-00 Engine compressor wash kit 2.0 4.4 1 05-30004-C E3310-001-00 Flashlight for copilot side 0.3 0.7 1 05-32014-A E3042-000-00 Windshield wiper system 4.9 10.8 1 05-33007-B E3113-000-00 Center console 1.4 3.1 1 05-34012-B E2570-000-00 Avionics compartment 4.6 10.1 1 05-37030-B E6700-000-20 Copilot flight controls, detachable parts 6.1 13.4 135 T3H/P3H 18.101.01 E 47 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 1 05-38025-B E3111-000-00 Instrument panel extension on copilot side 1.5 3.3 1 05-39021-A E2513-001-00 Map case in copilot door 0.4 0.9 1 05-39022-A E2514-000-00 Map cases on instrument panel glare shield 0.6 1.3 1 05-39023-A E3315-102-00 Illuminated chart holder, pilot 0.9 2.0 1 05-41013-B E2142-100-00 Bleed air heating system 6.4 14.1 1 05-61026-A E2433-100-00 Battery (40 Ah, 24 VDC) ULM (Saft) instead of standard battery 8.3 18.3 1 05-71003-B E6350-000-00 Rotor brake system 5.7 12.6 Specific Mission Equipment 1 06-45082-B E3343-200-10 Search & landing light, fixed provisions 1.2 2.6 1 06-45082-B E3343-200-20 Search & landing light, detachable parts 3.3 7.3 1 06-67080-A E2562-400-00 Automatic Deployable Emergency Locator Transmitter (ADELT) 10.3 22.7 1 06-71010-B E1150-200-00 Standard cockpit, cabin and cargo compartment - NVG 0.0 0.0 1 06-71011-B E2521-500-10 Separation curtain for cockpit / cabin, fixed provisions 0.3 0.7 1 06-71011-B E2521-500-20 Separation curtain for cockpit / cabin, detachable parts 0.3 0.7 Interior Layout 1 07-15035-A E2512-102-00 Height adjustable pilot seat instead of standard pilot seat 1.3 2.9 1 07-15035-A E2512-101-00 Height adjustable copilot seat instead of standard copilot seat 1.3 2.9 Avionics 1 08-00447-B E2300-120-00 Avionics Package DP IFR GC GTN 750 0.0 0.0 1 08-16164-C E2341-000-00 Digital Audio Control System (DACS), incl. ACP53 (Cobham), pilot + copilot 5.8 12.8 1 08-22083-A E3451-000-00 Transponder GTX 335R (Garmin)b 2.4 5.3 1 08-25519-A E3455-000-00 Distance Measuring Equipment (DME) DME-4000 (Rockwell Collins) 2.6 5.7 1 08-26063-A E3431-000-00 Marker beacon receiver MKR3300-1 (Becker) 1.2 2.6 1 08-43077-C E3463-001-00 GPS/NAV/COM GTN 750 (Garmin), copilotc 6.9 15.2 1 08-43077-C E3463-002-00 GPS/NAV/COM GTN 750 (Garmin), pilotc 8.2 18.1 1 08-65054-A E3161-001-00 Flight Display Subsystem (FDS), copilot 5.5 12.1 1 08-99005-B E0000-151-00 Avionics Package DP IFR GTN Series interconnection / wiring 23.5 51.8 1 08-21036-A E3441-000-00 Radar altimeter KRA 405B (Honeywell) 3.3 7.3 1 08-35068-B E3446-000-00 Helicopter Terrain Awareness and Warning System (H-TAWS) - Helionixd 0.1 0.2 1 08-35069-B E3446-100-00 Synthetic Vision System (SVS) - Helionixd 0.0 0.0 1 08-53010-B E2213-000-00 Additional Attitude and Heading Reference System (AHRS) & magnetometer 5.4 11.9 1 08-54004-B E3411-000-00 Copilot pitot static system 2.9 6.4 1 08-72007-A E2212-100-00 4-axis Automatic Flight Control System (AFCS) 17.6 38.8 1 08-81045-A E3139-000-00 Lightweight Aircraft Recording System (LARS) Alerts Vision 1000 (Appareo) 0.7 1.5 Qty Document Reference Commercial Reference Description kg lb The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 48 135 T3H/P3H 18.101.01 E Technical Data Reference Equipment General Equipment 1 05-02084-A E1111-100-00 Enhanced exterior painting instead of standard painting 2.0 4.4 1 05-26020-A E1241-100-00 Corrosion protection for high corrosive environment 3.2 7.1 Specific Mission Equipment 1 06-61036-B E3215-100-10 Emergency floats, fixed provisionse 9.5 20.9 1 06-61036-B E3215-000-20 Emergency floats, detachable parts 63.4 139.8 1 06-66024-B E3353-000-00 Emergency lights incl. boarding step illuminations 3.5 7.7 1 06-66026-A E3353-100-00 Helicopter Emergency Egress Lighting System (HEELS) 5.8 12.8 Interior Layout 1 07-27035-C E2522-307-00 Passenger seating, 1 seat with 4-point restraint system (rear row, facing in flight direction, LH) 11.3 24.9 1 07-27035-C E2522-308-00 Passenger seating, 1 seat with 4-point restraint system (rear row, facing in flight direction, RH) 11.3 24.9 1 07-27035-C E2522-006-00 Passenger seating, 3 seats with 4-point restraint system (front row, facing against flight direction) 38.1 84.0 1 07-40036-B E2515-000-00 Washable floor covering for cockpit, cabin & cargo compartment 9.2 20.3 1 07-40037-C E2532-000-00 Sealed cabin floor 0.3 0.7 1 07-50085-B E5212-000-00 Jettisonable cockpit doors 0.9 2.0 1 07-60050-B E2550-000-00 Variable tie-down net 3.3 7.3 Avionics 1 08-12101-A E2312-000-00 Tactical radio VHF-FM NPX138N (Cobham)f 2.5 5.5 7 08-18078-A E2315-100-00 Headset H 10-76 (David Clark), low impedance 4.2 9.3 2 08-18079-B E2342-000-00 Headset adapter cable crew GLENAIR / U92 0.2 0.4 5 08-18079-B E2342-005-00 Headset adapter cable pax GLENAIR / U92 1.0 2.2 1 08-81046-C E3132-000-10 Cockpit Voice and Flight Data Recorder (CVFDR), fixed provisions 3.3 7.3 1 08-81046-C E3132-000-20 Cockpit Voice and Flight Data Recorder (CVFDR), detachable partsg 4.7 10.4 1 08-83048-A E3171-200-00 Professional Ground Station (PGS) Vision Systemh GSE GSE Subtotal Weight: 332.9 733.9 1.5 % Weight margin: 10.0 22.0 Subtotal Weight (incl. margin): 342.9 755.9 Total Weight: 1,929.3 4,253.4 a. Customization of first aid kit content necessary to comply with EASA OPS requirements. Medications may have to be removed for Export. b. incl. ADS-B out c. SBAS RNP approach local service availability verification through your Airbus helicopter sales representative on request. d. The database update service is provided under a dedicated service contract. Please contact your Airbus helicopter sales representative for further information. e. incl. auto-activation. f. Onboard HF/tact. radio transm. can influence radio nav. systems (MKR, VOR, ILS, ADF) and com systems (VHF/other tact. radio). Depending on NAA cert. requirements, such systems must either be turned off during IFR approaches/departures or deactivated. g. Ground station not included. h. Recommended 1 per customer base if CVFDR is selected. Qty Document Reference Commercial Reference Description kg lb 135 T3H/P3H 18.101.01 E 49 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 4.3.3 Further Available Equipment Qty Document Reference Commercial Reference Description kg lb General Equipment 1 05-02085-B E6211-000-00 High visibility paint for main rotor blades 0.0 0.0 1 05-02086-A E1111-900-00 Surface protective coating (Airglaze) 0.5 1.1 1 05-02087-B E6211-100-00 Main rotor blade erosion protection paint 0.1 0.2 1 05-12010-A E7110-300-00 Maintenance step on cabin roof, LH 0.7 1.5 1 05-12011-B E2516-000-00 Boarding grips for cockpit 0.1 0.2 1 05-25037-C E7162-000-00 Inlet Barrier Filter (IBF) system 19.1 42.1 1 05-31146-A E2511-000-00 Tinted sun shades for cockpit windshield roof section 1.8 4.0 1 05-31147-A E5632-005-00 Sliding windows in sliding doors 1.2 2.6 1 05-31152-A E5632-100-00 Ram air deflectors for sliding windows in cockpit doors 0.6 1.3 1 05-31152-A E5632-105-00 Ram air deflectors for sliding windows in sliding doors 0.4 0.9 1 05-37031-B E6700-101-00 Pedal cover for copilot flight controls -4.8 -10.6 1 05-39023-A E3315-101-00 Illuminated chart holder, copilot 0.8 1.8 1 05-42051-B E2111-000-00 Air conditioning system (ACS) 49.7 109.6 1 05-81054-A E2818-000-10 Internal long range fuel tank system, fixed provisions 2.0 4.4 1 05-81054-A E2818-000-20 Internal long range fuel tank system, detachable parts 35.9 79.1 1 05-85018-A E2841-000-00 Fuel management system (fuel flow meters) 1.0 2.2 1 05-92019-A E6611-000-00 Main rotor blade folding, basic kit 1.5 3.3 1 05-92019-A E6611-100-10 Main rotor blade folding, fixed provisions for ground handling kit 0.8 1.8 1 05-92019-A E6611-100-90 Main rotor blade folding, ground handling kit GSE GSE 1 05-93017-A E1021-000-10 Lashing points for wind speeds up to 40 kts, fixed provisions 1.6 3.5 1 05-93017-A E1021-000-20 Lashing points for wind speeds up to 40 kts, detachable parts 0.8 1.8 1 05-95005-A E1320-200-00 Long term cover kit for helicopter GSE GSE Specific Mission Equipment 1 06-21042-D E8510-001-10 External hoist LH, fixed provisions 13.1 28.9 1 06-21042-D E8510-001-20 External hoist LH, detachable parts 2.6 5.7 1 06-21042-D E8510-002-10 External hoist RH, fixed provisions 13.8 30.4 1 06-21042-D E8510-002-20 External hoist RH, detachable parts 2.5 5.5 1 06-21042-D E8510-000-31 External hoist (without hook and damper kit), 50 m, vendor partsa 56.2 123.9 1 06-21042-D E8510-300-30 External hoist, small hook damper kit & D-LOK hook, vendor parts 2.3 5.1 1 06-26029-A E3181-000-10 External multi-purpose camera on tail boom, fixed provisions 2.0 4.4 1 06-26029-A E3181-000-20 External multi-purpose camera on tail boom, detachable parts 0.6 1.3 1 06-26029-A E3181-100-10 External rear-view camera on landing gear, fixed provisions 1.5 3.3 1 06-26029-A E3181-100-20 External rear-view camera on landing gear, detachable parts 1.4 3.1 1 06-46012-A E3344-100-00 White strobe lights 1.3 2.9 1 06-62034-A E2565-001-10 External Life Raft System (ELRS) LH, fixed provisions 0.8 1.8 1 06-62034-A E2565-001-20 External Life Raft System (ELRS) LH, detachable partsb 37.1 81.8 1 06-62034-A E2565-002-10 External Life Raft System (ELRS) RH, fixed provisions 0.8 1.8 1 06-62034-A E2565-002-20 External Life Raft System (ELRS) RH, detachable partsb 37.1 81.8 1 06-62034-A E2562-600-00 Survival emergency locator transmitter ELT(S) 0.9 2.0 1 06-65016-B E2625-100-00 2nd portable fire extinguisher 2.8 6.2 1 06-66027-B E3323-000-00 Illuminated signs "NO SMOKING / FASTEN SEAT BELT" 0.7 1.5 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 50 135 T3H/P3H 18.101.01 E Technical Data Interior Layout 1 07-50082-B E5231-000-00 One-hand latching system for clam-shell doors 1.4 3.1 1 07-50083-A E5231-100-00 Extended opening fasteners for clam-shell doors 0.1 0.2 1 07-50084-A E5213-101-00 Sliding door fastener, max. position, LH 0.3 0.7 1 07-50084-A E5213-102-00 Sliding door fastener, max. position, RH 0.3 0.7 1 07-50086-B E5212-100-00 Spoiler position for cockpit doors 1.0 2.2 1 07-60049-B E2513-005-00 Map cases in sliding doors 1.4 3.1 Avionics 1 08-12102-B E2317-000-00 Tactical radio, fixed provisions, incl. antenna, power supply & intercom interfacec 2.0 4.4 1 08-15568-B E2315-400-00 LTE phone, fixed provisions, incl. antenna, power supply (28 VDC) & intercom interfaced 1.0 2.2 1 08-15569-C E2316-000-00 Wireless intercom system PNG (Axnes), basic systeme 2.6 5.7 1 08-15569-C E2316-100-00 Wireless intercom system PNG (Axnes), cockpit control panel CP50 0.5 1.1 1 08-15569-C E2316-200-00 Wireless intercom system PNG (Axnes), mobile transceiver MP50f 1.0 2.2 1 08-15570-B E2315-000-00 Iridium satellite transceiver GSR 56 (Garmin) 4.3 9.5 1 08-16164-C E2341-005-00 Digital Audio Control System (DACS), ACP53 (Cobham), pax 1.2 2.6 1 08-35070-B E2327-000-10 Traffic Advisory System TAS620A (Avidyne), fixed provisions 3.0 6.6 1 08-35070-B E2327-000-20 Traffic Advisory System TAS620A (Avidyne), detachable parts 3.4 7.5 1 08-43078-A E3464-000-00 Wireless connectivity Connext (Garmin) 0.3 0.7 1 08-46070-A E3169-000-00 Moving map - Helionixg 0.0 0.0 1 08-83047-A E3171-000-10 Health Monitoring System (HMS), fixed provisions 3.1 6.8 1 08-83047-A E3171-000-20 Health Monitoring System (HMS), detachable parts 2.7 6.0 1 08-83049-A E3171-100-00 Helicopter Flight Data Monitoring (HFDM)h GSE GSE a. Hoist operation & maintenance training included. Details are provided in the respective documentation. b. Operator to equip ELT(S) meeting ICAO Annex 10 requirements to comply with EASA OPS. c. Onboard HF/tact. radio transm. can influence radio nav. systems (MKR, VOR, ILS, ADF) and com systems (VHF/other tact. radio). Depending on NAA cert. requirements, such systems must either be turned off during IFR approaches/departures or deactivated. d. Without integration and EASA certification of LTE phone. e. Mobile transceiver and cockpit control panel not included. f. Mobile transceiver with defined frequency range between 440 - 450 MHz and in yellow color. g. The database update service is provided under a dedicated service contract. Please contact your Airbus helicopter sales representative for further information. h. Instead of PGS Vision System Qty Document Reference Commercial Reference Description kg lb 135 T3H/P3H 18.101.01 E 51 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 4.3.4 Offshore Transportation Mission Performance Weight breakdown (with payload and fuel) Mission profile • Takeoff at SL (maximum 2,980 kg) • Climb flight AEO-MCP from SL to 5,000 ft with VY, mean 65 KIAS • Level flight in 5,000 ft with VBR (PW206B3: 136 KTAS; Arrius 2B2plus: 133 KTAS) • Descent from 5,000 ft to SL with R/D of 1,000 fpm, mean 80 KIAS & Landing Cat. A VTOL at SL • Takeoff Cat. A VTOL at SL (maximum 2,950 kg) • Climb flight, level flight, descent and landing as above Radius of action diagram Note: that the MTOW is limited by the Cat. A VTOL performance in case the outbound segment is too short to burn 30 kg fuel prior to Cat. A VTOL takeoff at the offshore helipad (Cat. A VTOL ISA +20°C: 2,950 kg). kg lb Weight basis for Payload Range Diagram Equipped empty weight Offshore Transport configuration (incl. engine oil, unusable fuel and weight margin) 1,929 4,253 2 pilots (2 x 85 kg) 170 375 Payload 5 passengers (5 x 95 kg) 475 1,047 Fuel Reserve fuel: 30 min in 1,500 ft with VY, mean 65 KIAS 76 168 Contingency fuel: 10% 30 66 Trip fuel 300 661 Mission takeoff weight (MTOW) 2,980 6,570 Figure 4.9: Offshore Transportation configuration - radius of action diagram PW206B3 engines Arrius 2B2 plus engines Calculated maximum radius of action (without payload, with trip fuel) 138 NM (256 km) 139 NM (257 km) Corresponding flight time (incl. 2x climb / descent phases) 2 h 17 min 2 h 21 min The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 52 135 T3H/P3H 18.101.01 E Technical Data 4.4 Aerial Work Mission With the best-in-class payload, long range, high endurance, low vibration levels and the lowest sound levels the H135 is also the best platform for various Aerial Work operations. The spacious, unobstructed cabin and cargo compartment including a flat floor with integrated seat rails, plus an extensive rage of off-the-shelf mission equipment, provides high mission flexibility and quick role change possibilities. The overall compact dimensions of the H135 with features including exceptional visibility, a high set main rotor, Fenestron, rugged landing gear, outstanding High and Hot twin and single engine performance combined with high reliability and low maintenance requirements prove that the H135 was designed for safe operation in remote and challenging conditions. The empty cabin and cargo compartment volume is 4.90 m3 and can be perfectly used to carry loads. Rear clam-shell and large sliding doors are designed for loading long or bulky freight. The floor loading is rated for 600 kg/m2 and cargo can be easily and safely secured with the adjustable tie-down rings mounted in the seat rails. Further available items from the respective Further Available Equipment or General Available Equipment (chapter 5.1) can be added to customize the mission configuration. Figure 4.10: Aerial Work configuration- external view 135 T3H/P3H 18.101.01 E 53 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 4.4.1 Mission Parameter 4.4.2 Aerial Work Configuration Baseline Aircraft Mission Equipment • Flight Rules Single Pilot IFR Night •Cat. A Yes • Instrumentation Glass Cockpit • NVG friendly Yes • EASA OPS Yes a a. Please refer to chapter 5.4 Figure 4.11: Aerial Work configuration - cabin layout Qty Document Reference Commercial Reference Description kg lb Baseline Aircraft 1 00-10048-A E0000-001-00 H135 Baseline Aircraft 135 T3H/P3H 18.100.01 E 1563.0 3445.8 1 00-10048-A E0000-003-01 Safran Helicopter Engine ARRIUS 2B2plus turbine engines (2 engines) 0.0 0.0 1 00-10048-A E0000-003-02 Pratt & Whitney Canada PW206B3 turbine engines (2 engines) 0.0 0.0 Subtotal Weight: 1,563.0 3,445.8 1.5 % Weight margin: 23.4 51.7 Subtotal Weight (incl. margin): 1,586.4 3,497.5 Qty Document Reference Commercial Reference Description kg lb Mandatory Equipment General Equipment 1 05-03018-B E2561-000-00 First aid kita 1.2 2.6 1 05-22030-B E2621-000-00 Engine fire extinguishing system 4.0 8.8 1 05-22031-A E7924-000-00 Fuzz burners for engines 1.0 2.2 1 05-22032-B E7111-000-00 Engine cowling heat protection 1.8 4.0 1 05-23009-B E7165-000-00 Engine compressor wash kit 2.0 4.4 1 05-32014-A E3042-000-00 Windshield wiper system 4.9 10.8 1 05-33007-B E3113-000-00 Center console 1.4 3.1 1 05-34012-B E2570-000-00 Avionics compartment 4.6 10.1 1 05-37030-B E6700-000-20 Copilot flight controls, detachable parts 6.1 13.4 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 54 135 T3H/P3H 18.101.01 E Technical Data 1 05-38025-B E3111-000-00 Instrument panel extension on copilot side 1.5 3.3 1 05-39022-A E2514-000-00 Map cases on instrument panel glare shield 0.6 1.3 1 05-39023-A E3315-102-00 Illuminated chart holder, pilot 0.9 2.0 1 05-41013-B E2142-100-00 Bleed air heating system 6.4 14.1 1 05-61026-A E2433-100-00 Battery (40 Ah, 24 VDC) ULM (Saft) instead of standard battery 8.3 18.3 1 05-71003-B E6350-000-00 Rotor brake system 5.7 12.6 Specific Mission Equipment 1 06-45082-B E3343-200-10 Search & landing light, fixed provisions 1.2 2.6 1 06-45082-B E3343-200-20 Search & landing light, detachable parts 3.3 7.3 1 06-67081-A E2562-000-00 Emergency Locator Transmitter (ELT) 1.7 3.7 1 06-71010-B E1150-200-00 Standard cockpit, cabin and cargo compartment - NVG 0.0 0.0 1 06-71011-B E2521-500-10 Separation curtain for cockpit / cabin, fixed provisions 0.3 0.7 1 06-71011-B E2521-500-20 Separation curtain for cockpit / cabin, detachable parts 0.3 0.7 Interior Layout 1 07-15035-A E2512-102-00 Height adjustable pilot seat instead of standard pilot seat 1.3 2.9 1 07-15035-A E2512-101-00 Height adjustable copilot seat instead of standard copilot seat 1.3 2.9 Avionics 1 08-00452-A E2300-122-00 Avionics Package SP IFR GC GTN 750 0.0 0.0 1 08-16164-C E2341-000-00 Digital Audio Control System (DACS), incl. ACP53 (Cobham), pilot + copilot 5.8 12.8 1 08-22083-A E3451-000-00 Transponder GTX 335R (Garmin)b 2.4 5.3 1 08-25519-A E3455-000-00 Distance Measuring Equipment (DME) DME-4000 (Rockwell Collins) 2.6 5.7 1 08-26063-A E3431-000-00 Marker beacon receiver MKR3300-1 (Becker) 1.2 2.6 1 08-43077-C E3463-001-00 GPS/NAV/COM GTN 750 (Garmin), copilotc 6.9 15.2 1 08-43077-C E3463-002-00 GPS/NAV/COM GTN 750 (Garmin), pilotc 8.2 18.1 1 08-99005-B E0000-152-00 Avionics Package SP IFR GTN Series interconnection / wiring 23.5 51.8 1 08-21036-A E3441-000-00 Radar altimeter KRA 405B (Honeywell) 3.3 7.3 1 08-35068-B E3446-000-00 Helicopter Terrain Awareness and Warning System (H-TAWS) - Helionixd 0.1 0.2 1 08-35069-B E3446-100-00 Synthetic Vision System (SVS) - Helionixd 0.0 0.0 1 08-53010-B E2213-000-00 Additional Attitude and Heading Reference System (AHRS) & magnetometer 5.4 11.9 1 08-54004-B E3411-000-00 Copilot pitot static system 2.9 6.4 1 08-72007-A E2212-100-00 4-axis Automatic Flight Control System (AFCS) 17.6 38.8 1 08-81045-A E3139-000-00 Lightweight Aircraft Recording System (LARS) Alerts Vision 1000 (Appareo) 0.7 1.5 Reference Equipment General Equipment 1 05-37031-B E6700-101-00 Pedal cover for copilot flight controls -4.8 -10.6 Specific Mission Equipment 1 06-12028-A E3210-100-00 Medium height landing gear instead of standard landing gear 5.2 11.5 1 06-26029-A E3181-000-10 External multi-purpose camera on tail boom, fixed provisions 2.0 4.4 1 06-26029-A E3181-000-20 External multi-purpose camera on tail boom, detachable parts 0.6 1.3 1 06-27049-D E8511-000-10 Single cargo hook system, fixed provisions 5.2 11.5 Interior Layout Qty Document Reference Commercial Reference Description kg lb 135 T3H/P3H 18.101.01 E 55 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 4.4.3 Further Available Equipment 1 07-40036-B E2515-000-00 Washable floor covering for cockpit, cabin & cargo compartment 9.2 20.3 Avionics 1 08-18078-A E2315-100-00 Headset H 10-76 (David Clark), low impedance 0.6 1.3 1 08-18079-B E2342-000-00 Headset adapter cable crew GLENAIR / U92 0.1 0.2 Subtotal Weight: 158.5 349.4 3.0 % Weight margin: 4.8 10.5 Subtotal Weight (incl. margin): 163.3 359.9 Total Weight: 1,749.7 3,857.4 a. Customization of first aid kit content necessary to comply with EASA OPS requirements. Medications may have to be removed for Export. b. incl. ADS-B out c. SBAS RNP approach local service availability verification through your Airbus helicopter sales representative on request. d. The database update service is provided under a dedicated service contract. Please contact your Airbus helicopter sales representative for further information. Qty Document Reference Commercial Reference Description kg lb Qty Document Reference Commercial Reference Description kg lb General Equipment 1 05-02084-A E1111-100-00 Enhanced exterior painting instead of standard painting 2.0 4.4 1 05-02085-B E6211-000-00 High visibility paint for main rotor blades 0.0 0.0 1 05-02086-A E1111-900-00 Surface protective coating (Airglaze) 0.5 1.1 1 05-02087-B E6211-100-00 Main rotor blade erosion protection paint 0.1 0.2 1 05-12010-A E7110-300-00 Maintenance step on cabin roof, LH 0.7 1.5 1 05-12011-B E2516-000-00 Boarding grips for cockpit 0.1 0.2 1 05-25037-C E7162-000-00 Inlet Barrier Filter (IBF) system 19.1 42.1 1 05-26020-A E1241-100-00 Corrosion protection for high corrosive environment 3.2 7.1 1 05-31146-A E2511-000-00 Tinted sun shades for cockpit windshield roof section 1.8 4.0 1 05-31147-A E5632-005-00 Sliding windows in sliding doors 1.2 2.6 1 05-31152-A E5632-100-00 Ram air deflectors for sliding windows in cockpit doors 0.6 1.3 1 05-31152-A E5632-105-00 Ram air deflectors for sliding windows in sliding doors 0.4 0.9 1 05-39023-A E3315-101-00 Illuminated chart holder, copilot 0.8 1.8 1 05-44014-B E2122-100-00 Ventilation enhancement for cockpit 1.0 2.2 1 05-81054-A E2818-000-10 Internal long range fuel tank system, fixed provisions 2.0 4.4 1 05-81054-A E2818-000-20 Internal long range fuel tank system, detachable parts 35.9 79.1 1 05-85018-A E2841-000-00 Fuel management system (fuel flow meters) 1.0 2.2 1 05-92019-A E6611-000-00 Main rotor blade folding, basic kit 1.5 3.3 1 05-92019-A E6611-100-10 Main rotor blade folding, fixed provisions for ground handling kit 0.8 1.8 1 05-92019-A E6611-100-90 Main rotor blade folding, ground handling kit GSE GSE 1 05-93017-A E1021-000-10 Lashing points for wind speeds up to 40 kts, fixed provisions 1.6 3.5 1 05-93017-A E1021-000-20 Lashing points for wind speeds up to 40 kts, detachable parts 0.8 1.8 1 05-95005-A E1320-200-00 Long term cover kit for helicopter GSE GSE The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 56 135 T3H/P3H 18.101.01 E Technical Data Specific Mission Equipment 1 06-21042-D E8510-001-10 External hoist LH, fixed provisions 13.1 28.9 1 06-21042-D E8510-001-20 External hoist LH, detachable parts 2.6 5.7 1 06-21042-D E8510-002-10 External hoist RH, fixed provisions 13.8 30.4 1 06-21042-D E8510-002-20 External hoist RH, detachable parts 2.5 5.5 1 06-21042-D E8510-100-31 External hoist (without hook and damper kit), 90 m, vendor partsa 62.4 137.6 1 06-21042-D E8510-300-30 External hoist, small hook damper kit & D-LOK hook, vendor parts 2.3 5.1 1 06-26028-A E8512-002-10 Cargo hook mirrors RH, fixed provisions 0.5 1.1 1 06-26028-A E8512-002-20 Cargo hook mirrors RH, detachable parts 4.0 8.8 1 06-26028-A E8512-002-90 Cover for cargo hook mirrors RH 0.4 0.9 1 06-26029-A E3181-100-10 External rear-view camera on landing gear, fixed provisions 1.5 3.3 1 06-26029-A E3181-100-20 External rear-view camera on landing gear, detachable parts 1.4 3.1 1 06-27049-D E8511-000-20 Single cargo hook system, detachable parts 25.9 57.1 1 06-27049-D E8511-600-10 Cargo hook system, remote control grip, fixed provisions 0.3 0.7 1 06-27049-D E8511-600-20 Cargo hook system, remote control grip, detachable parts 0.9 2.0 1 06-46012-A E3344-100-00 White strobe lights 1.3 2.9 1 06-61036-B E3215-100-10 Emergency floats, fixed provisionsb 9.5 20.9 1 06-61036-B E3215-000-20 Emergency floats, detachable parts 63.4 139.8 1 06-65016-B E2625-100-00 2nd portable fire extinguisher 2.8 6.2 1 06-66027-B E3323-000-00 Illuminated signs "NO SMOKING / FASTEN SEAT BELT" 0.7 1.5 1 06-81032-B E8511-900-10 Electrical release for fire extinguishing bucket (Bambi Bucket), fixed provisions 0.8 1.8 1 06-81032-B E8511-900-20 Electrical release for fire extinguishing bucket (Bambi Bucket), detachable parts 0.6 1.3 Interior Layout 1 07-27035-C E2522-006-00 Passenger seating, 3 seats with 4-point restraint system (front row, facing against flight direction) 38.1 84.0 1 07-27037-B E2522-106-10 Passenger seating, 3 utility seats with 4-point restraint system (rear row, facing in flight direction), fixed provisions 1.7 3.7 1 07-27037-B E2522-106-20 Passenger seating, 3 utility seats with 4-point restraint system (rear row, facing in flight direction), detachable parts 33.2 73.2 1 07-40037-C E2532-000-00 Sealed cabin floor 0.3 0.7 1 07-50082-B E5231-000-00 One-hand latching system for clam-shell doors 1.4 3.1 1 07-50083-A E5231-100-00 Extended opening fasteners for clam-shell doors 0.1 0.2 1 07-50084-A E5213-101-00 Sliding door fastener, max. position, LH 0.3 0.7 1 07-50084-A E5213-102-00 Sliding door fastener, max. position, RH 0.3 0.7 1 07-50085-B E5212-000-00 Jettisonable cockpit doors 0.9 2.0 1 07-50086-B E5212-100-00 Spoiler position for cockpit doors 1.0 2.2 1 07-60049-B E2513-005-00 Map cases in sliding doors 1.4 3.1 1 07-60050-B E2550-000-00 Variable tie-down net 3.3 7.3 1 07-74099-B AAT-35120-006-2 Foldable stretcher Rescue (AAT - STC)c 18.7 41.2 Qty Document Reference Commercial Reference Description kg lb 135 T3H/P3H 18.101.01 E 57 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data Avionics 1 08-12101-A E2312-000-00 Tactical radio VHF-FM NPX138N (Cobham)d 2.5 5.5 1 08-12102-B E2317-000-00 Tactical radio, fixed provisions, incl. antenna, power supply & intercom interfaced 2.0 4.4 1 08-15568-B E2315-400-00 LTE phone, fixed provisions, incl. antenna, power supply (28 VDC) & intercom interfacee 1.0 2.2 1 08-15569-C E2316-000-00 Wireless intercom system PNG (Axnes), basic systemf 2.6 5.7 1 08-15569-C E2316-100-00 Wireless intercom system PNG (Axnes), cockpit control panel CP50 0.5 1.1 1 08-15569-C E2316-200-00 Wireless intercom system PNG (Axnes), mobile transceiver MP50g 1.0 2.2 1 08-15570-B E2315-000-00 Iridium satellite transceiver GSR 56 (Garmin) 4.3 9.5 1 08-16164-C E2341-005-00 Digital Audio Control System (DACS), ACP53 (Cobham), pax 1.2 2.6 1 08-18079-B E2342-005-00 Headset adapter cable pax GLENAIR / U92 0.2 0.4 1 08-35070-B E2327-000-10 Traffic Advisory System TAS620A (Avidyne), fixed provisions 3.0 6.6 1 08-35070-B E2327-000-20 Traffic Advisory System TAS620A (Avidyne), detachable parts 3.4 7.5 1 08-43078-A E3464-000-00 Wireless connectivity Connext (Garmin) 0.3 0.7 1 08-46070-A E3169-000-00 Moving map - Helionixh 0.0 0.0 a. Hoist operation & maintenance training included. Details are provided in the respective documentation. b. incl. auto-activation. c. This STC is only EASA certified. Prices and leadtimes for national certifications are available on request. d. Onboard HF/tact. radio transm. can influence radio nav. systems (MKR, VOR, ILS, ADF) and com systems (VHF/other tact. radio). Depending on NAA cert. requirements, such systems must either be turned off during IFR approaches/departures or deactivated. e. Without integration and EASA certification of LTE phone. f. Mobile transceiver and cockpit control panel not included. g. Mobile transceiver with defined frequency range between 440 - 450 MHz and in yellow color. h. The database update service is provided under a dedicated service contract. Please contact your Airbus helicopter sales representative for further information. Qty Document Reference Commercial Reference Description kg lb The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 58 135 T3H/P3H 18.101.01 E Technical Data 4.4.4 Aerial Work Mission Performance Weight breakdown (with payload and fuel) Mission profile • Takeoff at SL (maximum 2,980 kg) • Climb flight AEO-MCP from SL to 5,000 ft with VY, mean 65 KIAS • Level flight in 5,000 ft with VBR (PW206B3: 133 KTAS; Arrius 2B2plus: 135 KTAS) • Descent from 5,000 ft to SL with R/D of 1,000 fpm, mean 80 KIAS • Landing at SL Payload range diagram Relevant flight data kg lb Weight basis for Payload Range Diagram Equipped empty weight aerial work configuration (incl. engine oil, unusable fuel and weight margin) 1750 3858 1 pilots (1 x 85 kg) 85 187 Payload Payload 585 1,290 Fuel Reserve fuel: 20 min in 1,500 ft with 130 KIAS 67 148 Trip fuel 493 1,087 Mission takeoff weight (MTOW) 2,980 6,570 Figure 4.12: Aerial Work configuration - payload range diagram PW206B3 engines Arrius 2B2 plus engines Calculated maximum range (without payload, with trip fuel) 344 NM (637 km) 346 NM (641 km) Corresponding flight time (incl. 2x climb / descent phases) 2 h 37 min 2 h 36 min 135 T3H/P3H 18.101.01 E 59 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 5 Further Equipment Information 5.1 General Available Equipment The following list presents the General Available Equipment which may be added to customize the mission configurations or to build specific configurations. For further mission adaptation specific equipment is also available on request. Any modification and/or complement of the proposed mission configuration shall be done with the assistance of an Airbus helicopter sales representative to avoid incompatibilities between various optional equipment items. The General Available Equipment is categorized as shown in the following table: Abbreviation Availability R Included in the Mandatory or Reference Equipment of the mission configuration F Included in the Further Available Equipment of the mission configuration G General Available Equipment for the mission configuration Document Reference Commercial Reference Description kg lb EMSLaw EnforcementOffshore TransportationAerial WorkGeneral Equipment 05-02084-A E1111-100-00 Enhanced exterior painting instead of standard painting 2.0 4.4 R R R F 05-02084-A E1111-300-00 Complex exterior painting instead of standard painting 2.7 6.0 05-02085-B E6211-000-00 High visibility paint for main rotor blades 0.0 0.0 G G F F 05-02086-A E1111-900-00 Surface protective coating (Airglaze) 0.5 1.1 G G F F 05-02087-B E6211-100-00 Main rotor blade erosion protection paint 0.1 0.2 F F F F 05-12010-A E7110-300-00 Maintenance step on cabin roof, LH 0.7 1.5 F F 05-12011-B E2516-000-00 Boarding grips for cockpit 0.1 0.2 F G F F 05-21036-C E8541-000-10 Cable cutter system, fixed provisions 3.1 6.8 F F G G 05-21036-C E8541-000-20 Cable cutter system, detachable parts 8.1 17.9 F F G G 05-25037-C E7162-000-00 Inlet Barrier Filter (IBF) system 19.1 42.1 F F F F 05-26020-A E1241-100-00 Corrosion protection for high corrosive environment 3.2 7.1 G F R F 05-30004-C E3310-001-00 Flashlight for copilot side 0.3 0.7 R R R G 05-31146-A E2511-000-00 Tinted sun shades for cockpit windshield roof section 1.8 4.0 F F F F 05-31147-A E5632-005-00 Sliding windows in sliding doors 1.2 2.6 R F F 05-31148-A E5633-001-00 Window in clam-shell door LH 0.3 0.7 R G G 05-31148-A E5633-002-00 Window in clam-shell door RH 0.3 0.7 F G G 05-31149-B E5611-300-00 Tinted front windshields 0.0 0.0GGGG 05-31149-B E5632-300-00 Tinted windows in cockpit doors 0.0 0.0 GGGG 05-31149-B E5632-305-00 Tinted windows in cabin incl. sliding windows in sliding doors 1.2 2.6 05-31150-A E2524-000-10 IFR training screens, fixed provisions 0.1 0.2 G G G 05-31150-A E2524-000-20 IFR training screens, detachable parts 1.2 2.6 G G G The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 60 135 T3H/P3H 18.101.01 E Technical Data 05-31151-A E2521-600-10 Curtains for cabin windows - NVG, fix provisions 0.2 0.4 F 05-31151-A E2521-600-20 Curtains for cabin windows - NVG, detachable parts 1.3 2.9 F 05-31152-A E5632-100-00 Ram air deflectors for sliding windows in cockpit doors 0.6 1.3 G G F F 05-31152-A E5632-105-00 Ram air deflectors for sliding windows in sliding doors 0.4 0.9 F F 05-36035-A E8532-001-00 Multifunction step LH instead of standard boarding step 3.9 8.6 R 05-36035-A E8532-002-00 Multifunction step RH instead of standard boarding step 3.9 8.6 R 05-37031-B E6700-101-00 Pedal cover for copilot flight controls -4.8 -10.6 F F F R 05-39021-A E2513-001-00 Map case in copilot door 0.4 0.9 R R R G 05-39023-A E3315-102-00 Illuminated chart holder, pilot 0.9 2.0 R R R R 05-39023-A E3315-101-00 Illuminated chart holder, copilot 0.8 1.8 F F F F 05-42051-B E2111-000-00 Air Conditioning System (ACS) 49.7 109.6 F F F 05-44014-B E2122-100-00 Ventilation enhancement for cockpit 1.0 2.2 F 05-62029-A E2420-000-00 Alternating Current (AC) systema 1.5 3.3 05-67040-B E2460-000-00 Power sockets (2x 28 VDC, 20 A) at center console 1.1 2.4 R 05-81054-A E2818-000-10 Internal long range fuel tank system, fixed provisions 2.0 4.4 F F 05-81054-A E2818-000-20 Internal long range fuel tank system, detachable parts 35.9 79.1 F F 05-85018-A E2841-000-00 Fuel management system (fuel flow meters) 1.0 2.2 F R F F 05-92019-A E6611-000-00 Main rotor blade folding, basic kit 1.5 3.3 F F 05-92019-A E6611-100-10 Main rotor blade folding, fixed provisions for ground handling kit 0.8 1.8 F F 05-92019-A E6611-100-90 Main rotor blade folding, ground handling kit GSE GSE F F 05-93017-A E1021-000-10 Lashing points for wind speeds up to 40 kts, fixed provisions 1.6 3.5GFFF 05-93017-A E1021-000-20 Lashing points for wind speeds up to 40 kts, detachable parts 0.8 1.8GFFF 05-93018-A E1021-100-10 Lashing points for ship landings, fixed provisions 2.1 4.6 05-93018-A E1021-100-20 Lashing points for ship landings, detachable parts 0.3 0.7 05-95005-A E1320-200-00 Long term cover kit for helicopter GSE GSE G G F F 05-95006-A E1320-300-00 Main rotor head cover GSE GSE 05-97006-B E6201-100-00 Accelerometers for track and balance system (Chadwick Helmuth) 0.0 0.0GGGG 05-97007-B E6201-200-10 Optical tracker FasTrak 11800-3 (Chadwick Helmuth), fixed provisions 0.1 02GGGG 05-97007-B E6201-200-20 Optical tracker FasTrak 11800-3 (Chadwick Helmuth), detachable parts 0.6 1.3GGGG Specific Mission Equipment 06-11044-A E3274-000-10 Settling protectors, fixed provisions 0.1 0.2 R F G G 06-11044-A E3274-000-20 Settling protectors, detachable parts 8.1 17.9 R F G G 06-11045-B E3272-000-10 Snow skids, fixed provisions 0.9 2.0 06-11045-A E3272-000-20 Snow skids, detachable parts 18.3 40.3 06-12028-A E3210-100-00 Medium height landing gear instead of standard landing gear 5.2 11.5 F R R Document Reference Commercial Reference Description kg lb EMSLaw EnforcementOffshore TransportationAerial Work 135 T3H/P3H 18.101.01 E 61 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 06-12029-A E3213-100-00 Extended skid protection 3.4 7.5 GGGG 06-21042-D E8510-001-10 External hoist LH, fixed provisions 13.1 28.9 F F F 06-21042-D E8510-001-20 External hoist LH, detachable parts 2.6 5.7 F F F 06-21042-D E8510-002-10 External hoist RH, fixed provisions 13.8 30.4 F F 06-21042-D E8510-002-20 External hoist RH, detachable parts 2.5 5.5 F F 06-21042-D E8510-100-31 External hoist (without hook and damper kit), 90 m, vendor partsb 62.4 137.6 F F 06-21042-D E8510-000-31 External hoist (without hook and damper kit), 50 m, vendor partsb 56.2 123.9 F 06-21042-D E8510-300-30 External hoist, small hook damper kit & D-LOK hook, vendor parts 2.3 5.1 F F F 06-21042-D E8510-300-31 External hoist, small hook damper kit & slide lock hook, vendor parts 2.3 5.1 06-24027-B E8534-101-21 External rope-down device for 2/1 persons (ECMS - STC), LH retractable, detachable partsc 16.3 35.9 06-24027-B E8534-102-21 External rope-down device for 2/1 persons (ECMS - STC), RH retractable, detachable partsc 16.3 35.9 06-24027-B E8534-200-10 Enhanced external rope down device (ECMS - STC), LH & RH, electrical fixed provisionsc 3.5 7.7 F 06-24027-B E8534-300-00 Enhanced external rope down device (ECMS - STC), control panel 0.5 1.1 F 06-24027-B E8534-400-00 Enhanced external rope down device (ECMS - STC), hand controllerc 2.0 4.4 F 06-24027-B E8534-601-20 Enhanced external rope down device for 2/1 persons (ECMS - STC), LH retractable, detachable partsc 19.3 42.5 F 06-24027-B E8534-602-20 Enhanced external rope down device for 2/1 persons (ECMS - STC), RH retractable, detachable partsc 19-3 42.5 F 06-24027-B E8534-001-10 External rope-down device for 2 persons, LH, fixed provisions 7.5 16.5 R 06-24027-B E8534-002-10 External rope-down device for 2 persons, RH, fixed provisions 7.5 16.5 R 06-26028-A E8512-002-10 Cargo hook mirrors RH, fixed provisions 0.5 1.1 F F 06-26028-A E8512-002-20 Cargo hook mirrors RH, detachable parts 4.0 8.8 F F 06-26028-A E8512-002-90 Cover for cargo hook mirrors RH 0.4 0.9 F F 06-26029-A E3181-000-10 External multi-purpose camera on tail boom, fixed provisions 2.0 4.4FFFR 06-26029-A E3181-000-20 External multi-purpose camera on tail boom, detachable parts 0.6 1.3FFFR 06-26029-A E3181-100-10 External rear-view camera on landing gear, fixed provisions 1.5 3.3FFFF 06-26029-A E3181-100-20 External rear-view camera on landing gear, detachable parts 1.4 3.1FFFF 06-27049-D E8511-000-10 Single cargo hook system, fixed provisions 5.2 11.5 R 06-27049-D E8511-000-20 Single cargo hook system, detachable parts 25.9 57.1 F 06-27049-D E8511-500-10 Dual cargo hook system, fixed provisions 6.6 14.6 F Document Reference Commercial Reference Description kg lb EMSLaw EnforcementOffshore TransportationAerial Work The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 62 135 T3H/P3H 18.101.01 E Technical Data 06-27049-D E8511-500-20 Dual cargo hook system, detachable parts 29.6 65.3 F 06-27049-D E8511-600-10 Cargo hook system, remote control grip, fixed provisions 0.3 0.7 F F 06-27049-D E8511-600-20 Cargo hook system, remote control grip, detachable parts 0.9 2.0 F F 06-27049-D E8511-700-00 Dual cargo hook system, copilot electrical release 0.3 0.7 F 06-27049-D E8511-800-10 Cargo hook weighing system, fixed provisions 0.2 0.4 F 06-27049-D E8511-800-20 Cargo hook weighing system, detachable parts 0.2 0.4 F 06-31029-B E8531-000-10 External loudspeaker system with siren, fixed provisions 5.9 13.0 G R G 06-31029-B E8531-000-20 External loudspeaker system with siren, detachable parts 4.8 10.6 G R G 06-45082-B E3343-300-10 2nd Search & landing light, fixed provisions 1.7 3.7 F F 06-45082-B E3343-300-20 2nd Search & landing light, detachable parts 3.1 6.8 F F 06-45082-B E3343-900-00 Search & landing light, IR mode 0.1 0.2 F R 06-45083-B E3346-000-10 Searchlight A800 (Trakka) basic LH, fixed provisions 4.4 9.7 R 06-45083-B E3346-000-20 Searchlight A800 (Trakka) basic LH, detachable parts 23.1 50,9 R 06-45083-B E3346-000-30 Searchlight A800 (Trakka), vendor parts 18.2 40.1 R 06-45083-B E3346-100-00 Searchlight A800 (Trakka), IR filters 0.0 0.0 R 06-45083-B E3346-200-00 Searchlight A800 (Trakka), IR laser pointer 0.1 0.2 R 06-46012-A E3344-100-00 White strobe lights 1.3 2.9 F F F F 06-61036-B E3215-100-10 Emergency floats, fixed provisionsd 9.5 20.9 F R F 06-61036-B E3215-000-20 Emergency floats, detachable parts 63.4 139.8 F R F 06-62034-A E2565-001-10 External Life Raft System (ELRS) LH, fixed provisions 0.8 1.8 F 06-62034-A E2565-001-20 External Life Raft System (ELRS) LH, detachable partse 37.1 81.8 F 06-62034-A E2565-002-10 External Life Raft System (ELRS) RH, fixed provisions 0.8 1.8 F 06-62034-A E2565-002-20 External Life Raft System (ELRS) RH, detachable partse 37.1 81.8 F 06-62034-A E2562-600-00 Survival emergency locator transmitter ELT(S) 0.9 2.0 F 06-65016-B E2625-100-00 2nd portable fire extinguisher 2.8 6.2 F F F F 06-66024-B E3353-000-00 Emergency lights incl. boarding step illuminations 3.5 7.7 R 06-66025-B E3342-400-00 Boarding step illuminations 0.3 0.7 R G 06-66026-A E3353-100-00 Helicopter Emergency Egress Lighting System (HEELS) 5.8 12.8 R 06-66027-B E3323-000-00 Illuminated signs "NO SMOKING / FASTEN SEAT BELT 0.7 1.5 F F 06-67080-A E2562-400-00 Automatic Deployable Emergency Locator Transmitter (ADELT) 10.3 22.7 R 06-71011-B E2521-500-10 Separation curtain for cockpit / cabin, fixed provisions 0.3 0.7 R R R R 06-71011-B E2521-500-20 Separation curtain for cockpit / cabin, detachable parts 0.3 0.7 R R R R 06-81032-B E8511-900-10 Electrical release for fire extinguishing bucket (Bambi Bucket), fixed provisions 0.8 1.8 F 06-81032-B E8511-900-20 Electrical release for fire extinguishing bucket (Bambi Bucket), detachable parts 0.6 1.3 F Interior Layout 07-15035-A E2512-202-00 Advanced pilot seat instead of standard pilot seat 1.6 3.5 07-15035-A E2512-201-00 Advanced copilot seat instead of standard copilot seat 1.6 3.5 Document Reference Commercial Reference Description kg lb EMSLaw EnforcementOffshore TransportationAerial Work 135 T3H/P3H 18.101.01 E 63 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 07-27035-C E2522-005-00 Passenger seating, 3 seats with 3-point restraint system (front row, facing against flight direction) 37.4 82.5 07-27035-C E2522-105-00 Passenger seating, 2 seats with 3-point restraint system (rear row, facing in flight direction) 22.2 48.9 07-27035-C E2522-307-00 Passenger seating, 1 seat with 4-point restraint system (rear row, facing in flight direction, LH) 11.3 24.9 R 07-27035-C E2522-308-00 Passenger seating, 1 seat with 4-point restraint system (rear row, facing in flight direction, RH) 11.3 24.9 R 07-27035-C E2522-006-00 Passenger seating, 3 seats with 4-point restraint system (front row, facing against flight direction) 38.1 84.0 R F 07-27037-B E2522-106-10 Passenger seating, 3 utility seats with 4-point restraint system (rear row, facing in flight direction), fixed provisions 1.7 3.7 F 07-27037-B E2522-106-20 Passenger seating, 3 utility seats with 4-point restraint system (rear row, facing in flight direction), detachable parts 33.2 73.2 F 07-30078-B E2581-100-00 Enhanced sound proofing kit 27.0 59.6 07-30079-A E2521-100-00 Separation wall for cabin / cargo compartment 4.4 9.7 07-40036-B E2515-100-00 Washable floor covering for cockpit 3.6 7.9 R 07-40036-B E2515-000-00 Washable floor covering for cockpit, cabin & cargo compartment 9.2 20.3 R R R 07-40037-B E2532-000-00 Sealed cabin floor 0.3 0.7 F R F 07-40038-B E2531-000-00 Multifunctional floor instead of standard cabin floor 16.7 36.8 G 07-50082-B E5231-000-00 One-hand latching system for clam-shell doors 1.4 3.1 R F F F 07-50083-A E5231-100-00 Extended opening fasteners for clam-shell doors 0.1 0.2 R F F 07-50084-A E5213-001-00 Sliding door fastener, intermediate and max. position, LH 1.2 2.6 07-50084-A E5213-101-00 Sliding door fastener, max. position, LH 0.3 0.7 F R F F 07-50084-A E5213-002-00 Sliding door fastener, intermediate and max. position, RH 1.2 2.6 07-50084-A E5213-102-00 Sliding door fastener, max. position, RH 0.3 0.7 G R F F 07-50085-B E5212-000-00 Jettisonable cockpit doors 0.9 2.0 G G R F 07-50086-B E5212-100-00 Spoiler position for cockpit doors 1.0 2.2 R F F 07-50088-B E8513-000-00 Abrasion protection at sliding doors 0.2 0.4 F G G 07-50089-A E5211-200-00 Securing device for complete opening of cockpit doors 1.1 2.4 F F 07-60049-B E2513-005-00 Map cases in sliding doors 1.4 3.1 F F F F 07-60050-B E2550-000-00 Variable tie-down net 3.3 7.3 F R F 07-74099-B AAT-35120-006-2 Foldable stretcher Rescue (AAT - STC)c 18.7 41.2 F F Avionics 08-10026-B E2311-000-10 HF system HF-9000 (Rockwell Collins), fixed provisionsf 7.2 15.9 G G 08-10026-B E2311-000-20 HF system HF-9000 (Rockwell Collins), detachable partsf 19.3 42.5 G G 08-12101-A E2312-000-00 Tactical radio VHF-FM NPX138N (Cobham)g 2.5 5.5 R R F Document Reference Commercial Reference Description kg lb EMSLaw EnforcementOffshore TransportationAerial Work The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 64 135 T3H/P3H 18.101.01 E Technical Data 08-12102-B E2317-000-00 Tactical radio, fixed provisions, incl. antenna, power supply & intercom interfaceg 2.0 4.4 R F F 08-15568-B E2315-400-00 LTE phone, fixed provisions, incl. antenna, power supply (28 VDC) & intercom interfaceh 1.0 2.2FFFF 08-15569-C E2316-000-00 Wireless intercom system PNG (Axnes), basic systemi 2.6 5.7FFFF 08-15569-C E2316-100-00 Wireless intercom system PNG (Axnes), cockpit control panel CP50 0.5 1.1FFFF 08-15569-C E2316-200-00 Wireless intercom system PNG (Axnes), mobile transceiver MP50j 1.0 2.2FFFF 08-15570-B E2315-000-00 Iridium satellite transceiver GSR 56 (Garmin) 4.3 9.5 F F F 08-16164-C E2341-005-00 Digital Audio Control System (DACS), ACP53 (Cobham), pax 1.2 2.6 R R F F 08-16166-A E2340-000-00 Headset electrical power supply (28 VDC), fixed provisionsk 0.5 1.1 08-18078-A E2315-100-00 Headset H 10-76 (David Clark), low impedance 0.6 1.3 R R R R 08-18078-A E2315-200-00 Headset H 10-56 (David Clark), high impedance 0.6 1.3 08-18079-B E2342-000-00 Headset adapter cable crew GLENAIR / U92 0.1 0.2 R R R R 08-18079-B E2342-005-00 Headset adapter cable pax GLENAIR / U92 0.2 0.4 R R R F 08-18079-B E2342-100-00 Headset adapter cable crew GLENAIR / LEMO ANR 0.1 0.1 08-18079-B E2342-105-00 Headset adapter cable pax GLENAIR / LEMO ANR 0.2 0.4 08-18080-B E2315-300-00 Headset A20 ANR LEMO (Bose), low impedance 0.3 0.7 08-24038-A E3452-100-00 Automatic Direction Finder (ADF), control unit CDF552 (Cobham) 1.0 2.2 F 08-24038-A E3452-000-00 Automatic Direction Finder (ADF), receiver DF-431B (Cobham) 11.0 24.3 F 08-31070-A E3443-200-00 Color weather radar RDR 2000 (Honeywell), radar radome 3.2 7.1 08-31070-A E3443-000-10 Color weather radar RDR 2000 (Honeywell), fixed provisions 0.8 1.8 08-31070-A E3443-010-30 Color weather radar RDR 2000 incl. control unit CP466 (Honeywell), vendor parts 6.7 14.8 08-31070-A E3443-020-30 Color weather radar RDR 2000 incl. control unit CP466 - NVG (Honeywell), vendor parts 6.7 14.8 08-31071-B E3443-300-00 Search and rescue weather radar RDR-1600 (Telephonics), radar radome 5.3 11.7 08-31071-B E3443-100-10 Search and rescue weather radar RDR-1600 (Telephonics), fixed provisions 1.7 3.7 08-31071-B E3443-100-20 Search and rescue weather radar RDR-1600 (Telephonics), detachable parts 12.9 28.4 08-35070-B E2327-000-10 Traffic Advisory System TAS620A (Avidyne), fixed provisions 3.0 6.6FFFF 08-35070-B E2327-000-20 Traffic Advisory System TAS620A (Avidyne), detachable parts 3.4 7.5FFFF 08-43078-A E3464-000-00 Wireless connectivity Connext (Garmin) 0.3 0.7 F F F F Document Reference Commercial Reference Description kg lb EMSLaw EnforcementOffshore TransportationAerial Work 135 T3H/P3H 18.101.01 E 65 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 08-46068-B E3168-000-00 Moving map EuroNav 7 – RN7 (EuroAvionics), basic versionl 6.3 13.9 R 08-46068-B E3168-100-00 Moving map EuroNav 7 – RN7 (EuroAvionics), Iridium satcom module 1.4 3.1 F 08-46068-B E3168-400-00 Moving map EuroNav 7– RN7 (EuroAvionics), GSM / UMTS module 0.5 1.1 F 08-46068-B E3168-300-00 Moving map EuroNav 7 – RN7 (EuroAvionics), FLARM module 0.6 1.3 F 08-46068-B E3168-600-00 Moving map EuroNav 7 – RN7 (EuroAvionics), weather radar interface 0.0 0.0 08-46070-A E3169-000-00 Moving map - Helionixm 0.0 0.0 F F F 08-65068-B E3315-002-00 Electrical fixed provisions, 5 VDC, pilot 0.6 1.3 08-65068-B E2461-001-00 Electrical fixed provisions, 5 VDC, copilot 0.6 1.3 08-65068-B E3315-302-00 iPad mini holder, pilot 0.6 1.3 08-65068-B E3315-402-00 iPad Air holder, pilot 0.7 1.5 08-65068-B E3315-301-00 iPad mini holder, copilot 0.6 1.7 08-65068-B E3315-401-00 iPad Air holder, copilot 0.7 1.5 08-81046-C E3132-000-10 Cockpit Voice and Flight Data Recorder (CVFDR), fixed provisions 3.3 7.3 F F R 08-81046-C E3132-000-20 Cockpit Voice and Flight Data Recorder (CVFDR), detachable partsn 4.7 10.4 F F R 08-83047-A E3171-000-10 Health Monitoring System (HMS), fixed provisions 3.1 6.8 F 08-83047-A E3171-000-20 Health Monitoring System (HMS), detachable parts 2.7 6.0 F 08-83048-A E3171-200-00 Professional Ground Station (PGS) Vision Systemo GSE GSE F F R 08-83049-A E3171-100-00 Helicopter Flight Data Monitoring (HFDM)p GSE GSEFFF a. 50 VA b. Hoist operation & maintenance training included. Details are provided in the respective documentation. c. This STC is only EASA certified. Prices and leadtimes for national certifications are available on request. d. incl. auto-activation e. Operator to equip ELT(S) meeting ICAO Annex 10 requirements to comply with EASA OPS. f. Onboard HF/tact. radio transm. can influence radio nav systems (MKR, VOR, ILS, ADF) and com systems (VHF/other tact. radio). Depending on NAA cert. requirements, such systems must either be turned off during IFR approaches/departures or deactivated. Export clearance needs to be clarified by Airbus helicopters sales representative. g. Onboard HF/tact. radio transm. can influence radio nav systems (MKR, VOR, ILS, ADF) and com systems (VHF/other tact. radio). Depending on NAA cert. requirements, such systems must either be turned off during IFR approaches/departures or deactivated. h. Without integration and EASA certification of LTE phone. i. Mobile transceiver and cockpit control panel not included. j. Mobile transceiver with defined frequency range between 440 – 450 MHz and in yellow color. k. Required for Active Noise Reduction (ANR). l. incl. 512 GB flashdisk and Global Map Package m. The database update service is provided under a dedicated service contract. Please contact your Airbus helicopter sales representative for further information. n. Ground station not included. o. Recommended 1 per customer base if CVFDR is selected. p. Instead of PGS Vision System Document Reference Commercial Reference Description kg lb EMSLaw EnforcementOffshore TransportationAerial Work The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 66 135 T3H/P3H 18.101.01 E Technical Data 5.2 Avionics Layout Single / Dual Pilot IFR with dual GTN 750 (Garmin) 1. GPS / NAV / COM GTN 750 (Garmin), pilot 2. Audio Control Panel ACP53 (Cobham), pilot 3. Cockpit Control Panel (CCP) 4. Data Transfer Device (DTD) 5. Audio Control Panel ACP53 (Cobham), copilot 6. GPS / NAV / COM GTN 750 (Garmin), copilot 7. Flight Display Subsystem (FDS), copilot Figure 5.1: Single / Dual Pilot IFR GTN 750 (Garmin) Qty Document Reference Commercial Reference Description kg lb 1 08-00447-B E2300-120-00 Avionics Package DP IFR GC GTN 750 0.0 0.0 1 08-16164-C E2341-000-00 Digital Audio Control System (DACS), incl. ACP53 (Cobham), pilot + copilot 5.8 12.8 1 08-22083-A E3451-000-00 Transponder GTX 335R (Garmin)a a. incl. ADS-B out. 2.4 5.3 1 08-25519-A E3455-000-00 Distance Measuring Equipment (DME) DME-4000 (Rockwell Collins) 2.6 5.7 1 08-26063-A E3431-000-00 Marker beacon receiver MKR3300-1 (Becker) 1.2 2.6 1 08-43077-C E3463-001-00 GPS/NAV/COM GTN 750 (Garmin), copilotb b. SBAS RNP approach local service availability verification through Airbus Helicopters on request. 6.9 15.2 1 08-43077-C E3463-002-00 GPS/NAV/COM GTN 750 (Garmin), pilotb 8.2 18.1 1 08-65054-A E3161-001-00 Flight Display Subsystem (FDS), copilot 5.5 12.1 1 08-99005-B E0000-151-00 Avionics Package DP IFR GTN Series interconnection / wiring 23.5 51.8 135 T3H/P3H 18.101.01 E 67 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data Single Pilot IFR with dual GTN 750 (Garmin) 1. GPS / NAV / COM GTN 750 (Garmin), pilot 2. Audio Control Panel ACP53 (Cobham), pilot 3. Cockpit Control Panel (CCP) 4. Data Transfer Device (DTD) 5. Audio Control Panel ACP53 (Cobham), copilot 6. GPS / NAV / COM GTN 750 (Garmin), copilot Figure 5.2: Single Pilot IFR GTN 750 (Garmin) Qty Document Reference Commercial Reference Description kg lb 1 08-00452-A E2300-122-00 Avionics Package SP IFR GC GTN 750 0.0 0.0 1 08-16164-C E2341-000-00 Digital Audio Control System (DACS), incl. ACP53 (Cobham), pilot + copilot 5.8 12.8 1 08-22083-A E3451-000-00 Transponder GTX 335R (Garmin)a a. incl. ADS-B out. 2.4 5.3 1 08-25519-A E3455-000-00 Distance Measuring Equipment (DME) DME-4000 (Rockwell Collins) 2.6 5.7 1 08-26063-A E3431-000-00 Marker beacon receiver MKR3300-1 (Becker) 1.2 2.6 1 08-43077-C E3463-001-00 GPS/NAV/COM GTN 750 (Garmin), copilotb b. SBAS RNP approach local service availability verification through Airbus Helicopters on request. 6.9 15.2 1 08-43077-C E3463-002-00 GPS/NAV/COM GTN 750 (Garmin), pilotb 8.2 18.1 1 08-99005-B E0000-152-00 Avionics Package SP IFR GTN Series interconnection / wiring 23.5 51.8 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 68 135 T3H/P3H 18.101.01 E Technical Data 5.3 Antenna Layout 1. ELT antenna 2. VOR / ILS antenna 3. VHF / AM 2 antenna 4. GPS 2 antenna 5. GPS 1 antenna 6. FM Antenna 7. IRIDIUM antenna 8. TETRA antenna 9. Radar altimeter antenna 10. ADF antenna 11. ATC antenna 12. Marker antenna 13. DME antenna 14. VHF-AM 1 antenna Figure 5.3: Typical IFR antenna layout 135 T3H/P3H 18.101.01 E 69 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 5.4 NVG friendly & NVIS Certification In order to increase mission capabilities and flight safety during night operations, the H135 can be fitted with NVG friendly cockpit and cabin layouts as well as NVG friendly exterior lighting. Helicopters in an "NVG friendly" configuration are designed and built in order to not degrade the NVG image performance, by considering the design standards detailed hereafter: • The internal lighting of the cockpit is designed and built in order to fulfill RTCA/DO-275 "Minimum Operational Performance Standard for Integrated Night Vision Imaging System Equipment". • All NVIS equipment items installed (excluding BFE) are not degrading the NVG image performance or the NVG image performance degradation is kept within acceptable limits in NVG mode. NOTE: BFE might not be compliant in accordance with the applicable specifications and requirements. Airbus does not perform any actions to ensure the NVG performance degradation is being kept within acceptable limits. • The interior of the helicopter is kept in dark, matt colors, showing no or only little reflectance of radiation, not degrading the NVG image performance in NVG mode. • An appropriate Day/Night/NVG switch is provided. • The external lighting of the cockpit is designed and built in order to fulfill SAE-ARP 4392, "Lighting, Aircraft Exterior, Night Vision Imaging System (NVIS) Compatible", i. e. the NVG performance degradation caused by the external lighting system in NVG mode is kept within acceptable limits. May 28, 2009, the first NVIS certification providing the H135 with a NVG aided operation capability was granted from EASA. Thus Airbus is the first Original Equipment Manufacturer (OEM) to offer this capability to civil operators. The EASA NVIS certification is based on one customer specific configuration; any additional changes to the configuration following EASA NVIS certification may require additional certification effort. EASA certification is based on night vision goggles with class B filter from well-known manufacturers (certified goggles include, ITT F4949 and L3 Communications M949). On customer's request, Airbus can develop and certify also night vision goggle systems from other manufacturers. Please note that classic night flight capability remains unrestricted. For the avoidance of doubt, configurations marked as being "NVG friendly" in this document do not include a helicopter NVIS certification. Such "Night Vision Imaging System (NVIS) certification" is only provided by Airbus, if it is explicitly listed in the individual customer's contract. The "Night Vision Imaging System (NVIS) certification" includes delivery of a customer configuration specific Flight Manual Appendix ("Appendix for Night Vision Imaging Systems (NVIS) / NVG - Operator") and "Operator Substantiation Report for Night Vision Imaging System (NVIS) / NVG" and provides proof of compliance with the airworthiness requirements for the NVG operations capabilities of the helicopter. Note that the "Night Vision Imaging System (NVIS) certification" does not constitute an approval for NVG operations as per Commission Regulation No 965/2012, SPA.NVIS.100 ("Helicopters shall only be operated under VFR at night with the aid of NVIS if the operator has been approved by the competent authority"). The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 70 135 T3H/P3H 18.101.01 E Technical Data 5.5 Disclaimers EASA-OPS Please note that some recommended mission configurations include equipment requested by EASA- OPS. They do not cover oxygen equipment and the entire equipment required for extended over water or offshore operations. The operator shall contact his national authority for the approval of the planned aircraft mission configuration. Export control regulations Airbus Helicopters is committed to strict compliance with all applicable export control regulations and requires a corresponding commitment from the Customer. Some items/commodities are controlled under at least one export control law or regulation and therefore may require export authorization(s) and Airbus Helicopters cannot guarantee that they will be granted. Nevertheless Airbus Helicopters will perform all necessary procedures for obtaining such authorization(s). The Customer shall support the authorization(s) application(s) procedure(s) by providing the necessary documentation and information, particularly end-user certificates, undertakings, documents on the utilization of the items/commodities, etc. The Customer shall comply with the conditions of the export authorization(s). Airbus Helicopters reserves the right to deliver the helicopter without the controlled items, should the competent authorities deny or delay export authorization(s). The same is valid if the competent authorities do not react at all or in cases of a return without action or if otherwise the absence of a required authorizations or provisions of any regulations inhibit a delivery in time. 135 T3H/P3H 18.101.01 E 71 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 6 Main Performance The performance figures shown hereafter are guaranteed minimum performance data (minimum specification engine power). Only the fuel consumption, range and endurance values and figures refer to a H135 equipped with minimum specified new production engines. Unless otherwise specified, the values and figures refer to a clean helicopter configuration at Sea Level (SL), in International Standard Atmosphere (ISA) and zero wind condition. 6.1 Performance Summary Tables All Engine Operative (AEO) - Altitude, Rate of Climb Pratt & Whitney Canada PW206B3, standard air intake kg lb 2,720 5,997 2,835 6,250 2,910 6,415 2,980 6,570 Hover ceiling IGE (4 ft AGL), TOPa •ISA m ft 4,816 15,800 4,465 14,650 4,237 13,900 4,039 13,250 • ISA + 20°C m ft 4,084 13,400 3,719 12,200 3,490 11,450 3,277 10,750 Hover ceiling OGE, TOPa •ISA m ft 4,084 13,400 3,429 11,250 2,896 9,500 2,195 7,200 • ISA +20°C m ft 3,261 10,700 2,880 9,450 2,484 8,150 1,844 6,050 Service ceiling, MCP (climb reserve 200 ft/min)a •ISA m ft 5,410 17,750 5,121 16,800 4,938 16,200 4,770 15,650 • ISA +20°C m ft 4,541 14,900 4,267 14,000 4,100 13,450 3,962 13,000 Rate of climb, TOP, VY = 65 KIASa m/s ft/min 9.5 1,870 8.8 1,730 8.3 1,640 7.9 1,560 a. Preliminary performance data. The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 72 135 T3H/P3H 18.101.01 E Technical Data All Engine Operative (AEO) - Speed, Fuel Consumption, Range Pratt & Whitney Canada PW206B3, standard air intake All Engine Operative (AEO) - Speed, Fuel Consumption, Range at 5,000 ft Pratt & Whitney Canada PW206B3, standard air intake kg lb 2,720 5,997 2,835 6,250 2,910 6,415 2,980 6,570 Maximum speed (VNE)a, as IAS km/h kts 259 140 259 140 259 140 259 140 Fast cruise speed (VH)a, at TAS km/h kts 257 139 255 138 253 137 252 136 Fuel consumption at fast cruise speeda kg/h lb/h 229 505 229 505 229 505 229 505 Best range speed (VBR)a, at IAS km/h kts 248 134 248 134 246 133 246 133 Fuel consumption at best range speeda kg/h lb/h 220 485 221 487 222 489 223 492 Fuel consumption at 65 KIASa kg/h lb/h 156 344 159 351 161 355 163 359 Maximum range at best range speed (no reserve)a • Standard fuel tank (560.4 kg) km NM 646 349 641 346 637 344 633 342 • Standard and long range fuel tank (730.6 kg) km NM 846 457 841 454 837 452 832 449 Maximum endurance at 65 KIAS (no reserve)a • Standard fuel tank (560.4 kg) h:min3:463:423:393:36 • Standard and long range fuel tank (730.6 kg) h:min 4:58 4:53 4:49 4:46 a. Preliminary performance data kg lb 2,720 5,997 2,835 6,250 2,910 6,415 2,980 6,570 Fast cruise speed (VH)a, at TAS km/h kts 263 142 259 140 256 138 254 137 Fuel consumption at fast cruise speeda kg/h lb/h 219 483 219 483 219 483 219 483 Best range speed (VBR)a, at IAS km/h kts 222 120 222 120 224 121 224 121 Fuel consumption at best range speeda kg/h lb/h 194 428 198 437 203 448 205 452 135 T3H/P3H 18.101.01 E 73 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data One Engine Inoperative (OEI) - Altitude, Rate of Climb Pratt & Whitney Canada PW206B3, standard air intake One Engine Inoperative (OEI) - Maximum Gross Mass Pratt & Whitney Canada PW206B3, standard air intake Fuel consumption at 65 KIASa kg/h lb/h 144 317 147 324 150 331 153 337 Maximum range at best range speed (no reserve)a • Standard fuel tank (560.4 kg) km NM 719 388 707 382 700 378 691 373 • Standard and long range fuel tank (730.6 kg) km NM 946 511 932 503 920 497 913 493 Maximum endurance at 65 KIAS (no reserve)a • Standard fuel tank (560.4 kg) • Standard and long range fuel tank (730.6 kg) h:min h:min 4:07 5:26 4:01 5:19 3:57 5:15 3:54 5:10 a. Preliminary performance data kg lb 2,720 5,997 2,835 6,250 2,910 6,415 2,980 6,570 kg lb 2,720 5,997 2,835 6,250 2,910 6,415 2,980 6,570 Service ceiling, MCP (climb reserve 100 ft/min)a •ISA m ft 3,930 12,900 3,570 11,700 3,440 11,300 3,200 10,500 • ISA +20°C m ft 3,140 10,300 2,740 9,000 2,620 8,600 2,190 7,200 • Rate of climb, MCP, VY = 65 KIASa m/s ft/min 2.8 560 2.3 460 2.1 410 1.8 350 a. Preliminary performance data ISA ISA +20°C Hover OGE, 30 s power (NR 100%)a kg lb 2,725 6,008 2,665 5,875 Hover OGE, 2 min power (NR 102%)a kg lb 2,710 5,975 2,555 5,633 Hover OGE, 2 min power, 10 kts headwind (NR 102%)a kg lb 2,755 6,074 2,600 5,732 Hover IGE (4 ft AGL), 2 min power (NR 102%)a kg lb 2,965 6,537 2,810 6,195 Category A - VTOL, surface level and elevateda kg lb 2,980 6,570 2,950 6,504 Category A - VTOL, short fielda kg lb 2,980 6,570 2,950 6,504 a. Preliminary performance data. The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 74 135 T3H/P3H 18.101.01 E Technical Data All Engine Operative (AEO) - Altitude, Rate of Climb Pratt & Whitney Canada PW206B3, Inlet Barrier Filter (IBF) All Engine Operative (AEO) - Speed, Fuel Consumption, Range Pratt & Whitney Canada PW206B3, Inlet Barrier Filter (IBF) kg lb 2,720 5,997 2,835 6,250 2,910 6,415 2,980 6,570 Hover ceiling IGE (4 ft AGL), TOPa •ISA m ft 4,724 15,500 4,343 14,250 4,115 13,500 3,901 12,800 • ISA + 20°C m ft 3,932 12,900 3,551 11,650 3,322 10,900 3,109 10,200 Hover ceiling OGE, TOPa •ISA m ft 3,993 13,100 3,429 11,250 2,880 9,450 2,195 7,200 •ISA +20°C m ft 3,139 10,300 2,743 9,000 2,454 8,050 1,829 6,000 Service ceiling, MCP (climb reserve 200 ft/min)a •ISA m ft 5,335 17,500 5,045 16,550 4,845 15,900 4,680 15,350 •ISA +20°C m ft 4,420 14,500 4,145 13,600 3,995 13,100 3,780 12,400 Rate of climb, TOP, VY = 65 KIASa m/s ft/min 9.5 1,870 8.8 1,730 8.3 1,640 7.9 1,560 a. Preliminary performance data. kg lb 2,720 5,997 2,835 6,250 2,910 6,415 2,980 6,570 Maximum speed (VNE)a, at IAS km/h kts 259 140 259 140 259 140 259 140 Fast cruise speed (VH)a, at TAS km/h kts 257 139 255 138 253 137 252 136 Fuel consumption at fast cruise speeda kg/h lb/h 231 509 231 509 231 509 231 509 Best range speed (VBR)a, at IAS km/h kts 246 133 246 133 247 133 244 132 Fuel consumption at best range speeda kg/h lb/h 221 487 223 492 225 497 225 496 135 T3H/P3H 18.101.01 E 75 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data All Engine Operative (AEO) - Speed, Fuel Consumption, Range at 5,000 ft Pratt & Whitney Canada PW206B3, Inlet Barrier Filter (IBF) Fuel consumption at 65 KIASa kg/h lb/h 159 350 162 357 164 362 166 367 Maximum range at best range speed (no reserve)a • Standard fuel tank (560.4 kg) km NM 643 347 637 344 632 341 626 338 • Standard and long range fuel tank (730.6 kg) km NM 839 453 833 450 828 447 824 445 Maximum endurance at 65 KIAS (no reserve)a • Standard fuel tank (560.4 kg) • Standard and long range fuel tank (730.6 kg) h:min h:min 3:44 4:56 3:40 4:50 3:37 4:47 3:34 4:43 a. Preliminary performance data kg lb 2,720 5,997 2,835 6,250 2,910 6,415 2,980 6,570 kg lb 2,720 5,997 2,835 6,250 2,910 6,415 2,980 6,570 Fast cruise speed (VH)a, at TAS km/h kts 263 142 259 140 256 138 254 137 Fuel consumption at fast cruise speeda kg/h lb/h 221 487 221 487 221 487 221 487 Best range speed (VBR)a, at IAS km/h kts 222 120 222 120 224 121 224 121 Fuel consumption at best range speeda kg/h lb/h 196 432 200 441 205 452 207 456 Fuel consumption at 65 KIASa kg/h lb/h 145 320 149 328 152 335 154 340 Maximum range at best range speed (no reserve)a • Standard fuel tank (560.4 kg) km NM 711 384 700 378 693 374 685 370 • Standard and long range fuel tank (730.6 kg) km NM 937 506 922 498 913 493 904 488 Maximum endurance at 65 KIAS (no reserve)a • Standard fuel tank (560.4 kg) • Standard and long range fuel tank (730.6 kg) h:min h:min 4:04 5:23 3:59 5:16 3:55 5:12 3:52 5:07 a. Preliminary performance data The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 76 135 T3H/P3H 18.101.01 E Technical Data One Engine Inoperative (OEI) - Altitude, Rate of Climb Pratt & Whitney Canada PW206B3, Inlet Barrier Filter (IBF) One Engine Inoperative (OEI) - Maximum Gross Mass Pratt & Whitney Canada PW206B3, Inlet Barrier Filter (IBF) kg lb 2,720 5,997 2,835 6,250 2,910 6,415 2,980 6,570 Service ceiling, MCP (climb reserve 100 ft/min)a •ISA m ft 3,750 12,300 3,320 10,900 3,080 10,100 2,960 9,700 • ISA +20°C m ft 2,870 9,400 2,380 7,800 2,040 6,700 1,740 5,700 • Rate of climb, MCP, VY = 65 KIASa m/s ft/min 2.8 560 2.3 460 2.1 410 1.8 350 a. Preliminary performance data. ISA ISA +20°C Hover OGE, 30 s power (NR 100%)a kg lb 2,725 6,008 2,660 5,864 Hover OGE, 2 min power (NR 102%)a kg lb 2,710 5,975 2,515 5,545 Hover OGE, 2 min power, 10 kts headwind (NR 102%)a kg lb 2,755 6,074 2,560 5,644 Hover IGE (4 ft AGL), 2 min power (NR 102%)a kg lb 2,965 6,537 2,760 6,085 Category A - VTOL, surface level and elevateda kg lb 2,980 6,570 2,950 6,504 Category A - VTOL, short fielda kg lb 2,980 6,570 2,950 6,504 a. Preliminary performance data. 135 T3H/P3H 18.101.01 E 77 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data All Engine Operative (AEO) - Altitude, Rate of Climb Safran Helicopter Engines Arrius 2B2plus, standard air intake All Engine Operative (AEO) - Speed, Fuel Consumption, Range Safran Helicopter Engines Arrius 2B2plus, standard air intake kg lb 2,720 5,997 2,835 6,250 2,910 6,415 2,980 6,570 Hover ceiling IGE (4 ft AGL), TOP •ISA m ft 4,880 16,000 4,495 14,750 4,265 14,000 4,025 13,200 • ISA + 20°C m ft 4,025 13,200 3,595 11,800 3,352 11,000 3,065 10,050 Hover ceiling OGE, TOP •ISA m ft 4,085 13,400 3,385 11,100 2,865 9,400 2,195 7,200 • ISA +20°C m ft 3,048 10,000 2,575 8,450 2,315 7,600 1,830 6,000 Service ceiling, MCP (climb reserve 200 ft/min) •ISA m ft 5,625 18,450 5,335 17,500 5,150 16,900 4,985 16,350 • ISA +20°C m ft 4,755 15,600 4,450 14,600 4,300 14,100 4,145 13,600 Rate of climb, TOP, VY = 65 KIAS m/s ft/min 9.5 1,870 8.8 1,730 8.3 1,640 7.9 1,560 kg lb 2,720 5,997 2,835 6,250 2,910 6,415 2,980 6,570 Maximum speed (VNE), at IAS km/h kts 259 140 259 140 259 140 259 140 Fast cruise speed (VH), at TAS km/h kts 257 139 255 138 253 137 252 136 Fuel consumption at fast cruise speed kg/h lb/h 230 507 230 507 230 507 230 507 Best range speed (VBR), at IAS km/h kts 250 135 250 135 250 135 250 135 Fuel consumption at best range speed kg/h lb/h 223 492 225 495 227 500 228 503 Fuel consumption at 65 KIAS kg/h lb/h 165 363 168 370 170 374 172 378 Maximum range at best range speed (no reserve) • Standard fuel tank (560.4 kg) km NM 625 337 621 335 617 333 614 332 • Standard and long range fuel tank (730.6 kg) km NM 823 444 817 441 813 439 810 437 Maximum endurance at 65 KIAS (no reserve) • Standard fuel tank (560.4 kg) • Standard and long range fuel tank (730.6 kg) h:min h:min 3:28 4:36 3:24 4:31 3:22 4:28 3:20 4:26 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 78 135 T3H/P3H 18.101.01 E Technical Data All Engine Operative (AEO) - Speed, Fuel Consumption, Range at 5,000 ft Safran Helicopter Engines Arrius 2B2plus, standard air intake kg lb 2,720 5,997 2,835 6,250 2,910 6,415 2,980 6,570 Fast cruise speed (VH), at IAS km/h kts 263 142 259 140 256 138 252 137 Fuel consumption at fast cruise speed kg/h lb/h 226 498 226 498 226 498 226 498 Best range speed (VBR), at TAS km/h kts 230 124 230 124 230 124 230 124 Fuel consumption at best range speed kg/h lb/h 196 432 199 439 202 445 204 450 Fuel consumption at 65 KIAS kg/h lb/h 148 326 151 333 153 337 155 342 Maximum range at best range speed (no reserve) • Standard fuel tank (560.4 kg) km NM 732 395 722 390 715 386 709 383 • Standard and long range fuel tank (730.6 kg) km NM 961 519 950 513 941 508 933 504 Maximum endurance at 65 KIAS (no reserve) • Standard fuel tank (560.4 kg) • Standard and long range fuel tank (730.6 kg) h:min h:min 3:59 5:14 3:54 5:09 3:51 5:03 3:48 5:02 135 T3H/P3H 18.101.01 E 79 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data One Engine Inoperative (OEI) - Altitude, Rate of Climb Safran Helicopter Engines Arrius 2B2plus, standard air intake One Engine Inoperative (OEI) - Maximum Gross Mass Safran Helicopter Engines Arrius 2B2plus, standard air intake kg lb 2,720 5,997 2,835 6,250 2,910 6,415 2,980 6,570 Service ceiling, MCP (climb reserve 100 ft/min) •ISA m ft 4,025 13,200 3,640 11,950 3,415 11,200 3,200 10,500 • ISA +20°C m ft 3,260 10,700 2,790 9,150 2,470 8,100 2,150 7,050 Rate of climb, MCP, VY = 65 KIAS m/s ft/min 2.8 560 2.3 460 2.0 400 1.8 350 ISA ISA +20°C Hover OGE, 30 s power (NR 100%) kg lb 2,725 6,008 2,665 5,875 Hover OGE, 2 min power (NR 102%) kg lb 2,710 5,975 2,545 5,611 Hover OGE, 2 min power, 10 kts headwind (NR 102%) kg lb 2,750 6,063 2,600 5,732 Hover IGE (4 ft AGL), 2 min power (NR 102%) kg lb 2,965 6,537 2,800 6,173 Category A - VTOL, surface level and elevated kg lb 2,980 6,570 2,950 6,504 Category A - VTOL, short field kg lb 2,980 6,570 2,950 6,504 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 80 135 T3H/P3H 18.101.01 E Technical Data All Engine Operative (AEO) - Altitude, Rate of Climb Safran Helicopter Engines Arrius 2B2plus, Inlet Barrier Filter (IBF) All Engine Operative (AEO) - Speed, Fuel Consumption, Range Safran Helicopter Engines Arrius 2B2plus, Inlet Barrier Filter (IBF) kg lb 2,720 5,997 2,835 6,250 2,910 6,415 2,980 6,570 Hover ceiling IGE (4 ft AGL), TOP •ISA m ft 4,635 15,200 4,280 14,050 4,070 13,350 3,885 12,750 • ISA + 20°C m ft 3,625 11,900 3,215 10,550 2,985 9,800 2,715 8,900 Hover ceiling OGE, TOP •ISA m ft 3,930 12,900 3,385 11,100 2,865 9,400 2,195 7,200 •ISA +20°C m ft 2,745 9,000 2,345 7,700 2,025 6,650 1,830 6,000 Service ceiling, MCP (climb reserve 200 ft/min) •ISA m ft 5,565 18,250 5,275 17,300 5,090 16,700 4,875 16,000 •ISA +20°C m ft 4,665 15,300 4,390 14,400 4,205 13,800 4,055 13,300 Rate of climb, TOP, VY = 65 KIAS m/s ft/min 9.5 1,870 8.8 1,730 8.3 1,640 7.9 1,560 kg lb 2,720 5,997 2,835 6,250 2,910 6,415 2,980 6,570 Maximum speed (VNE), at IAS km/h kts 259 140 259 140 259 140 259 140 Fast cruise speed (VH), at TAS km/h kts 257 139 255 138 253 137 252 136 Fuel consumption at fast cruise speed kg/h lb/h 232 512 232 512 232 512 232 512 Best range speed (VBR), at IAS km/h kts 250 135 250 135 250 135 250 135 Fuel consumption at best range speed kg/h lb/h 225 497 227 500 229 505 230 507 Fuel consumption at 65 KIAS kg/h lb/h 166 367 169 373 171 378 173 382 Maximum range at best range speed (no reserve) • Standard fuel tank (560.4 kg) km NM 619 334 615 332 612 330 609 329 • Standard and long range fuel tank (730.6 kg) km NM 815 440 810 437 806 435 802 433 Maximum endurance at 65 KIAS (no reserve) • Standard fuel tank (560.4 kg) • Standard and long range fuel tank (730.6 kg) h:min h:min 3:26 4:33 3:22 4:29 3:20 4:26 3:18 4:23 135 T3H/P3H 18.101.01 E 81 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data All Engine Operative (AEO) - Speed, Fuel Consumption, Range at 5,000 ft Safran Helicopter Engines Arrius 2B2plus, Inlet Barrier Filter (IBF) kg lb 2,720 5,997 2,835 6,250 2,910 6,415 2,980 6,570 Fast cruise speed (VH), at IAS km/h kts 263 142 259 140 256 138 252 137 Fuel consumption at fast cruise speed kg/h lb/h 233 514 233 514 233 514 233 514 Best range speed (VBR), at TAS km/h kts 230 124 230 124 230 124 230 124 Fuel consumption at best range speed kg/h lb/h 198 437 201 443 204 450 206 454 Fuel consumption at 65 KIAS kg/h lb/h 149 328 152 335 155 342 157 346 Maximum range at best range speed (no reserve) • Standard fuel tank (560.4 kg) km NM 724 391 715 386 709 383 702 379 • Standard and long range fuel tank (730.6 kg) km NM 951 514 941 508 932 503 924 499 Maximum endurance at 65 KIAS (no reserve) • Standard fuel tank (560.4 kg) • Standard and long range fuel tank (730.6 kg) h:min h:min 3:56 5:11 3:52 5:06 3:49 5:02 3:46 4:59 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 82 135 T3H/P3H 18.101.01 E Technical Data One Engine Inoperative (OEI) - Altitude, Rate of Climb Safran Helicopter Engines Arrius 2B2plus, Inlet Barrier Filter (IBF) One Engine Inoperative (OEI) - Maximum Gross Mass Safran Helicopter Engines Arrius 2B2plus, Inlet Barrier Filter (IBF) kg lb 2,720 5,997 2,835 6,250 2,910 6,415 2,980 6,570 Service ceiling, MCP (climb reserve 100 ft/min) •ISA m ft 4,025 13,200 3,640 11,950 3,415 11,200 3,200 10,500 •ISA +20°C m ft 3,260 10,700 2,790 9,150 2,470 8,100 2,150 7,050 Rate of climb, MCP, VY = 65 KIAS m/s ft/min 2.8 560 2.3 460 2.0 400 1.8 350 ISA ISA +20°C Hover OGE, 30 s power (NR 100%) kg lb 2,725 6,008 2,665 5,875 Hover OGE, 2 min power (NR 102%) kg lb 2,710 5,975 2,505 5,523 Hover OGE, 2 min power, 10 kts headwind (NR 102%) kg lb 2,750 6,063 2,550 5,622 Hover IGE (4 ft AGL), 2 min power (NR 102%) kg lb 2,965 6,537 2,750 6,063 Category A - VTOL, surface level and elevated kg lb 2,980 6,570 2,950 6,504 Category A - VTOL, short field kg lb 2,980 6,570 2,950 6,504 135 T3H/P3H 18.101.01 E 83 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 6.2 Operating Limitations • Maximum operating altitude 6,095 m PA 20,000 ft PA • Maximum altitude for hover takeoff and landing 4,877 m DA or PA 16,000 ft DA or PA Whichever is less • Minimum air temperature -35 °C • Maximum air temperature ISA +39 °C (max. +50 °C) • Category A - Maximum takeoff and landing altitude for Clear Heliport operations 3,655 m DA or PA 12,000 ft DA or PA Whichever is less • Category A - Maximum takeoff and landing altitude for Vertical Takeoff and Landing (VTOL) 2,743 m DA or PA 9,000 ft DA or PA Whichever is less The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 84 135 T3H/P3H 18.101.01 E Technical Data 6.3 Performance Charts • Hover In Ground Effect (HIGE, TOP) with two Pratt & Whitney Canada PW206B3, standard air intake 6.3-1 • Hover In Ground Effect (HIGE, TOP) with two Pratt & Whitney Canada PW206B3, Inlet Barrier Filter (IBF) 6.3-2 • Hover Out of Ground Effect (HOGE, TOP) with two Pratt & Whitney Canada PW206B3, standard air intake 6.3-3 • Hover Out of Ground Effect (HOGE, TOP) with two Pratt & Whitney Canada PW206B3, Inlet Barrier Filter (IBF) 6.3-4 • Fuel consumption with two Pratt & Whitney Canada PW206B3 6.3-5 • Hover In Ground Effect (HIGE, TOP) with two Safran Helicopter Engines Arrius 2B2plus, standard air intake 6.3-6 • Hover In Ground Effect (HIGE, TOP) with two Safran Helicopter Engines Arrius 2B2plus, Inlet Barrier Filter (IBF) 6.3-7 • Hover Out of Ground Effect (HOGE, TOP) with two Safran Helicopter Engines Arrius 2B2plus, standard air intake 6.3-8 • Hover Out of Ground Effect (HOGE, TOP) with two Safran Helicopter Engines Arrius 2B2plus, Inlet Barrier Filter (IBF) 6.3-9 • Fuel consumption with two Safran Helicopter Engines Arrius 2B2 plus 6.3-10 135 T3H/P3H 18.101.01 E 85 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 6.3-1 Hover In Ground Effect (HIGE, TOP) with two Pratt & Whitney Canada PW206B3 Standard air intake. Figure 6.1: Hover in Ground Effect (HIGE, TOP) with two Pratt & Whitney Canada PW206B3, standard air intake The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 86 135 T3H/P3H 18.101.01 E Technical Data 6.3-2 Hover In Ground Effect (HIGE, TOP) with two Pratt & Whitney Canada PW206B3 Inlet Barrier Filter (IBF), clogged filter / bypass closed Figure 6.2: Hover In Ground Effect (HIGE, TOP) with two Pratt & Whitney Canada PW206B3, IBF 135 T3H/P3H 18.101.01 E 87 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 6.3-3 Hover Out of Ground Effect (HOGE, TOP) with two Pratt & Whitney Canada PW206B3 Standard air intake. Figure 6.3: Hover Out of Ground Effect (HOGE, TOP) with two Pratt & Whitney Canada PW206B3, standard air intake The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 88 135 T3H/P3H 18.101.01 E Technical Data 6.3-4 Hover Out of Ground Effect (HOGE, TOP) with two Pratt & Whitney Canada PW206B3 Inlet Barrier Filter (IBF), clogged filter / bypass closed Figure 6.4: Hover Out of Ground Effect (HOGE, TOP) with two Pratt & Whitney Canada PW206B3, IBF 135 T3H/P3H 18.101.01 E 89 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 6.3-5 Fuel consumption with two Pratt & Whitney Canada PW206B3 Bleed air heating off. Figure 6.5: Fuel consumption with two Pratt & Whitney Canada PW206B3, 0 - 80 KCAS The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 90 135 T3H/P3H 18.101.01 E Technical Data Figure 6.6: Fuel consumption with two Pratt & Whitney Canada PW206B3, 80 KCAS - VH 135 T3H/P3H 18.101.01 E 91 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 6.3-6 Hover In Ground Effect (HIGE, TOP) with two Safran Helicopter Engines Arrius 2B2plus Standard air Intake. Figure 6.7: Hover in Ground Effect (HIGE, TOP) with two Safran Helicopter Engines ARRIUS 2B2plus, standard air intake The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 92 135 T3H/P3H 18.101.01 E Technical Data 6.3-7 Hover In Ground Effect (HIGE, TOP) with two Safran Helicopter Engines Arrius 2B2plus Inlet Barrier Filter (IBF), clogged filter / bypass closed Figure 6.8: Hover in Ground Effect (HIGE, TOP) with two Safran Helicopter Engines Arrius 2B2plus, IBF 135 T3H/P3H 18.101.01 E 93 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 6.3-8 Hover Out of Ground Effect (HOGE, TOP) with two Safran Helicopter Engines Arrius 2B2plus Standard air intake. Figure 6.9: Hover Out of Ground Effect (HOGE, TOP) with two Safran Helicopter Engines Arrius 2B2plus, standard air intake The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 94 135 T3H/P3H 18.101.01 E Technical Data 6.3-9 Hover Out of Ground Effect (HOGE, TOP) with two Safran Helicopter Engines Arrius 2B2plus Inlet Barrier Filter (IBF), clogged filter / bypass closed Figure 6.10: Hover Out of Ground Effect (HOGE, TOP) with two Safran Helicopter Engines Arrius 2B2plus, IBF 135 T3H/P3H 18.101.01 E 95 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 6.3-10 Fuel consumption with two Safran Helicopter Engines Arrius 2B2plus Bleed air heating off. Figure 6.11: Fuel consumption with two Safran Helicopter Engines Arrius 2B2plus, 0 - 80 KCAS 96 135 T3H/P3H 18.101.01 E Blank The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data Figure 6.12: Fuel consumption with two Safran Helicopter Engines Arrius 2B2plus, 80 KCAS - VH 135 T3H/P3H 18.101.01 E 97 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 7 Service and Support Information 7.1 Assets Proven reliability and availability based on experience At Airbus, supporting customer's helicopter operations with the highest level of excellence is our priority. We have developed a strong reputation worldwide for being fully committed to providing customers with mission-efficient aircraft combining both high aircraft availability rate and cost-effective services solutions. This high level of performance has been our main target throughout the years, and therefore Airbus has stressed the importance of sharing operational feed-back with its customers to better understand their operational needs, and closely follow-up in-service Reliability, Availability and Maintainability/Testability (RAMT). The final target is to reach the most optimized operational cost while ensuring the highest flight safety. To ensure the most efficient support of these helicopters whatever the location in the world, Airbus offers: • A worldwide service network of 29 Customers Centers, more than 100 distributors, representatives, training centers, maintenance, repair and overhaul facilities • 8 logistics hubs, central & regional inventories (France, Germany, UK, Hong Kong, Australia, Mexico, Brazil and the USA) • 3 Customer Support Centers in Europe, Asia and the USA offering 24/7 customer assistance, 365 days a year • A comprehensive offer of HCare ® services: a wide array of service solutions to meet all operators' needs in terms of material management, helicopter maintenance, technical support, training & flight operations and connected services - at Airbus' facilities or at customer's location. 7.2 H135 Inspection Programs The maintenance program specifies the intervals between maintenance operations that are recommended by Airbus, irrespective of whether they are mandatory or not. The program can: • either be used as is • or be adapted by each operator to suit his own specific organization, provided he complies with the maximum intervals For the performance of scheduled and unscheduled maintenance, Airbus has classified the maintenance tasks by the following three maintenance levels: Organizational Level (O - Level) This Organizational Level (O-Level) comprises tasks such as the daily servicing, pre-flight checks, visual inspections for condition, replacement of modular components and simple repairs. This work can be performed by trained helicopter mechanics with standard tools only (no special tools necessary). Intermediate Level (I - Level) This Intermediate Level (I-Level) comprises tasks such as smaller repairs ON / OFF helicopter, periodical inspections and replacement of modular components as well as modifications. This work can be performed by trained and experienced mechanics and may require the usage of special tools and / or test equipment. The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 98 135 T3H/P3H 18.101.01 E Technical Data Depot Level (D - Level) The Level (D-Level) comprises tasks such as repairs OFF helicopter, overhaul of major components and heavy airframe repair. This work can be performed by Original Equipment Manufacturer (OEM), authorized repair centers or Airbus and requires the usage of special overhaul and repair tools, as well as test benches (if required) according to repair manuals or instructions. The following table provides an overview of all inspections. Scheduled inspections with shorter time intervals are included in those with longer time intervals. Note: All the "hands-on" aircraft values mentioned here above are given on the basis of a 20,000 FH life cycle. They refer only to the scheduled inspections for the standard helicopter without optional equipment in accordance with the Master Servic- ing Manual (MSM). The announced mean man hours are without incoming flight, work preparation, reworking, servicing, Service Bulletin (SB) implementation and unscheduled maintenance. Engine inspection programs The following table provides an overview of all engine inspections. Each inspection has to be performed for the respective time frame. Note: For further details on the engine inspections and the respective D-Level maintenance please refer to the applicable engine maintenance manual. Note: For further details on the engine inspections and the respective D - Level maintenance please refer to the applicable main- tenance manual. Scheduled airframe inspections Maintenance level Estimated mean man hours Pre-flight check O - Level 0.5 12-month inspection (max. exceedance by 3 months) I - Level 19 Intermediate inspection every 500 Fh (max. exceedance by 50 Fh) O - Level 26 Periodical inspection every 1,000 Fh or 3 years (max. exceedance by 100 Fh or 3 months) I - Level 80 Pratt & Whitney Canada PW206B3 period- ic inspections Maintenance level Estimated man hours 12-month O - Level 2 1,000 Fh O - Level 2 900 Fh Clean and test Fuel Nozzles O - Level 4 Safran Helicopter Engines ARRIUS 2B2plus periodic inspections Maintenance level Estimated mean man hours 500 Fh I - Level 2.5 1,000 Fh I - Level 10 135 T3H/P3H 18.101.01 E 99 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 7.3 Main Components Limitations 7.3.1 Airframe Main Components Time Between Overhaul (TBO) The component in question must be removed at each interval that corresponds to the value indicated, in order to undergo the operations in a specialized workshop that will enable it to be put back into service for the next interval. The given time limit may be exceeded by 3 % of the respective interval. All subcomponents may have a Service Life Limit (SLL), rated above the Time Between Overhaul (TBO) limit. Note: Non exhaustive list. Time Change Item (TCI) or Service Life Limit (SLL) A Time Change Item (TCI) is a component which has an airworthiness Service Life Limit (SLL). The affected component must be removed from service when it reaches the limit indicated. Note: Non exhaustive list. Airframe main components TBO as per MSM Rev. 23 from 2017.06.26 Fire extinguisher bottle 10 years Fuel motor pump cartridge 5,000 Fh Longitudinal actuator 7,500 Fh Lateral actuator 7,500 Fh Collective actuator 7,500 Fh Hydraulic pump 7,500 Fh Main transmission 5,000 Fh Tail rotor transmission 5,000 Fh Thermal actuator of the oil cooler bypass valve 3,000 Fh Airframe main components TCI or SLL as per MSM Rev. 23 from 2017.06.26 Fire extinguishing system cartridge 10 years Ring frame X5730 L535A1501 210 7,700 Fh Ring frame X9227 L535H2120 301 18,000 Fh Main rotor blade damper 12 years Rotor mast hub 30,000 Fh Tail rotor splined hub flange 20,000 Fh Tail rotor blade 12,000 Fh Rotor hub 27,400 Fh Tail rotor drive shaft long & coupling flange 20,000 Fh Rubber sleeve 5 years Mixing lever gear unit 30,000 Fh Collective actuator 20,000 Fh The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 100 135 T3H/P3H 18.101.01 E Technical Data 7.3.2 Engine Main Components Time Between Overhaul (TBO) The initial Time Between Overhaul (TBO) values are applicable to the engines / modules / accessories and are summarized in the tables below. Service Life Limit (SLL) Certain components of the engine, of which failures could cause a hazardous effect to the engine or its regulation, have service life limit expressed in cycles (reference flight cycle). The limited service life to which this term refers is the number of cycles that a critical part can run before having to be withdrawn from service. Note: The compressor turbine disk is commercially supported to 15,000 cycles. Note: Cycles are calculated automatically by the Engine Electronic Control Unit. Average experienced rate is about 0.5 cycles/Fh. Pratt & Whitney Canada PW206B3 overhauls TBO as per engine MM Turbo machinery module 4,000 Fh Reduction gearbox module 4,000 Fh Safran Helicopter Engines ARRIUS 2B2plus overhauls TBO as per engine MM Complete engine 4,000 Fh Accessory & reduction gearbox module (Module 01) 4,000 Fh Gas generator module (Module 02) 4,000 Fh Fuel control unit 3,500 Fh Pratt & Whitney Canada PW206B3 components SLL as per engine MM Impeller 15,000 cycles Compressor turbine disk 10,000 cycles Power turbine disk 15,000 cycles Safran Helicopter Engines ARRIUS 2B2plus components SLL as per engine MM Centrifugal impeller 20,000 cycles High pressure turbine disk 13,000 cycles Power turbine disk 14,000 cycles 135 T3H/P3H 18.101.01 E 101 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 7.4 HCare - Material Management Airbus offers its clients a comprehensive choice of material management services to ensure availability and costs control. This array of services ranges from basic Original Equipment Manufacturer (OEM) spare parts supply, repair and overhaul services up to comprehensive, "by-the-hour" support programs. The different services are tailored for different user profiles and demands, such as customers: • with a high flying hours level • with a low flying hours level • looking for immediate component availability • wishing optimal budget control To respond to the different customers' demands, Airbus offers the following services: HCare Easy: Open & seamless access to all customers under catalogue conditions • Easy Part for spare parts, components repair & overhaul and second hand parts • Easy Rental for tools and Ground Support Equipment (GSE) • Easy Repair for secured turn-around-times on components • Easy Exchange for secured availability on components HCare Smart: Performance commitment, budget control, suited to customers' needs • Repair By-the-Hour (RBH) • Exchange By-the-Hour (EBH) • Parts By-the-Hour (PBH) • Full By-the-Hour (FBH) HCare Infinite: Full availability commitment, all-inclusive turnkey solution • Fleet availability Notes: • Specific mission equipment e.g. STC´s might be excluded from above services. • Local authority regulations may have an impact on the above described material management services. Airbus would be pleased to propose further extensive services adapted to specific mission and customer expectations, such as stock and maintenance management. 7.4.1 HCare Easy HCare Easy is a classical way of material support. The material is delivered on demand when needed. It comprises spare parts, components repair & overhaul, second-hand parts, standard exchange and tool/GSE rental. The requested level of operational availability determines provisioning part quantities and therefore the required investment. With this support concept the customers bear the responsibility to monitor repairs; manage obsolescence and procure the right mix and quantity of components and spare parts to ensure availability when required. For specific lists of part numbers, Airbus has invested in dedicated stocks, and offers through Easy Repair & Easy Exchange services, secured turn-around-times, or secured parts availability for standard exchange. The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 102 135 T3H/P3H 18.101.01 E Technical Data 7.4.2 HCare Smart Repair By-the-Hour (RBH) The RBH service offers guaranteed repair & overhaul turn-around-times as well as guaranteed prices. This service enables the customer to best size its own inventory of repairable parts, and better schedule its helicopter maintenance while keeping property of its material. The price for this service is calculated per flight hour, thus enabling the customer to spread and predict component scheduled and unscheduled maintenance expenses. The RBH service includes component unscheduled third level repairs (Depot Level maintenance), component scheduled overhauls, life-limited part replacement as well as mandatory modification kits (to the extent covered by the RBH contract). This service is available for dynamic components, blades, basic and optional equipment (covered optional equipment list to be defined with the customer). Exchange By-the-Hour (EBH) With the Exchange-By-the-Hour (EBH) service, Airbus offers the customer an immediate part replacement, and a controlled budget for unscheduled maintenance while remaining responsible for the scheduled events (overhaul, life limited parts replacement). Price for this service is calculated per flight hour. The EBH service includes component unscheduled third level (Depot Level maintenance) repairs and guaranteed parts delivery within 24 hours FCA (Incoterms 2010) through Standard Exchange based on a dedicated inventory. This service is available for dynamic components, blades, basic and optional equipment (covered optional equipment list to be defined with the customer). Parts By-the-Hour (PBH) The Parts-By-the-Hour (PBH) service is a comprehensive program that offers and balances at the same time guaranteed maintenance costs for both scheduled and unscheduled events, reduced inventory and minimized helicopter downtime. This service is intended for customers looking for optimized cost control and high level of aircraft readiness. Price for this service is calculated per flight hour. The PBH service includes component unscheduled third level (Depot Level maintenance) repairs; component scheduled overhauls as well as Life Limited Part replacement. Parts delivery is guaranteed within 24 hours FCA (Incoterms 2010) through Standard Exchange based on dedicated inventory. This service is available for dynamic components, blades, basic and optional equipment (covered optional equipment list to be defined with the customer). Full By-the-Hour (FBH) The Full By-the-Hour (FBH) service is an extension of the PBH service including the supply of non- repairable parts such as consumables and hardware. This service is intended for customers looking for total cost control and high level of aircraft readiness. Price for this service is calculated per flight hour. 135 T3H/P3H 18.101.01 E 103 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 7.4.3 HCare infinite The HCare Infinite program provides customers a fleet availability commitment from Airbus. It is a turnkey solution, adapted to various customers' needs, enabling them to focus on flights while Airbus takes care of supporting the fleet. The program comprises material support, logistics management and technical services. It can be extended to helicopter maintenance and airworthiness management. Price for this service is usually calculated per flight hour. 7.4.4 A complementary Initial Provisioning of Spare Parts and Tools Within that range, Airbus provides a customized initial provisioning package. It includes spare parts, tools, test equipment, etc.to sustain helicopter operations for a defined initial period of time. The dimensioning of the package is tailored according to the number of helicopters, operational bases, flight hours per year and requested availability. 7.4.5 Logistics Assistance Upon request, Airbus can propose an on-site logistics assistance through a Logistics Field Representative (LFR) detached at customer premises or near the operational base, to optimize logistics flows back and forth. Thanks to unrivalled knowledge of internal processes and logistics tools / network, the LFR is the privileged interface between the customer and Airbus. The LFR is able to assist the customer on material and inventory management, logistics forecasting, order administration and will report on the logistics activities. 7.4.6 Airbus Aircraft-On-Ground (AOG) Service Airbus provides a twenty four hours a day/seven days a week and three hundred and sixty five days per year (24/7/365) AOG service to guarantee an efficient service and respond quickly to any AOG situation. An Aircraft-On-Ground (AOG) service is available for spare orders. The order placed by the customer shall cover an actual failure (and not a scheduled maintenance shortage) and may consist of up to 3 items per grounded aircraft listed in the Illustrated Parts Catalogue (IPC), except main assemblies, raw materials, ingredients and hazardous material. In the case of direct part availability, the parts will be immediately delivered under CIP (Incoterms 2010) conditions to the nearest international airport with delivery times dependent on the region and export license requirements (normally 48 to 72 hours). The AOG Department is responsible for answering to the following customer requests 24/7/365: • 1st level troubleshooting and diagnosis assistance • Part ordering with immediate information on part availability • Part delivery, delivery of repair solution (even temporary) or any possible service to put helicopter back to flight line. The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 104 135 T3H/P3H 18.101.01 E Technical Data 7.5 Engine Service and Support Programs 7.5.1 Pratt & Whitney Canada (PWC) A vast menu of services offered through the P&WC customer service network P&WC's worldwide facilities offer you a full menu of reliable and high-quality after-market engine services. These services include: • Engine repair and overhaul • Hot Section Inspections (HSI's) • Customized work scopes • Component repairs • Accessory repairs and overhauls • Pay-per-hour programs including both Fleet Management Programs (FMP®) and the Eagle Service™ Plan (ESP®) Program for the corporate and general aviation market • Rental and exchange engines • New spare engine sales • Fleet Enhancement Program (FEP) where you exchange your core engine for a new engine of the same model at an attractive price providing all the associated benefits of a new engine • Used serviceable engine sales • Mobile Repair Team (MRT) support with over 200 teams available • On-wing inspections • Trouble-shooting, 24-hour AOG support and technical assistance through our C-First Centre • Providing serviceable and exchange parts from the largest pool in the industry • Diagnostics, Prognostics and Health Management, providing you with an integrated solution for acquiring, downloading, and analyzing crucial aircraft and engine performance data for predictive maintenance and performance optimization • OEM Engineering support Fleet Services- Simplifying engine maintenance and financial planning P&WC's Fleet Services business unit offers "pay-per-hour" programs for both the airline and corporate markets. The airline program is entitled the Fleet Management Program (FMP®), while the corporate program is entitled the Eagle Service™ Plan (ESP®). The objective of both programs is to establish a steady, simplified engine management and financial planning tool that will guarantee operating costs tailored to suit your individual requirements. With close to 8,000 Pratt & Whitney Canada engines already enrolled on "pay by the hour" programs, the industry demonstrated its confidence on the advantages of the following services, as described hereafter. 135 T3H/P3H 18.101.01 E 105 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data Eagle Service™ Plan (ESP®) The Eagle Service Plan (ESP) is a "pay per the hour" engine maintenance budget plan designed for the operators of select Pratt & Whitney Canada (P&WC) engine models. The PW206 Series ESP program offers two engine maintenance budget plans designed to suit individual operator needs. The coverage options for each plan are listed on the P&WC website: www.pwc.ca. The ESP program virtually eliminates the risk of high cost surprises and engine maintenance expenses become much more predictable. Other advantages include transferability on resale to subsequent operators and renewability at the end of the contract term. Fleet Management Program (FMP®) This FMP program is a customized engine maintenance and service coverage vehicle which provides a guaranteed operating cost and can be tailored to suit individual coverage and payment requirements. P&WC offers two types of coverage and two types of FMP plans: Basic engine coverage • Engine major refurbishment/overhaul • Hot Section Inspection • Basic unscheduled engine removals • ECTM analysis Optional coverage: • Fuel nozzles • Rental Engine support • Accessory BUR repairs • Up front exchange for accessories • Life limited parts replacement • Engine diagnostics (Aircraft Data Acquisition System) • Many others.. This program allows customers to focus on their core business and provide operational optimization reduce the overhead and logistical issues associated with operating a maintenance facility. When an agreement is signed, a P&WC Customer Manager is appointed to provide all the essential coordination and support required to ensure customer satisfaction. MyPWC power customer portal MyP&WC Power is tailored to the needs of all customers - from fleet owners and operators, to individual aircraft operators, to administrators. The portal is simple to use yet powerful in its ability to manage a comprehensive array of transactions. The customer portal provides customers with a variety of applications to facilitate day-to-day transactions with P&WC. The Warranty & Commercial Support application provides customers with electronic claiming options, as well as additional Warranty information resources. Technical publications are also posted on the P&WC customer portal, offering customers instantaneous updates. Customer can view or download engine documentation in the moment it is published, create and customize indices, search for bulletins based on a multitude of criteria, view the status of their technical publications with the simple click of a mouse. In addition, customers can easily find, order, track and pay for parts and tech pubs; initiate engine rentals and returns; submit Eagle Service Plan® (ESP) hours - all from their computer, smartphone or tablet. 7.5.2 Safran Helicopter Engines Always careful to maximize the efficiency of your operations and reduce your costs, Safran Helicopter Engines, the engine manufacturer has developed and improved its service offering. The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 106 135 T3H/P3H 18.101.01 E Technical Data Safran Helicopter Engines puts at customers' disposal 32 Repair Centers across the globe, supplemented by several new factory-authorized service facilities strategically located near customer's operations. Safran Helicopter Engines range of services covers: • Classical Repair and Overhaul • Standard Exchange • AOG services • By-the-Hour services Within the By-the-Hour coverage, Safran Helicopter Engines developed specific maintenance packages, as summarized hereafter. Safran Helicopter engines Global Support Package (GSP®) For military and parapublic missions, the aircraft must be operational at any time. Safran Helicopter Engines GSP service includes an extensive range of options that can be tailored to customers' needs. To bring more reliability, safety and availability while controlling budget and cost, Safran Helicopter Engines proposes to forge a real partnership through four service packages: • Equipment availability and stock optimization: To control key parameters to reach results on stock optimization and availability equipment. • Up to Depot Level maintenance (from Level 2 to 4): To manage engine maintenance from level 2 to 4, with flying hours invoicing and guaranteed prices. • Financial solutions: To bring visibility and help to finance operational needs. • Support of "O" Level maintenance: To facilitate "O" Level maintenance execution. Safran Helicopter engines Support By the Hour (SBH®) Safran Helicopter Engines SBH is a comprehensive service for civilian missions, providing financial and operational coverage for engine support. • To customers choice, it can cover scheduled as well as unscheduled events, limiting exposure to unexpected expenses. • Customer "pay as customer flies": SBH provides a fixed cost per engine flight hour. It is directly linked to customers' flight activity. One SBH, many solutions: Safran Helicopter Engines SBH is one single name and concept offering flexible and standard combinations between 4 dimensions: • Coverage: scheduled and/or unscheduled events, with flexibility on some engine components. Complete engine or modular maintenance. • Availability: pool access option with standard exchange or rental • Logistics: a choice of transport solutions • Finance: different payment terms, contract duration SBH was made to be tailored to customer exact needs. Safran Helicopter Engines SBH benefits: • Predictability: Control of budget and smooth of engine maintenance costs: expenses are clear and predictable • Flexibility: Safran Helicopter Engines SBH offers total modularity, to cover customers' exact needs • Insurance: scheduled and/or unscheduled coverage, with risks partially transferred to Safran Helicopter Engines • Availability: effective replacement solutions including Standard Exchange, available through Safran Helicopter Engines' worldwide pool 135 T3H/P3H 18.101.01 E 107 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data • Win-win: contractual commitments on hourly rates and lead times • Visibility: clear view of combinations and options Safran Helicopter engines operator online support (tools) Customers‘ feedback has also allowed Safran Helicopter Engines to greatly improve tools, a website dedicated to operator support. Safran Helicopter Engines Operator On Line Support is a fully interactive website developed and programmed specifically for customer support needs. A portion of the site is available to anyone seeking information regarding customer support services and activities. The other portion of the site is exclusively available to clients, providing a wealth of information and services, such as: • Technical Publications • Direct communication access with the needed resources • On-line training • A clear overview of all other Safran Helicopter Engines services such as second hand engines and warranty • ... and much more to serve customers 7.6 HCare - Helicopter Maintenance 7.6.1 Aircraft Maintenance, Repair & Overhaul (MRO) Airbus proposes a complete range of industry-leading Maintenance, Repair & Overhaul (MRO) solutions such as: inspection, repair and overhaul capabilities for the full range of Airbus product range, with optimized turn-around-times and cost-efficiency. Approved by the most stringent airworthiness authorities in the world, Airbus industrial facilities ensure the highest quality for the maintenance and repair actions of customers' fleet. Works are performed by our teams of specialized and duly qualified technicians which technicity has been built on long and diverse field experience on the worldwide fleet. Airbus can perform the work within its facilities around the world or at customer premises. 7.6.2 On-Site Assistance When requested, Airbus teams of skilled field service technicians provide the customer with world- class support and enhanced services for aircraft maintenance, repairs and retrofits at customer's premises. As part of this service Airbus technicians will bring the required parts and tools to carry out the maintenance, repair and upgrade tasks on site. The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 108 135 T3H/P3H 18.101.01 E Technical Data 7.6.3 Upgrades Airbus proposes tailored solutions to increase customers‘ helicopter overall performance and reduce its maintenance cost, contributing to harmonized fleet or role/mission change, the better to be prepared for missions. Upgrades maintain aircraft at the latest version, benefitting from innovations and advanced technology, perfectly adapted to customers‘ aircraft configuration and defined by Airbus experienced design office teams. The portfolio of AH Standard Upgrades is available on customer portal Keycopter, allowing direct order of kits or request of customized quotation. The set of upgrades is regularly updated. This portfolio proposes number of equipment that may be installed on helicopters after delivery from Airbus Helicopters in order to fulfil specific operational needs or aircraft upgrades. These equipment are either designed and certified by Airbus Helicopters as SB (Service Bulletin) or by Airbus Helicopters customer centers or third parties as STC‘s (Supplementary Type Certificate). Please note that some constraints may exist between optional equipment. Technical confirmation by an Airbus Helicopters sales representative is recommended before submitting any purchase order. 7.7 HCare - Technical Support 7.7.1 Technical Assistance An Airbus Technical Representative can be detached at customers' base to perform On-the-Job Training and ensure an efficient and safe start of the operations. The on-site Technical Representative covers mainly the following activities: • Daily relationship interface with the customer • Aircraft assistance (explanation for usage of special maintenance tools and equipment) • Troubleshooting (assistance in solving technical events and management of the process from the diagnosis up to the solution) • Interface with Airbus mother company (engineering support) • Contribution to fleet technical knowledge management • Local day-to-day recommendations to optimize the customer maintenance efficiency • Safety (analysis of events in case of minor or major incidents to identify airworthiness impact) 7.7.2 Technical Expertise 24/7 Airbus will provide technical knowledge dedicated to your helicopters, aimed at supporting the safe and reliable operations of the aircraft. A team of highly skilled engineers in close and daily relation with design office is committed to answer any technical question. This group is also in charge to establish technical improvements, recommendations for use, customer information (Service Bulletins, Information Notices…), and is the focal point of contact for technical relation with Airbus. Any technical question can be raised 24 hours/7 days, through our toll free number or our Keycopter website for organizations using the internet (eRequests function). 7.7.3 Continuing Airworthiness Management (CAM) Services Airbus consulting & training services improve operational performance of customers' fleet. Such services can be complemented by CAM services offering diagnosis up to full implementation of a full airworthiness follow-up organization. 135 T3H/P3H 18.101.01 E 109 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 7.7.4 eTechPub Airbus provides the technical publications required for safe operations and cost-effective maintenance. Airbus technical publications are available on Keycopter® portal within eTechpub service. An interactive electronic browser, O.R.I.O.N, is available. O.R.I.O.N. includes the maintenance and identification information and contains at minimum • Aircraft Maintenance Manual (AMM), • System Description Section (SDS), • Master Servicing Manual (MSM), • Illustrated Parts Catalog (IPC), • Wiring Diagram Manual (WDM), • Structure Repair Manual (SRM), • Standard Practices Manual (SPM/MTC). The technical publications are available in English. They include the latest information and are regularly updated. Keycopter /eTechpub also provide access to the List Of Applicable Publications / Status Revision Documentation (LOAP/SRD), Flight Manual (FLM), Pilot's Check List (PCL) and Master Minimum Equipment List (MMEL). Along with Keycopter / eTechpub, Airbus provides a hard copy of: • Flight Manual, • Master Minimum Equipment List (MMEL), • Pilots-Checklist, • Logbooks, • Historical Record. The delivery of hard copies may be cancelled without further notice in case of changes to the legal requirements. As chargeable option, the technical publications are also available on PDF format on Keycopter portal. When online solutions do not fit to user constraints, physical means may be proposed as chargeable options: • O.R.I.O.N. light on USB Key, same content than O.R.I.O.N on line but with a reduced set of functions • O.R.I.O.N. full on USB Key, same content than O.R.I.O.N on line but as local network solutions (full functionalities) • Hard copies Selected Component Maintenance Manuals (CMM) are available on PDF format: • On Keycopter / eTechpub as Online Component Maintenance Manual (OCMM), • On USB key as Electronic Component Maintenance Manual (ECMM). The engine documentation is provided by the engine manufacturer. The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 110 135 T3H/P3H 18.101.01 E Technical Data 7.7.5 Technical Information Publication on Internet (T.I.P.I.) The Technical Information Publication on Internet (T.I.P.I.) website is entirely dedicated to provide a real-time issuing service for the following publications: • Service Bulletin (SB), Alert Service Bulletin (ASB), Emergency Alert Service Bulletin (EASB), Service Letter (SL), Information Notice (IN), Safety Information Notice (SIN), Technical Information Letter (TIL), Flight Operations Briefing Note (FOBN), • Master Minimum Equipment List (MMEL), • Technical Improvement Proposal (TIP), • Revisions of Flight Manual (FLM). The T.I.P.I. application is now also available for tablets and smartphones. The T.I.P.I. application for smartphones and tablets can be downloaded free of charge by following the link: http:// www.airbushelicopters.com/techpub/ or in a mobile equipment application stores (Apple store, Play Store - formerly Android Market, etc.). Main features • Each time one of the above listed publications is issued, the customer is automatically informed by an e-mail. • A small summary, already included in the e-mail, helps the customer to quickly understand the subject. • Small icons allow the customer to immediately identify the type of information received. • The download of the publication in PDF format is possible after logging on the T.I.P.I. website. • A keyword search tool is provided (aircraft family, type of publication, date of edition, etc.). • Address: www.airbushelicopters.com/techpub The publications are available in English. 7.8 HCare - Training & Flight Ops Training With over 50 years of experience, the Airbus helicopter training centers provide the world's leading helicopter training for pilots and technicians, whether civilian or military. Since 2011, a completely new blended learning process based on interactive learning with the latest technology for theoretical and practical instruction is implemented. The instruction team is composed of experts in their fields with the utmost operational experience and knowledge. Although a lot of things have changed in the past 50 years Airbus major goal remains unchanged: to stand up to customers' expectations and to contribute decisively to flight safety. The course catalogue is designed to cover the full range of customers' training needs. Nevertheless, Airbus can also provide customers' organization with the most effective training solution tailored to customers' demand. The high quality of Airbus training courses is assured by a very strict internal quality system and regular audits by national authorities (EASA, FAA, DGAC, LBA, CAA, CAAC…). The main training centers are certified to issue certificates according to EASA Part 147 and Part FCL. Airbus has set up a network of 24 helicopter training centers and 23 Full Flight Simulators (FFS) all over the world. Centers are equipped with multimedia classrooms. This includes computers overhead projectors and state-of-the-art means such as Computer Aided Instruction (CAI), Computer Based Training (CBT) or instructor lead presentation. 135 T3H/P3H 18.101.01 E 111 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data Basic H135 training course Note: Training duration and content are given as information and depend on pilot or technician qualification or experience and the configuration of the aircraft. Complementary courses may be required. For detailed information refer to: http://www.helicopters.airbus.com/website/en/ref/Training-&-Flight-Ops_72.html Engine training courses Training courses dedicated to engine maintenance are organized by the engine manufacturer´s training schools and approved centers all over the world. COURSE TYPE COURSE REFERENCE THEORETICAL INSTRUCTION FLIGHT INSTRUCTION Pilots Type Rating VFR 3 weeks 10 Fh COURSE TYPE COURSE REFERENCE THEORETICAL AND PRACTICAL INSTRUCTION Technicians Airframe Type rating B1.3 5 weeks Avionic Type Rating B2 4 weeks The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 112 135 T3H/P3H 18.101.01 E Technical Data 7.9 Flight Operations Services This set of services activities aims at answering all operational related constraints and issues met by pilots and operations departments. 7.9.1 Pilots Assistance (on site) Through on-site pilot assistance, Airbus provides customers' pilots complementary knowledge on their new helicopter and also on how to master the associated mission systems and equipment in customer's specific operational environments. Available for civil and military operations, it is built according to customer's specific needs and is held at customer's desired location. This pilot assistance can be provided at helicopter delivery, and also upon request at any time. 7.9.2 Crew Help Desk (on-line support) The Crew Help Desk provides answers to queries relative to best knowledge and operation of the helicopter among e.g. regulations, aircrew publications, aircraft limitations, performance, procedures/ operations and systems. The Crew Help Desk support is ensured through the worldwide Airbus network. This service is provided free of charge. Any question can be raised 24/7 through our toll free number or our Keycopter website for organizations using the internet (eRequest function). 7.9.3 Pilots Check-list - PCL - (Operational Documentation) The PCL presents abbreviated standard operating procedures based on the helicopter flight manual (FLM) or the Flight Crew Operating Manual (FCOM). The PCL does not replace nor supersede the current FLM/FCOM. It is updated in accordance with the corresponding FLM/FCOM revisions when applicable. The PCL is provided in PDF/paper format, in English language. 7.9.4 Flight Ops Briefing Note - FOBN - (Operational Documentation) Customers Flight Ops Department publishes on Customer or Internal request briefing note to address Fleet Safety and Ops Procedures needs. The FOBN are distributed free of charge on T.I.P.I. 7.9.5 Flight Crew Operating Manual – FCOM - (Operational Documentation) The FCOM is issued as a guideline for operators to develop their own Standard Operating Procedures in accordance with applicable requirements. It is designed for a specific model, type of operation and configuration. In any case, the approved Flight Manual remains the only official document with regards to certification authorities. 7.9.6 Safety Management System (SMS) Services A Safety Management System (SMS) is a structured approach to safety management, which encompasses the organizational structures, responsibilities, policies and procedures necessary in order to ensure safe operations of a company. Airbus Helicopters International Services (AHIS) consulting division can support the introduction of SMS in Customer's organization. AHIS consulting experts have extensive operational and technical knowledge and can provide practical solutions tailored to customer's needs. 135 T3H/P3H 18.101.01 E 113 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 7.10 HCare - Connected Services Two families of essential service package (available online or locally) accessible through Keycopter website and/or the e-Apps Apple store: 7.10.1HCare Flight For efficient flight preparation •Flight Planner: Airbus all-in-one portable Electronic Flight Bag for mission planning on ground and mission execution in flight, running on rugged windows tablet. •Flight Perfo: separate iOS app for Performance computation •Flight Balance: separate iOS app for Weight and Balance computation 7.10.2HCare fleet More dedicated to support maintenance operations and for a smarter fleet management. •Fleet Keeper application: The full e-solution by Airbus for your Technical Log Book linking Flight Operations, Airworthiness and Maintenance Crew (mobile and Web-based). • Monitor & control fleet status in real-time • Record flight reports • Manage technical events •Envision nGen: Airbus trusted solution for aviation management. Powerful all-inclusive software developed for operators in need of a complete Maintenance Information System. This tool is customizable across various modules, and covers any activity related to helicopter operations. 7.10.3HCare for Helionix With eAvionics Airbus proposes a set of system and software services: System and configuration management services: • Support, services or tools related to the system & software configuration management • The configuration management of the loadable/configurable equipment is fully managed in the technical documentation (Technical Logbook, IPC, SB). Loading and logistic services: • Spare & repair (preloaded equipment) • Customer software loading package (loading tool, documentation, training, software distribution). The loading tool provides customers with autonomy for loading/configuring their equipment. • Equipment loading service in Airbus network • Equipment loading by Airbus at customer premises Software maintenance services: • Airbus proposes software maintenance services consisting in regular maintenance releases. The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 114 135 T3H/P3H 18.101.01 E Technical Data Failure Management (Diagnosis & eDynamic Troubleshooting) An online tool accessible via Keycopter which shall help you solve any observed issues with the H/C in a quick and efficient manner. The failure codes recorded within Helionix are available via the online Diagnosis Report and/or Helionix Maintenance Page. The eDynamic Troubleshooting helps to isolate the root cause, either by using the failure codes, or by looking for symptoms. Prerequisite to use the diagnosis report is a data exchange with Airbus via the MGS. Full offline eDynamic Troubleshooting: for customers not able to share their aircraft data via the MGS and /or having no web access, an offline version of the eDynamic Troubleshooting is available on request. Aerodata This service provides databases and tools for the following enhanced awareness functions of Helionix hosted in the Multi-Functional Display (MFD): • Helicopter Terrain Awareness and Warning System (H-TAWS) • Moving Map (DMAP) • Synthetic Vision System (SVS) 135 T3H/P3H 18.101.01 E 115 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data 8Abbreviations Abbreviation Meaning AAT Air Ambulance Technology AC Alternating Current ACP Audio Control Panel ACS Air Conditioning System ACU Audio Control Unit ADELT Automatic Deployable Emergency Locator Transmitter ADF Automatic Direction Finder ADS-B Automatic Dependent Surveillance Broadcast AEL Aerolite AEO All Engines Operating AFCS Automatic Flight Control System AFT Aft AGL Above Ground Level AHDL Airbus Helicopters Data Loader AIS Automatic Identification System AM Amplitude Modulation AMC Aircraft Management Computer AMLCD Active Matrix Liquid Crystal Display AMM Aircraft Maintenance Manual ANR Active Noise Reduction AOG Aircraft On Ground ARIS Anti-Resonance Isolation System ARP Aerospace Recommended Practice AS Aerospace Standard ASB Alert Service Bulletin ATC Air Traffic Control BFE Buyer Furnished Equipment BMR Bearingless Main Rotor BUL Bucher Leichtbau BUR Basic Unscheduled Removals CAA Civil Aviation Authority CAAC Civil Aviation Administration of China CAI Computer Aided Instruction Cat. A Category A CBT Computer Based Training CCP Cockpit Control Panel CECG Corrosion and Erosion Control Guide CIP Carriage Insurance Paid (Incoterms 2010) CMM Component Maintenance Manual CMP Continuous Maintenance Program COM Communication CS Certification Specifications CVFDR Cockpit Voice and Flight Data Recorder The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 116 135 T3H/P3H 18.101.01 E Technical Data CVR Cockpit Voice Recorder D - Level Depot Level DA Density Altitude DACS Digital Audio Communication System DGAC Direction Générale de l‘Aviation Civile DMAP Digital Moving Map DMC Direct Maintenance Costs DME Distance Measuring Equipment DO Design Order DOC Direct Operating Costs DP Dual Pilot DTD Data Transfer Device DVCS Digital Voice Control System EASA European Aviation Safety Agency EASB Emergency Alert Service Bulletin EBH Exchange By the Hour ECMM Electronic Component Maintenance Manuals ECP Event Cost Plan ECTM Engine Condition Trend Monitoring EFH Engine Flight Hour ELRS External Life Raft System ELT Emergency Locator Transmitter ELT(S) Survival Emergency Locator Transmitter EMS Emergency Medical Services EOS Electro Optical System EPNdB Effective Perceived Noise level Decibel EPNL Effective Perceived Noise Level ERS Enhanced Reality System ES Extended Squitter ESP Eagle Service Plan FAA Federal Aviation Administration FADEC Full Authority Digital Engine Control FAR Federal Aviation Regulations FBH Full By the Hour FCA Free Carrier (Incoterms 2010) FCL Flight Crew License FCOM Flight Crew Operating Manual FDCR Flight Data Contiuous Recorder FDS Flight Display Subsystem Fh Flight Hour FLI First Limit Indicator FLIR Forward Looking Infra Red FLM Flight Manual FM Frequency Modulated FMP Fleet Management Program FND Flight and Navigation Display Abbreviation Meaning 135 T3H/P3H 18.101.01 E 117 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data FNPT Flight and Navigation Procedures Trainer FOBN Flight Operations Briefing Note FOV Field Of View FWD Forward GPS Global Positioning System GS Ground Speed GSE Ground Support Equipment GSM Global Systems Mobile GSP Global Support Package H/C Helicopter HD High Definition HEELS Helicopter Emergency Egress Lighting System HEMS Helicopter Emergency Medical Service HF High Frequency HFDM Helicopter Flight Data Monitoring HICAMS Helicopter Intensive CAre Medical Service HIGE Hover In Ground Effect HMI Human Machine Interface HMS Health Monitoring System HOGE Hover Out of Ground Effect HSI Hot Section Inspection H-TAWS Helicopter Terrain Awareness and Warning System HUMS Health and Usage Monitoring System I - Level Intermediate Level IAS Indicated Air Speed IBF Inlet Barrier Filter ICAO International Civil Aviation Organisation IESI Integrated Electronic Stand-by Instrument IFR Instrument Flight Rules IGE In Ground Effect ILS Instrument Landing System IMU Inertial Measurement Unit IN Information Notice IPC Illustrated Parts Catalog IR Infrared ISA International Standard Atmosphere (15 °C at SL) KIAS Knots Indicated Air Speed LARS Lightweight Aircraft Recording System LBA Luftfahrt Bundesamt LCF Low Cycle Fatigue LED Light Emitting Diode LFR Logistics Field Representative LH Left Hand LN Luftfahrt-Norm (Aviation Standard) LNAV Lateral Navigation LOAP List Of Applicable Publications Abbreviation Meaning The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 118 135 T3H/P3H 18.101.01 E Technical Data LPV Localizer Performance with Vertical Guidance LTE Long Term Evolution Max. Maximum MCP Maximum Continuous Power MFD Multi-Function Display MGS Maintenance Ground Station MKR Marker MMEL Master Minimum Equipment List MRO Maintenance, Repair and Overhaul MSM Master Servicing Manual MTOW Maximum Take Off Weight MWIR Mid-Wave Infrared NAA National Aviation Authority NAV Navigation NR Rotor Speed NVG Night Vision Goggle NVIS Night Vision Imaging System O - Level Organizational Level O.R.I.O.N. Optimized Reader for Internet and Other Networks OAT Outside Air Temperature OCMM Online Component Maintenance Manual OEI One Engine Inoperative OEM Original Equipment Manufacturer OGE Out of Ground Effect OPS Operations PA Pressure Altitude PAX Passenger PBH Parts By the Hour PC Personal Computer PCL Pilot's Check List PFD Primary Flight Display PGS Professional Ground Station PNG Polycon New Generation PTT Push To Talk PWC Pratt & Whitney Canada R/D Rate of Descent RAMT Reliability Availability Maintainability/Testability RBH Repair By the Hour RDR Radar REU Remote Electronic Unit Rev. Revision RH Right Hand RIA Retractable Interface Adapter RNP Required Navigation Performance RPM Revolutions Per Minute RTCA Radio Technical Commission for Aeronautics Abbreviation Meaning 135 T3H/P3H 18.101.01 E 119 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data SAE Society of Automotive Engineering Safran HE Safran Helicopter Engines SAR Search And Rescue SAS Stability Augmentation System SB Service Bulletin SBAS Satellite Based Augmentation System SBH Support By the Hour SDS System Description Section SII Staged Intermediate Inspection SIN Safety Information Notice SL Sea Level SL Service Letter SLL Service Life Limit SMS Safety Management System SPM Standard Practices Manual SRM Structure Repair Manual STANAG Standardization Agreement STC Supplemental Type Certificate SVS Synthetic Vision System SWAT Special Weapons And Tactics T.I.P.I Technical Information Publication on Internet TAS Traffic Advisory System TAS True Air Speed TBO Time Between Overhaul TCI Time Change Item TCP Term Cost Plan TIL Technical Information Letter TIP Technical Improvement Proposal TLB Technical LogBook TOOLS Safran Helicopter Engines Operator On-Line Support TOP Takeoff Power TOT Turbine Outlet Temperature TQ Torque TV Television UK United Kingdom ULM Ultra Low Maintenance UMS Usage Monitoring System UMTS Universal Mobile Telecommunications System USB Universal Serial Bus VBR Best Range Speed VDC Volt Direct Current VFR Visual Flight Rules VH Maximum Horizontal Speed VHF Very High Frequency VMS Vehicle Management System VNAV Vertical Navigation Abbreviation Meaning The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. 120 135 T3H/P3H 18.101.01 E Technical Data VNE Never Exceed Speed VOR VHF Omnidirectional Radio Range VOX Voice Operated Exchange VTOL Vertical Take Off and Landing VY Best Rate of Climb Speed WDM Wiring Diagram Manual Abbreviation Meaning 135 T3H/P3H 18.101.01 E 121 The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data Manufacturer´s Notes This document provides general information on the description, specification, weights, dimensions and performance data of helicopters manufactured by Airbus Helicopters and on related services and support. Depending on the exactly selected configuration and/or the respective mission profile, these data may vary. For specific, individual performance data and operating limitations reference shall be made to the approved flight manual and all appropriate documents. The operational or certification regulations, as defined by competent local authorities, may require as compulsory the installation of some of the recommended or further available equipment as listed in this document, with present document however not being meant to be comprehensive in terms of all worldwide operational requirements. The operator shall be responsible to clarify with its respective local authorities that any potential configuration of the helicopter complies with the regulatory requirements for the area of operation and/or type of mission. The Airbus Helicopters product policy aims at continuous product improvements. Therefore Airbus Helicopters reserves the right to make data changes at any time without any notice being given with reference to present issue of this document. The depicted images (i.e. photos, 3D-pictures, general drawings, diagrams or similar) are for illustration purposes only. The facts and figures contained in this document and expressed in good faith shall not constitute any offer from or the acceptance of an offer leading to a contract with Airbus Helicopters. Airbus Helicopters‘ logo, H135®, Helionix®, Fenestron®, HUMS®, HCare®, Keycopter® and Stylence® are registered trademarks of Airbus Helicopters.l 122 135 T3H/P3H 18.101.01 E Blank The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents. This document is the property of Airbus Helicopters®; no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed. © Airbus Helicopters® 2018 – All rights reserved. Technical Data © AIRBUS HELICOPTERS, Aeroport International Marseille Provence - 13725 Marignane Cedex - France - 2018 - All rights reserved Airbus Helicopters’ logo and the names of its products and services are registered trademarks. Airbus Helicopters reserves the right to make configuration and data changes at any time without notice. The facts and figures contained in this document and expressed in good faith do not constitute any offer or contract with Airbus Helicopters. Designed by AIRBUS HELICOPTERS Photos: AIRBUS HELICOPTERS Cover photo: © Airbus Helicopters, Guillaume Plisson, 2017 Printed by SPI (France) 135 T3H/P3H 18. 101 .01 E Exhibits A Declaration Statement & Conflict of Interest Affidavit B H135 2018 Technical Data Book C Collier County HCare Presentation This Page Intentionally Left Blank H135HLX Support Program 2018 What is HCare? HCare is the Airbus brand for all Support Services •Material Management •Helicopter MRO & Upgrades •Training & Flight Operations •Technical Support •Connected Services Material Management consisting of 3 Service Levels •Easy Parts Comprehensive catalog of parts. Airbus commitment to deliver 100% on time for orders placed 15 days in advance. •Easy Repair Secured performance. You will receive a part by the end of the committed repair cycle. •Easy Exchange Gives you access to a dedicated stock of spare parts. •Easy Rental Rent out a part for a defined period, saving time and ensuring readiness. HCare Smart is the promotional name for Airbus Contracted Service Plans Benefits: •Guaranteed customer commitments •Relieves customer of inventory costs •Levels cost of operation •Improved aircraft residual value With HCare Smart Without HCare Smart Material Management: •Parts by Hour (PBH) •Exchange by Hour (EBH) •Repair by Hour (RBH) •Consumables by Hour (CBH) •Full by Hour (FBH) •Shipping •Consignment Spares Pay by the Hour Service Options Contracted Services Commitment HCare Commitment •Scheduled overhauls Delivery 10 days before removal •AOG events Delivery within 24hr •Unscheduled events (Rush) Delivery within 7 days H135HLX – Parts By the Hour (PBH) Airbus Helicopters TC’d Basic and Optional Equipment Covers Primary Cost Drivers •Defined List of Parts •Basic Equipment •Dynamics •Blades •Avionics •Note: Factory Optional Equipment (in addition to the basic, blades and dynamics, defined list of parts) may be covered at an additional cost •Examples……AC, ADELT, CVFDR, HEELS, IBF, Radar, Hoist, etc. Scheduled and Unscheduled events H135HLX – Exchange By the Hour (EBH) Covers Primary Cost Drivers •Defined List of Parts •Basic Equipment •Dynamics •Blades Covers Unscheduled Events Only •No reserve for TBO or SLL parts Like PBH except no reserve for scheduled TBO or SLL Airbus Helicopters TC’d Basic and Optional Equipment H135HLX – Repair By the Hour (RBH) Repair of: •Dynamic Components •Blades •Basic & Mission Equipment •Repairable Parts •Non-Repairable Parts (defined list) Recommended for Operators: •With a large Inventory •Wishing to keep their own material Airbus Helicopters TC’d Basic and Optional Equipment H135HLX – Consumables By the Hour (CBH) Consumables By the Hour (CBH) cover parts not included in PBH (Defined list of parts Basic, Dynamics, Blades, Avionics) •Consumables By the Hour (CBH) •$250 deductible •Extended CBH •$0 deductible •CBH must be combined with PBH Airbus Helicopters TC’d Basic and Optional Equipment H135HLX Additional Support Options •Consignment Spares* •Spares placed at customer location •Shipping* •Parts to customer •Cores back to Airbus * Additional Charge at customers expense Airbus Helicopters TC’d Basic and Optional Equipment H135HLX – Full By the Hour (FBH) FBH is an enhanced program combining PBH and CBH covering the aircraft “nose-to-tail” FBH Options: •PBH + CBH = Full By the Hour (FBH) •PBH + Extended CBH = Extended Full By the Hour (FBH) Full By the Hour is the combination of •Parts By the Hour (Defined List of Parts) •Consumables By the Hour (CBH) OR •Extended Consumables By the Hour (Extended CBH) Airbus Helicopters TC’d Basic and Optional Equipment H135HLX – CBH/FBH Coverage Parts with a unit price over $250 (or $0 if Extended CBH), examples…. •Relays / Switches, Antennas •Windshield & Windows (other than exclusions) •Doors •Lights •Clamps, Valves •Detectors •Power supply •Pipes, Flexibles, Cooling fans •Tanks •Filters •Airframe parts Airbus Helicopters TC’d Basic and Optional Equipment H135HLX – PBH/CBH/FBH Exclusions PBH/CBH/FBH does not cover damages resulting from: •Misuse or abuse •Lack of reasonable care •Damage due to force majeure or natural forces •Abnormal corrosion •Inadequate repairs performed by user •Excessive cycle consumption (+4 Cycles per Hour) •Unjustified Removal and/or return of Core Unit without prior approval of the Seller •Unusual wear and tear •Incorrect maintenance, handling and storage condition •Return of incomplete core unit •Non repairable core unit •Part lost by the buyer Minimum of 100 Flight Hours H135HLX – CBH/FBH Exclusions •Batteries (unless specifically covered) •Extinguishers (except if specifically covered in the contract) •Raw materials •Lubricants •Paints •Label, Tape and adhesives •Non mandatory Service Bulletins •Parts with a unit price less than $250 (unless covered by Extended CBH) •3rd level parts •Wear and tear items (seat covers, seat belts, flooring, coverings) Airbus Helicopters TC’d Basic and Optional Equipment •Non AH/AHD parts such as Engine and Engine parts •Customization, STC, non-authorized parts •ITAR restricted parts weapons •Tools and GSE and related parts •Crew Equipment •Mission equipment •Life Vest & Raft •Floats (unless covered by optional PBH) •Medical Interiors •Interior furnishings Parts with a value of $5,000 or greater value may be subject to AH prior approval What is NOT covered under CBH/FBH? H135HLX Support Program Pricing Options Parts By the Hour (PBH) Option A PBH – (minimum coverage) In Warranty Rate/HR Out of Warranty Rate/HR PBH – Basic Equipment $69.11 $115.19 PBH – Dynamics $84.39 $140.65 Total $153.50 $255.84 Option B PBH – (traditional) PBH – Basic Equipment $69.11 $115.19 PBH – Dynamics $84.39 $140.65 PBH – Blades $10.91 $18.19 Total $164.42 $274.03 *2018 Conditions, sub-group pricing Minimum Package = Basic + Dynamics PBH Per Defined List of Parts Includes a 3% discount to Collier County H135HLX Support Program Pricing Options Parts By the Hour (PBH) Option C PBH – (Avionics) In Warranty Rate/HR Out of Warranty Rate/HR PBH – Basic Equipment $69.11 $115.19 PBH – Dynamics $84.39 $140.65 PBH – Blades $10.91 $18.19 PBH – Avionics $63.29 $105.49 Total $227.71 $379.51 *2018 Conditions, sub-group pricing Minimum Package = Basic + Dynamics PBH Per Defined List of Parts Includes a 3% discount to Collier County H135HLX Support Program Pricing Options Full By the Hour (FBH) Option D FBH – ($250 deductible) In Warranty Rate/HR Out of Warranty Rate/HR PBH – Basic Equipment $69.11 $115.19 PBH – Dynamics $84.39 $140.65 PBH – Blades $10.91 $18.19 PBH – Avionics $63.29 $105.49 CBH – Consumables By The Hour – ($250 deductible) $36.38 $60.63 Total $264.08 $440.14 *2018 Conditions, sub-group pricing Minimum Package = Basic + Dynamics PBH Per Defined List of Parts Includes a 3% discount to Collier County H135HLX Support Program Pricing Options Full By the Hour (FBH) Option E FBH – ($0 deductible) In Warranty Rate/HR Out of Warranty Rate/HR PBH – Basic Equipment $69.11 $115.19 PBH – Dynamics $84.39 $140.65 PBH – Blades $10.91 $18.19 PBH – Avionics $63.29 $105.49 CBH – Consumables By The Hour – ($0 deductible) $54.56 $90.94 Total $282.27 $470.45 *2018 Conditions, sub-group pricing Minimum Package = Basic + Dynamics PBH Per Defined List of Parts Includes a 3% discount to Collier County H135HLX Support Program Pricing Options Exchange By the Hour (EBH) Option F EBH – (minimum coverage) In Warranty Rate/HR Out of Warranty Rate/HR EBH – Basic Equipment, Dynamics, Blades $61.23 $244.93 Option G EBH + Avionics EBH – Basic Equipment, Dynamics, Blades $61.23 $244.93 EBH – Avionics $62.29 $105.49 Total $124.52 $350.41 *2018 Conditions, sub-group pricing Minimum Package = Basic + Dynamics EBH Per Defined List of Parts, Unscheduled Events Only Includes a 3% discount to Collier County H135HLX Support Program Pricing Options Exchange By the Hour (EBH) Option H EBH + Avionics ($250 deductible) In Warranty Rate/HR Out of Warranty Rate/HR EBH – Basic Equipment, Dynamics, Blades $61.23 $244.93 EBH – Avionics $62.29 $105.49 CBH – Consumables By The Hour – ($250 deductible) $36.38 $60.63 Total $160.90 $411.04 *2018 Conditions, sub-group pricing Minimum Package = Basic + Dynamics EBH Per Defined List of Parts, Unscheduled Events Only Includes a 3% discount to Collier County H135HLX Support Program Pricing Options Exchange By the Hour (EBH) Option I EBH + Avionics ($0 deductible) In Warranty Rate/HR Out of Warranty Rate/HR EBH – Basic Equipment, Dynamics, Blades $61.23 $244.93 EBH – Avionics $62.29 $105.49 CBH – Consumables By The Hour – ($0 deductible) $54.56 $90.94 Total $179.09 $441.35 *2018 Conditions, sub-group pricing Minimum Package = Basic + Dynamics EBH Per Defined List of Parts, Unscheduled Events Only Includes a 3% discount to Collier County 135HLX PBH COVERAGE Assembly Part Number Qty. Electrical Power System SPC-10(HD)1 Electrical Power System 409CH2 1 Electrical Power System 4504-300-6 1 Electrical Power System 4503-350-4 1 Electrical Power System 4502-350-4 1 Electrical Power System 23081-073 2 Engine Controls 200-150 1 Engine Indicating L771M40C1031 1 Equipment/Furnishings L331M5861101 1 Fuel System B13000 4 Fuel System 10271-13-0 1 Fuel System L284M30C1005 2 Fuel System L284M30C1006 2 Fuel System B25B00 2 Fuel System L281M20C1015 1 Fuel System L281M20C1012 1 INDICATOR TRIPLE RPM CHARTHOLDER PILOT DRAIN VALVE FILLER PLUG FUEL SENSOR MAIN TANK FUEL SENSOR SUPPLY TANK FUEL SHUT OFF VALVE MAIN TANK SUPPLY TANK BASIC PACKAGE Component INVERTER BATTERY 40AH 'SAFT' BATTERY MASTER BOX ELECTRIC MASTER BOX 1 FULL OPT. ELECTRIC MASTER BOX 2 FULL OPT. STARTER GENERATOR (200A) INTERFACE CONTROL UNIT (PILOT) 135HLX PBH COVERAGE Assembly Part Number Qty. HEATING SYSTEM JBS880-3 1 HEATING SYSTEM JBS13016-10 1 HEATING SYSTEM JBS881-1 1 Hydraulic Power System L290M20A1014 2 Hydraulic Power System L290M20A1017 2 Hydraulic Power System L293M00C1002 2 ICE AND RAIN PROTECTION L304M2806101 1 ICE AND RAIN PROTECTION L304M2003103 1 INDICATING AND RECORDING SYSTEMS B18-945.22.28.1.A 1 INDICATING AND RECORDING SYSTEMS C19243BC09 1 INDICATING AND RECORDING SYSTEMS B19030GC09 1 INDICATING AND RECORDING SYSTEMS 0129N 1 INDICATING AND RECORDING SYSTEMS L311M1075108 1 INDICATING AND RECORDING SYSTEMS L315M5002051 1 Lights 4000020-002 1 Lights LRA15 1 BASIC PACKAGE Component CAD VEMD OAT-SENSOR SWITCH UNIT 20VE WARNING UNIT ASSY COCKPIT LIGHT ASSY DC-CONVERTER MIXING VALVE BLOWER VENTILATION CONTROL BOX HYDRAULIC PUMP HYDRAULIC VALVE BLOCK, RESERVOIR PRESSURE SWITCH, HYDRAULIC GEARBOX WINDSHIELD WIPER ARM CLOCK 135HLX PBH COVERAGE Assembly Part Number Qty. Lights 2LA455359-00 1 Lights 0230191-001 1 Lights 03-9500-4001 1 Lights 03-9200-2006 1 Lights 2LA455358-00 1 Navigation 501-1228-03 1 Navigation 501-1849-01 1 Navigation C17133AA01 1 Navigation 5A58.32.18K.28.4.BH 1 Navigation 3A43.32.20F.28.4.EE 1 Navigation 621396-231 1 Oil Cooling System Z0513001 1 Oil Cooling System L792M3004105 1 Oil Cooling System L792M3005105 1 Power Plant L713M2077101 1 Power Plant L713M2078101 1 BASIC PACKAGE Component MAGNETIC COMPASS OIL COOLER OIL COOLER FAN LH OIL COOLER FAN RH INLET CHANNEL LH (P/W) INLET CHANNEL RH (P/W) LED ANTI-COLLISON LIGHT LED TAIL POSITION LIGHT RED POSITION LIGHT (NVG) EMERGENCY POWER SUPPLY STAND-BY HORIZON AI-804DC AIR DATA UNIT (ADU 3200) AIRSPEED INDICATOR 2" ALTIMETER 2" GREEN POSTION LIGHT (NVG) L&S LIGHT 250 W 135HLX PBH COVERAGE Assembly Part Number Qty. Rotor Flight Control L673M40A1003 1 Rotor Flight Control 76CF8716 1 Rotor Flight Control L673M20A1012 1 Rotor Flight Control L673M20A1011 1 Rotor Flight Control L673M20A1008 1 Rotor Flight Control L671M3013102 1 Rotor Flight Control L671M7001220 1 Rotor Flight Control L671M3009104 3 Rotor Flight Control L671M3012102 1 Rotor Flight Control L671M7003104 1 Rotor Flight Control L671M3011103 2 Rotor Flight Control 15-9932P 1 Rotor Flight Control 15-9931P 1 Navigation 5A58.32.18K.28.4.BH 1 Navigation 3A43.32.20F.28.4.EE 1 Navigation 621396-231 1 BASIC PACKAGE Component LINK ASSY RH AIRSPEED INDICATOR 2" ALTIMETER 2" MAGNETIC COMPASS LATERAL AXIS ACTUATOR LONGTIDUAL AXIS ACTUATOR BEARING BLOCK ASSY BOLT CONTROL ROD FORKED LEVER ASSY HINGED SUPPORT LEVER LINK ASSY LH FENESTRON SERVO ACTUATOR FLEXIBLE BALL CABLE FENESTRON COLLECTIVE AXIS ACTUATOR 135HLX PBH COVERAGE Assembly Partnumber Qty. MAIN BLADES L621M1001205 8 MAIN BLADES L621M1003110 8 MAIN BLADES L621M1010059 4 MAIN BLADES 11-10097P 4SPHERICAL BEARING BLADE PACKAGE Component BLADE BOLT DAMPER ELASTOMERIC MRB 135HLX PBH COVERAGE Component Partnumber Qty. CHIP DETECTOR 1D1772-1 1 MAIN DRIVE SHAFT 19E293-1A 2 FREE WHEEL CLUTCH 4649 202 002 2 MGB L632M1130101 1 OIL TEMPERATURE SENSOR TM004 1 PRESSURE SWITCH L634M60C1001 2 PRESSURE TRANSDUCER ZRB378-00 1 SPEED PICK UP 4-301-062-02 1 TEMPERATURE SWITCH 800101E00010100 1 TORQUE STRUT L633M1001104 2 Z-ARIS L633M2010109 4 ROD BODY L671M20V1002 4 Main Rotor Drive Main Rotor Drive Main Rotor Drive Main Rotor Drive Main Rotor Drive Main Rotor System DYNAMIC PACKAGE Assembly Main Rotor Drive Main Rotor Drive Main Rotor Drive Main Rotor Drive Main Rotor Drive Main Rotor Drive 135HLX PBH COVERAGE Component Partnumber Qty. ROD END ASSY BO L671M20V1004 4 ROD END ASSY UP L671M20V1005 4 HELICAL LEVER ASSY L623M4003102 2 HELICAL TUBE ASSY L623M4002104 2 MAIN ROTOR MAST ASSY L623M1231101 1 SWASHPLATE - BOLT (SLIDING SLEEVE L623M2006213 2 SWASHPLATE - CONTROL RING L623M2001215 1 ROTOR RING ROT-EURO-6 1 SENSOR AMPLIFIER UNIT SV-EURO-5 1 SIGNAL PROCESS UNIT AW-EURO-5 1 STATOR ANTENNA ANT-EURO-6 1 FENESTRON BLADE ASSY L642A2002101 10 DYNAMIC PACKAGE Assembly REAR BLADES Main Rotor System Main Rotor System Main Rotor System Main Rotor System Main Rotor System Main Rotor System Main Rotor System Main Rotor System Main Rotor System Main Rotor System Main Rotor System 135HLX PBH COVERAGE Component Partnumber Qty. HUB BODY L642A2003102 1 PITCH CHANGE SPIDER ASSY L642A2004101 1 SPLINED FLANGE L642A2019201 1 TENSION TORSION STRAPS 350A33318000 10 COUPLING FLANGE L651M2008220 2 FLEXIBLE COUPPLING L651A1001101 4 RUBBER SLEEVE L651M1008218 6 SHAFT CFK (AFT)L651M2010101 1 SHAFT CFK (FRONT)L651M2012101 1 SHAFT LONG ASSY L651M2008101 1 INPUT FLANGE L652A2006203 1 TGB L652A0000053 1 DYNAMIC PACKAGE Assembly Tail Rotor Drive Tail Rotor Drive Tail Rotor Drive Tail Rotor Drive Tail Rotor Tail Rotor Tail Rotor Tail Rotor Tail Rotor Drive Tail Rotor Drive Tail Rotor Drive Tail Rotor Drive 135HLX PBH COVERAGE Component Partnumber Qty. AFCS 3 & 4 AXES 261104913-1001 1 AFCS 3 & 4 AXES 261104913-2001 1 AFCS 3 & 4 AXES 261104921-6001 1 AFCS 3 & 4 AXES 704A47135071 2 AFCS 3 & 4 AXES 704A47135072 4 AFCS 4 AXES 261104921-7001 1 AFCS 4 AXES 704A47135072 1 AMC PLATFORM (HELIONIX)X422C10A1003 2 IMA DATA TRANSFER DEVICE (HELIONIX) X429C40A1003 1 MFD PLATFORM (HELIONIX)X423C10A1002 3 AHRS 261500123-0460 3 AHRS 420-00339-000 2 INTEGRATED ELEC STANDBY INSTRUMENT (IESI) (HELIONIX) X342C50A1001 1 Navigation Navigation Auto Flight System Auto Flight System Auto Flight System Auto Flight System IMA PLATFORM AND MODULES IMA PLATFORM AND MODULESIMA PLATFORM AND MODULES Navigation AVIONICS PACKAGE Assembly Auto Flight System Auto Flight System Auto Flight System Important to you. Essential to us.