H175. Technical Data 2018 HELICOPTERS

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1 H175 Technical Data 2018 HELICOPTERS

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3 Contents 1 Foreword General Characteristics Cockpit and Cabin Layouts Weight Power Ratings Fuel Capacities External Dimensions Internal Dimensions Enhanced Level of Safety Superior Passenger Comfort Baseline Aircraft Definition Mission Configurations Offshore Transportation Public Services Favorite Private & Business Aviation Main Performance Aircraft Performance Operating Limitations Performance Charts Support & Services Material Management Helicopter Maintenance Technical Support Training and Flight Operations Connected Services Abbreviations B E 1

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5 1 Foreword Since its Entry Into Service (EIS) in December 2014, the super-medium H175 has proven its capabilities, on all over the world (Europe, Asia, America and Africa) in Offshore transportation and VIP missions with over 25,000 flight hours logged from Passenger comfort, high safety, superior performance and low pilot workload are key characteristics of the H175. As a result, a high availability rate has been achieved thanks to an exceptional maturity assured through a rigorous development process. Designed in collaboration with major Oil & Gas (O&G) and Public Services operators, the H175 responds to the most demanding markets expectations will be the year of Public Services delivery. The H175 exceeds the requirements of the latest and most demanding regulation (certification standard CS-29) and International Oil & Gas Producer (IOGP) guidelines. Its first Type Certification was delivered by the European Aviation Safety Agency (EASA), DGAC Mexico, Russian FATA-AR, Brazilian ANAC, Australian CASA and subsequent certification validation processes are in progress with the Federal Aviation Administration (FAA), as well as Transport Canada (TCCA). Certification for flight in limited icing conditions was obtained and deployed. With high cruise speed, high payload and mission flexibility combined with its competitive operational cost the H175 offers the best economic solution in the new super medium class. 175 B E 3

6 In each area the H175 offers key advantages and operational benefits: H175 has the highest ratio of payload to MTOW. In addition, the mass extension to 7,800 kg brings an extra 300 kg of payload. Operational mission range/endurance flexibility with a single aircraft configuration thanks to an unrivalled standard fuel tank capacity of over 2,000 kg. Smooth flight at 160 kt (Fast cruise speed) with no Active Vibration Control System required Superior performance: Very high performance allowing Performance Class 1 (PC1) take-off and landing procedures. Safe hoisting operations with possible use of Extended Power duration (TOP rating up to 30 min continuous within a cumulative duration of 50 min per flight) and the high super emergency power OEI 30 s (> 2,000 shp) which can be combined with the OEI 2 min (> 1,900 shp) for a cumulative duration of 2 min 30 s. High payload thanks to an optimized design and a low mission equipped empty weight. APU mode enabled through left engine declutching; no payload impact, no APU additional costs. Helionix cockpit communality offers our multi-platform customers with training credits. Helionix is now embedded on H135, H145, H175 as well as the H160 in the near future. Unique flight envelope protection and pilot assistance, shared on all Helionix cockpits and inherited from the H225 s best in class AFCS and Human Machine Interface. This includes safety features such as First Limit Indicator (FLI), Localizer Performance with Vertical guidance LPV, Rig N Fly automatic approach, TCAS II coupled with the autopilot, recovery modes in case of pilot disorientation and Control Flight Into Terrain prevention. Offshore favorite configuration includes Rig N Fly, LPV, SVS, HUMS, HFDM, alerting system and failure management, HTAWS, TCAS II, ADSB-out and the latest Airbus avionics suite, Helionix; intuitive, reducing pilot workload and increasing safety. Gear box capability of 30 min following oil loss has already been demonstrated. An extension of this test duration is planned in 2018 with the objective of publishing a 30 min limitation in the H175 Flight Manual. Optimum comfort with the largest cabin and volume per passenger: the H175 offers a capacity of up to 18 crashworthy seats. The cabin arrangement presents seat rows with a maximum of 4 seats per row, avoiding unsafe and uncomfortable 5 seats per row configurations. Largest egress surface per passenger with extra-large windows. HCare provides comprehensive customer support solutions adapted for H175 material management. Providing easier and safer means for managing flight preparation, Airbus HCare Flight proposes two new Apps for H175 Weight & Balance and Performance. These Apps available for ipad provide safe operational limits and flight manual performance accounting for specific mission profiles, payload and optional equipment. The Flight Crew Operating Manual (FCOM) developed specifically for flight crews, provides all necessary information about operational, technical, procedural and performance characteristics required for safe and efficient aircraft operation. Comprehensive training and support services available for customers prior to aircraft delivery. This includes a certified Level-D Full Flight Simulator B E

7 Thanks to its high performance and versatility the H175 addresses a wide range of missions: Offshore transportation with the possibility to add Public Services equipment Public Services, including, Search and Rescue (SAR) Law enforcement EMS & MEDEVAC Private & Business Aviation Offshore transportation Configured for Offshore transportation missions the H175 provides the ideal balance between passenger transport and Radius of Action (RoA). To widen their mission scope, Oil & Gas operators can select and benefit from SAR mission equipment with the ability to perform quick role change Public Services operations. In an EASA OPS mission profile (Offshore configuration), ISA+20 C conditions, the H175 achieves the following performance with a MTOW of 7,800 kg: 12 passengers up to 218 NM radius of action (RoA) 16 passengers up to 162 NM radius of action (RoA) 18 passengers up to 130 NM radius of action (RoA) The H175 performances are EASA certified for Class 1 helideck operations down to 16 m of D-value and even 12 m with quite small take-off weight restriction. Also, some 16 m North Sea platforms are already approved. Public Services For Public Services missions, the H175 is the most capable in its class satisfying customer mission requirements both inshore and out at sea. It provides the longest range/endurance capability with more than 2,000 kg of standard fuel tank capacity. Inherent multi-role capabilities enable a rapid transformation based on mission requirements. The large cabin volume with direct cabin access to the rear cargo compartment and long cabin with a flat floor ensures high multi-mission flexibility for SAR, law enforcement and MEDEVAC as well as EMS missions. For Public Service missions, the primary equipment proposed on the H175 is the inbuilt chin mounted Electro- Optical System (EOS) for observation and tracking, along with an enhanced Digital Map display, both managed by the crew or from an operator console in the cabin To ensure multi-mission flexibility specific mission equipment can be configured such as dual hoists, searchlight, external loud hailers and steerable external lighting. Furthermore, the H175 highly capable autopilot incorporates advanced modes for search and rescue operations. 175 B E 5

8 Private & Business Aviation To differentiate its approach to Private & Business Aviation, Airbus Helicopters introduces ACH Airbus Corporate Helicopters its exclusive brand offering end to end service-based ownership experience. ACH provides an exclusive platform from which customers can benefit from best in class Corporate and VIP transport solutions, tailored completion and service. ACH ensures that only the highest quality materials and the best craftsmanship are on offer to customers. ACH range now features the ACH prefix: ACH125, ACH130, ACH135, ACH145, ACH160 ACH175. and Please visit our dedicated website: Working with Pegasus Design in creating the ACH175 VIP versions, Airbus brings a superior level of creativity and luxury to the cabin interiors. The refinement and level of quality incorporated by Pegasus Design are a result of their inherent understanding of high-end customer expectations. VIP mission benefits from the ACH175 s fast cruise speed, very low sound and vibration levels. The large windows, efficient Environmental Control System including air conditioning with APU mode (left engine declutch) provide unrivalled passenger comfort. Developed with the longest cabin in its class, the ACH175 offers a unique cabin layout with two seating areas accommodating from seven to twelve passengers in VIP configuration B E

9 Supporting helicopter operations with the highest level of excellence and the best proximity is Airbus priority. Airbus is dedicated to meet customer needs whatever the mission is: A worldwide service network of 30 subsidiaries and participations, more than 100 distributors, representatives, training centers, repair and overhaul facilities and maintenance centers around the globe, as well as logistic hubs in France, Hong Kong and the USA. Customer Service Centers in Europe, Asia and the USA offering around-the-clock customer assistance, 7 days a week, 365 days a year to keep H175 in the skies. Airbus proposes a wide array of proven service solutions to meet all customer requirements such as standard exchange, field and office support. In addition new services have been developed: failure management, interactive electronic technical publications, system and software support. Taking advantage of Airbus long and unique experience on after-sales, the support of the H175 model has been tailored with operators, for operators. Its flexibility assures customer operational needs are met, and it incorporates many new features clearly opening the path towards a new helicopter generation. 175 B E 7

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11 2 General Characteristics 2.1 Cockpit and Cabin Layouts Minimum crew VFR IFR Passenger transportation Single / dual pilot Single (optional) / dual pilot Up to 16 passengers (standard Offshore configuration) 18 passengers (optional) Public Services Up to 18 passengers Cabin operator console Stretchers EMS equipment Private & Business Aviation ACH Line ACH Exclusive Up to 16 passengers Up to 12 passengers 2.2 Weight Empty Weight Equipped in Offshore Transportation configuration: Offshore transportation mission configuration ( CI) (1) kg lb 4,717 10,399 Empty Weight Equipped in Public Services configuration: Public Services mission configuration ( CI) (1) With dedicated SAR mission equipment (2) 5,026 11,080 With dedicated Law Enforcement mission equipment (3) 4,727 10,421 Empty Weight Equipped in ACH Line configuration for 11 passengers: ACH Line configuration ( CI) and 11 passengers cabin layout ( CI) (1) 4,599 10,139 Empty Weight Equipped in ACH Exclusive configuration for 7 passengers: ACH Exclusive configuration ( CI) and 7 passenger cabin layout ( CI) (1) 5, Maximum all-up weight 7,800 17,196 Maximum load on cargo sling 2,700 6,393 (1) Including engine oil and unusable fuel, excluding airborne kit (2) For details please refer to (3) For details please refer to General note: Empty weight accuracy: within ± 2 % 175 B E 9

12 2.3 Power Ratings 2 Pratt & Whitney PT6C-67 E turboshaft engines All Engines Operative (AEO) kw shp Take-Off Power (TOP) / Extended Power (EP) 1,324 1,775 Maximum Continuous Power (MCP) 1,227 1,645 One Engine Inoperative (OEI) kw shp OEI 30 s 1,541 2,067 OEI 2 min 1,422 1,907 OEI Continuous Power 1,347 1,806 Note: Thermodynamic values per engine in standard atmosphere at sea level 2.4 Fuel Capacities Standard fuel tanks with ground pressure refueling (equipment included in the standard mission configurations) Standard fuel tanks with gravity refueling Usable Fuel liters US gal kg lb 2, ,067 4,555 2, ,001 4, B E

13 2.5 External Dimensions 175 B E 11

14 2.6 Internal Dimensions Dimensions in Offshore Transportation Configuration Floor area Volume Cockpit 2.0 m² 21.5 ft² 3.2 m ft 3 Passenger cabin 8.0 m² 86.1 ft² 12.0 m ft 3 Luggage hold 3.1 m² 33.4 ft² 2.3 m ft B E

15 2.7 Enhanced Level of Safety H175 Cockpit Safety The H175 advanced Helionix avionics suite combines innovation with proven technologies for enhanced safety, situation awareness and mission capacity together with reduced pilot workload through an intuitive, ergonomic and simplified maintainability: A full glass cockpit with integrated avionics: the Helionix Flight Display Subsystem (FDS) is composed of 4 High Definition Smart Multi-Function Displays (MFD): 6 x 8 Active Matrix Liquid Crystal Displays (AMLCD) encompassing LED technology Innovative concept with perfect readability from any angle and light condition A fully integrated dual duplex 4 axis autopilot; unrivalled pilot assistance and flight envelope protection. This most advanced autopilot system is specifically derived from the reference H225 autopilot and fully integrated in the avionics system. Specially designed for helicopters, it offers unique pilot assistance with integrated automatic modes such as: High flight stability and precision from hover up to VNE Unique flight envelope protection (aircraft, MGB and engine protection over the full flight envelope and a Controlled Flight Into Terrain (CFIT) protection) Automatic take-off procedure Automatic management of engine failure during cruise, take-off and hover (automatic goaround procedure) New AFCS Modes including: Automatic Rig approach, Rig N Fly Ground Trajectory Control (GTC) with auto hover acquisition and distance to stop Flight Path Angle (FPA) Ground slope whatever the wind TRacK angle hold (TRK) Upper modes dedicated to SAR missions: automatic transition to and from hover, ground speed acquisition, etc A pilot friendly interface to enhance pilot situational awareness 175 B E 13

16 Smart HMI Design keeping it simple, clean & clear with no overhead panel A high level of system redundancy: dual duplex aircraft management computers, 3 inertial sensors, plus one Integrated Electronic Stand-by Instrument (IESI) and one backup SAS An automatic extensive Built In Test An innovative crew alerting system A centralized radio management system on the two Flight Management Systems with back-up Integrated and redundant DMAP, HTAWS, Synthetic Vision System An Integrated Health and Usage Monitoring System (UMS, HMS and FDCR) H175 Passenger Safety Equipped with oversized emergency exits the H175 offers the largest egress surface per passenger: 4 emergency exits on each side of the cabin with a surface exceeding "Type IV" size requirements 1 3 or maximum of 4 passengers per row with each passenger being at one seat maximum from an emergency exit Sea state 6 certified emergency flotation gear that can be manually inflated in flight or automatically at ditching: High waterline floatation for higher stability preventing helicopter capsizing External life raft integrated in cabin footsteps 1 Type IV = 480 mm x 660 mm (19 inch x 26 inch), as indicated in red on the above picture B E

17 High performance Pratt & Whitney PT6C-67 E engine The PT6C-67 E is the latest evolution of the proven Pratt & Whitney PT6C engine family. The PT6C-67 E offers: High performance providing H175 with CAT-A / PC1 performance for safe operations: High super emergency power OEI 30s with up to 2,067 shp OEI 2 min with up to 1,907 shp Extended power rating (Take off Power, TOP): 30 min continuous within a cumulative duration of 50 min per flight Dual channel FADEC Improved fuel efficiency Declutch capability of left engine offering APU mode on ground High safety with high pressure turbine blade melting and power turbine blade shedding Pneumatic fire detection system - higher reliability and larger detection zone In flight power check The engine installation is optimized to ease maintenance; short exhaust limiting thermal impact and facilitating access to engine components and accessories. 175 B E 15

18 2.8 Superior Passenger Comfort Thanks to a very long, open cabin and full flat floor, the H175 offers the best in class comfort and volume per passenger. The cockpit is accessible through 2 lateral doors with footsteps. Passengers access the cabin via two large sliding doors and long footsteps. With five seat rows, each seat position is close to a large window, providing every passenger with an excellent external visibility. Comfort is reinforced thanks to a very low vibration level ensured by design and without any need of Active vibration Control System, up to maximum speed. Two independent Environmental Control Systems with regulated air conditioning system ensure an efficient regulation/ventilation of the cabin and cockpit with individual outlets for crew & passengers. The large cargo compartment is easily accessible from both sides. Loading is further eased by an integrated and deployable step ladder. For Public Service layouts, a direct access is possible from the cabin. The cargo compartment volume is always available for cargo; no need for auxiliary fuel tank thanks to the tremendous H175 standard fuel tank capacity B E

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20 3 Baseline Aircraft Definition B E

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23 4 Mission Configurations The H175 is a safe, reliable, powerful and versatile helicopter able to perform a wide spectrum of missions such as Passenger transportation, Offshore transportation, Public Services including Search and Rescue, EMS, law enforcement mission as well as Private & Business Aviation missions. For these missions, Airbus proposes dedicated mission equipped configurations. The subsequent chapters describe the following Favorite configurations for: Offshore Transportation Public Services ACH Line & ACH Exclusive The proposed mission equipped configurations are established by Airbus based on extensive years of experience in helicopter development. Furthermore, the H175 benefits from the experience and feedback of operators and customers around the world through Customer Advisory Team meetings performed at the early stages of the H175 development. With the H175, customers benefit from a state of the art helicopter that complies with current operational and regulation requirements. Each configuration encompasses basic equipment common for all missions, combined with an integrated avionics and radio suite (with a dual FMS installation), an efficient environmental control system, and a Health and Usage Monitoring System and FDCR ensuring a high safety level. This is known as the Mission Configuration. These dedicated mission configurations can be customized thanks to an extensive list of optional equipment proposed for each mission. The final configuration is therefore: mission configuration + additional mission equipment. 175 B E 21

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25 4.1 Offshore Transportation The H175 in Offshore Transportation configuration is designed to carry 16 passengers in unrivalled security and comfort over long ranges. Its high power level including Class I performance for helideck ensures safe operations. The H175 offers the highest volume per passenger in supermedium class ensuring superior comfort and rapid egress capability. The Offshore mission configuration integrates additional, dedicated equipment for offshore operations such as Rig N Fly and LPV approach capability, TCAS II and ADSB-out. An optional 18 passenger configuration is also proposed. This comfortable seat arrangement has a maximum of 4 seats per row. Each passenger is at most 1 seat distance from an emergency exit. 175 B E 23

26 4.1.1 Offshore Transportation Configuration Document reference Commercial reference Description kg lb A CI Offshore Transportation Mission Configuration 4,717 10, A CI H175 Baseline Aircraft On request as per 175 B E A CI Customized external polyurethane paint scheme A CI First aid kit - EASA OPS compatible A CI De-clutching system A CI Windshield washer A CI Cargo compartment step ladder (on RH side door) A CI Dual-zone regulated air conditioning system A CI DC emergency electrical generator A CI Ground pressure refuelling On request A CI Airworthy mooring rings for moderate weather A FP Goodrich Category 1 electrical 28VDC hoist (290ft, 600lb) - Fixed Parts A FP Cargo sling - Fixed Parts A CI HID retractable and swiveling front LH landing light On request A CI Tail fin video camera A CI Cockpit video camera with embedded recorder A FP Tail skid video camera - Fixed Parts A FP Emergency floatation gear - Fixed Parts On request A RP Emergency floatation gear - Removable Parts On request A FP External RFD liferafts installation (2*12 pax) (including PLB space provisions) - Fixed Parts A RP External RFD liferafts installation (2*12 pax) (including PLB space provisions) - Removable Parts A CI Helicopter Emergency Egress Lighting (HEEL) A CI HR Smith serie ADELT with GPS connection A CI 16 energy absorbing seat cabin layout B CI Comfort cabin lining A CI VHF/AM Rockwell-Collins VHF-4000 n A CI VHF/AM Rockwell-Collins VHF-4000 n A CI NAT - NPX138 VHF/FM-H A FP Wireless intercom system Telephonics Trulink (rescuer communication) - Fixed Parts A CI NAT DACS ICS - Basic set: 2 control panels in cockpit A FP NAT DACS ICS - Control panel on right side of the cabin - Fixed Parts A CI NAT 251 passenger address C CI Thales - AHV Radio altimeter B CI Thales - AHV1600-2nd Radio altimeter A CI Collins - Transponder TDR94D with Mode A / C / S (ELS & EHS) / Flight identification / ADS-B Out A CI DME Collins DME A CI VOR/ILS/MKR - Collins NAV-4500 n A CI VOR/ILS/MKR - Collins NAV-4500 n A CI Telephonics RDR-1600 Weather / Search Radar B CI Rockwell Collins TTR4100 ACAS II A CI Helicopter Terrain Awareness Warning System (HTAWS) - Helionix A CI Second Canadian Marconi - CMA GPS receiver A CI Dual Flight Management System installation (2 x FMS CMA9000 and 1 x GPS CMA 5024) including Radio Control with Backup A CI Required Navigation Performance Approach (RNP APCH), On request up to LPV A CI Rig'N Fly On request B CI Solid State Cockpit Voice and Flight Data Recorder (CVFDR) L3-COM with Recorder Independent Power Supply (RIPS) A CI Usage Monitoring System (UMS) A CI Health Monitoring System (HMS) A CI Flight Data Continuous Recorder (FDCR) for HFDM (HOMP) application B E

27 4.1.2 Additional Equipment: may be selected up to 5 months before delivery The H175 Offshore configuration can be further developed with additional equipment from the following list. Items from this equipment list may be selected up to 5 months before delivery. Document reference General Equipment Commercial reference Description kg lb A CI Kit for flight in limited icing conditions Certification for flight in limited icing conditions, approved by EASA A CI Windshield heating control A CI Icing detector with severity indication A CI Horizontal stabiliser protective cover On request A CI Windshield heating control A CI Icing detector with severity indication A CI Horizontal stabiliser protective cover A CI 10 kva AC alternator A CI Airworthy mooring rings for heavy weather Specific Mission Equipment A RP Goodrich Category 1 electrical 28VDC hoist (290ft, 600lb) - Removable Parts A RP Cargo sling - Removable Parts A FP Sling hook video camera - Fixed Parts A RP Sling hook video camera - Removable Parts A RP Tail skid video camera - Removable Parts A CI Emergency Locator Transmitter Kannad Integra with embedded GPS A CI Personal Locator Beacon HR Smith (121.5 & 406 MHz) for external life raft (Qty 2) Interior Layout A CI Water protection cover for energy absorbing seat (Qty 1) A CI Cargo hold net and separation device kit Avionics C FP HF/SSB Collins - HF Fixed Parts C RP HF/SSB Collins - HF Removable Parts A RP Wireless intercom system Telephonics Trulink (rescuer communication) - Removable Parts A CI VHF/AM Rockwell-Collins VHF-4000 F n 1 - Extended frequency range, instead of VHF/AM Rockwell-Collins VHF-4000 n A CI VHF/AM Rockwell-Collins VHF-4000 F n 2 - Extended frequency range, instead of VHF/AM Rockwell-Collins VHF-4000 n A CI SKY CONNECT (EMS) fleet tracking system (including SatCom: voice and text) A CI SKYTRAC fleet tracking system (including SatCom) A RP NAT DACS ICS - Control panel on right side of the cabin Removable Parts A CI Automatic briefing unit Avionics Innovations DMP A CI David Clark H10-13 H headsets (US jacks - Qty 2) A CI David Clark H10-13 H headsets (EU jacks - Qty 2) A CI VOR/ILS/MKR/ADF - Collins NAV-4000 n 1, instead of VOR/ILS/MKR - Collins NAV-4500 n B FP Direction Finder Chelton DF V/UHF - Fixed Parts B RP Direction Finder Chelton DF V/UHF - Removable Parts B E 25

28 4.1.3 Additional Equipment: to be selected at contract signature The H175 Offshore configuration can be complemented and customized by additional equipment from the following list. Items from this equipment list are to be selected at contract signature. Document reference General Equipment Commercial reference Description A CI Complex external paint scheme A CI Acrylic external painting, instead of standard external 0.0 painting A CI Cable cutter system A CI High visibility main rotor blades A CI High visibility markings of the main rotor blade tip caps A FP Engine Air Particle Separator - Fixed Parts On requ A RP Engine Air Particle Separator - Removable Parts On requ B CI Kit for Full Ice Protection System For date of availability, please refer to a sales representative A CI Main / tail rotor blade de-icing / anti-icing systems, with two AC alternators A CI Windshield heating control A CI Icing detector with severity indication On requ A CI Horizontal stabiliser protective cover On requ Specific Mission Equipment A CI High energy absorbing landing gear On requ For date of availability, please refer to a sales representative A CI Rear cabin sea tray for Offshore Transportation On requ Configuration For date of availability, please refer to a sales representative A FP High intensity search light TRAKKA A800 - Fixed Parts 0.0 For date of availability, please refer to a sales representative A RP High intensity search light TRAKKA A800 - Removable 0.0 Parts For date of availability, please refer to a sales representative A FP Chin mounted EOS Ultra Force 350 HD - Fixed Parts 0.0 For date of availability, please refer to a sales representative A RP Chin mounted EOS Ultra Force 350 HD - Removable 0.0 Parts For date of availability, please refer to a sales representative Interior Layout A CI 16 energy absorbing seat cabin layout - Leather covered 0.0 instead of fabric covering, instead of 16 seat layout For date of availability, please refer to a sales representative A CI 18 energy absorbing seat cabin layout, instead of seat layout For date of availability, please refer to a sales representative A CI 18 energy absorbing seat cabin layout - Leather covered 0.0 instead of fabric covering, instead of 16 seat layout For date of availability, please refer to a sales representative A FP Cabin access to cargo compartment - Fixed Parts On requ A RP Cabin access to cargo compartment - Removable Parts On requ A CI Hoistable floating stretcher, Transaco TRS 902 (Qty 1) (loose equipment, delivered separately) On requ Avionics A CI Single Pilot IFR (SPIFR) 0.0 For date of availability, please refer to a sales representative A CI Automatic Identification System SaaB R4-AIS via On requ Helionix For date of availability, please refer to a sales representative B CI Digital Map EUROAVIONICS EURONAV 7 On requ For date of availability, please refer to a sales representative A CI Cockpit mission display 0.0 For date of availability, please refer to a sales representative A CI Automatic transition and hover modes (cockpit control only) 0.0 kg B E

29 4.1.4 Offshore Transportation Mission Performance The H175 aircraft has the highest standard fuel tank capacity in its class with more than 2,000 kg of fuel allowing long range mission capability. The use of latest technologies as well as the configuration and weight monitoring from an early design stage, results in a low mission empty weight and high mission payload for this 7,800 kg Maximum Take Off Weight aircraft. The following diagram presents the payload / radius of action performance for an H175 in Offshore configuration: Configuration Summary Offshore Transportation mission configuration ( CI) Equipped Empty Weight Offshore Mission profile 2 4,717 kg 1 10,399 lb Take off at Maximum Take Off Weight (Category A Clear Area, sea level): Payload Outbound flight: climb up to 5,000 ft, cruise at Best Range Speed: Radius of Action Landing / Platform operation / Take off (class 1) Inbound flight: climb up to 5,000 ft, cruise at Best Range Speed (same number of passengers as Outbound): Radius of Action Reserve: 10 % of the mission fuel and 30 min at Best Endurance Speed 1,500 ft (Reserve as per EASA OPS) Payload / Radius of Action in 16-seat Offshore configuration (EASA OPS) 1 The actual empty weight may vary within ±2 % 2 Depending on the helicopter configuration, for RoA beyond 260 NM with very few passengers, lest may be required. 175 B E 27

30 The H175 can equally accommodate up to 18 passengers in an optional configuration. This additional diagram provides the payload / radius of action performance for an H175 in Offshore configuration and equipped with the 18 passenger cabin layout: Configuration Summary Offshore Transportation mission configuration ( CI) and the 18 passenger cabin layout ( CI) Equipped Empty Weight Offshore 4,752 kg 1 10,476 lb Mission profile 2 Take off at Maximum Take Off Weight (Category A Clear Area, sea level): Payload Outbound flight: climb up to 5,000 ft, cruise at Best Range Speed: Radius of Action Landing / Platform operation / Take off (class 1) Inbound flight: climb up to 5,000 ft, cruise at Best Range Speed (same number of passengers as Outbound): Radius of Action Reserve: 10 % of the mission fuel and 30 min at Best Endurance Speed 1,500 ft (Reserve as per EASA OPS) Payload / Radius of Action in 18-seat Offshore configuration (EASA OPS) 1 The actual empty weight may vary within ±2 % 2 Depending on the helicopter configuration, for RoA beyond 260 NM with very few passengers, lest may be required B E

31 4.2 Public Services Favorite The H175 Public Services configuration replies to a wide spectrum of multi-mission demands: Search And Rescue (SAR), law enforcement and EMS. It is the result of Airbus extensive experience in helicopter design and dedicated design work with operators through Customer Advisory Team meetings. An unrivalled cabin size with large access doors and direct access to the cargo compartment offers both efficient and flexible cabin layouts. With more than 2,000 kg of standard fuel capacity the cabin and cargo compartment are maintained available for Public Services missions, avoiding any auxiliary fuel tank configuration changes, while offering the longest range/endurance in its class. The high payload and OEI performance results in unique mission efficiency and safe hoisting operations. The Public Services favorite configuration benefits from the state-of-the-art avionics suite, Helionix, coupled with the worldwide reference AFCS derived from the H225, complemented with specific SAR modes. It also encompasses an integrated mission system including Electro Optical System (EOS), search & weather radar, Automatic Identification System (AIS), Direction Finder (DF), digital moving map, and more, allowing all weather operations on land and at sea. 175 B E 29

32 4.2.1 Public Services Favorite Configuration Document reference Commercial reference Description A CI Public Services Mission Configuration A CI H175 Baseline Aircraft O as per 175 B E A CI Customized external polyurethane paint scheme A CI De-clutching system A CI Windshield washer A CI Cabin floor for public services / multi mission A CI Dual-zone regulated air conditioning system for Public Services A CI DC emergency electrical generator A CI Multi-mission cabin connector panel (28vdc, console connector, USB) O A CI Ground pressure refuelling O A CI Airworthy mooring rings for moderate weather A CI Ceiling hard attachement points (Qty 4) O A FP Cargo sling - Fixed Parts A FP External hailers - Fixed Parts O A CI HID retractable and swiveling front LH landing light O A CI Dual white & IR hover light O A FP High intensity search light TRAKKA A800 - Fixed Parts A FP Cabin operator console, including display - Fixed parts O A FP Chin mounted EOS Ultra Force 350 HD - Fixed Parts A CI Tail fin video camera A CI Cockpit video camera with embedded recorder A FP Sling hook video camera - Fixed Parts A FP Tail skid video camera - Fixed Parts A FP Emergency floatation gear - Fixed Parts O A FP External RFD liferafts installation (2*14 pax) (including PLB space provisions) Fixed Parts A FP Helicopter powered handheld searchlight - LED 3W - Fixed Parts O A RP Helicopter powered handheld searchlight - LED 3W - Removable Parts O A CI Helicopter Emergency Egress Lighting (HEEL) A CI Emergency Locator Transmitter Kannad Integra 406 with embedded GPS A CI Certified NVG operation (cockpit) A FP Black curtain between cabin and cockpit - Fixed Parts A CI Public services cabin lining A FP Cabin access to cargo compartment - Fixed Parts O A RP Cabin access to cargo compartment - Removable Parts O A CI Handle on the cabin ceiling above the sliding door (Qty 1 on each side) O A CI VHF/AM Rockwell-Collins VHF-4000 n A CI VHF/AM Rockwell-Collins VHF-4000 n A FP Wireless intercom system POLYCON - Fixed Parts A RP Wireless intercom system POLYCON - Removable Parts A CI NAT DACS ICS - Basic set: 2 control panels in cockpit A FP NAT DACS ICS - Control panel on right side of the cabin - Fixed Parts A RP NAT DACS ICS - Control panel on right side of the cabin - Removable Parts A FP NAT DACS ICS - Control panel on front left side of cabin - Fixed Parts A RP NAT DACS ICS - Control panel on front left side of cabin - Removable Parts A CI NAT DACS ICS - Control panel on rear right and left side of cabin (1 each 0.0 side) A CI Additional ICS functions (Foot PTT & cyclic mute switch for each pilot) A CI NAT 251 passenger address 0.0 kg B E

33 Document reference Commercial reference Description A CI Public Services Mission Configuration (continued) C CI Thales - AHV Radio altimeter B CI Thales - AHV1600-2nd Radio altimeter A CI Collins - Transponder TDR94D with Mode A / C / S (ELS & EHS) / Flight identification / ADS-B Out A CI DME Collins DME A CI VOR/ILS/MKR - Collins NAV-4500 n A CI VOR/ILS/MKR - Collins NAV-4500 n B FP Direction Finder Chelton DF V/UHF - Fixed Parts A CI Telephonics RDR-1700A Weather / Search Radar B CI Rockwell Collins TTR4100 ACAS II A CI Helicopter Terrain Awareness Warning System (HTAWS) - Helionix A CI Second Canadian Marconi - CMA GPS receiver A CI Dual Flight Management System installation (2 x FMS CMA9000 and 1 x GPS CMA 5024) including Radio Control with Backup A CI Automatic transition and hover modes (cockpit control only) B CI Digital Map EUROAVIONICS EURONAV A CI Enhanced Cursor Control Device A CI Required Navigation Performance Approach (RNP APCH), up to LPV A CI Cockpit mission display B CI Solid State Cockpit Voice and Flight Data Recorder (CVFDR) L3-COM with Recorder Independent Power Supply (RIPS) A CI Usage Monitoring System (UMS) A CI Health Monitoring System (HMS) A CI Flight Data Continuous Recorder (FDCR) for HFDM (HOMP) application 175 B E 31

34 4.2.2 Mandatory Equipment Document reference Interior Layout Commercial reference Description A CI SAR cabin layout 0.0 including: 1 Cabin operator console - including display - Removable Parts 1 Energy absorbing cabin operator swiveling seat 4 Energy absorbing seats 2 Seats with foldable seat pan 1 Foldable stretcher with quick release A CI Law Enforcement cabin layout 0.0 including: 1 Cabin operator console - including display - Removable Parts 1 Energy absorbing cabin operator swiveling seat 12 Energy absorbing seats A CI Aircraft cabin configuration to be customized 0.0 Helicopter cabin configuration must be chosen in the list of 07 - INTERIOR LAYOUT, in accordance with the cabin configurations already certified. See specific document A CI 18 passenger cabin layout 0.0 including: 18 Energy absorbing seats A CI EMS cabin layout O including: 4 Energy absorbing seats 2 Seats with foldable seat pan 2 Foldable stretchers with quick release 1 Medical wall (Fixed and Removable Parts) kg Further Available Equipment The H175 Public Services configuration can be further developed with additional equipment from the following list. Document reference General Equipment Commercial reference Description A CI Acrylic external painting, instead of standard external painting A CI First aid kit - EASA OPS compatible A CI Cable cutter system A CI High visibility main rotor blades A CI Main and tail rotor illumination system (white) On A CI Main and tail rotor illumination system (Complement IR) On A CI High visibility markings of the main rotor blade tip caps A FP Engine Air Particle Separator - Fixed Parts On A RP Engine Air Particle Separator - Removable Parts On A CI Openable windows on both side of the cabin A CI Kit for flight in limited icing conditions 8.1 Certification for flight in limited icing conditions, approved by EASA A CI Windshield heating control A CI Icing detector with severity indication A CI Horizontal stabiliser protective cover On r B CI Kit for Full Ice Protection System On For date of availability, please refer to a sales representative A CI Main / tail rotor blade de-icing / anti-icing systems, with two AC alternators A CI Windshield heating control A CI Icing detector with severity indication On A CI Horizontal stabiliser protective cover On A CI Windshield heating control A CI Icing detector with severity indication A CI Horizontal stabiliser protective cover A CI 10 kva AC alternator A CI Airworthy mooring rings for heavy weather 1.5 kg B E

35 Document reference Commercial reference Specific Mission Equipment Description kg lb A CI High energy absorbing landing gear On request For date of availability, please refer to a sales representative A FP Single / Dual Goodrich Category 1 electrical 28VDC hoist - Fixed Parts A RP Dual Goodrich Category 1 electrical 28VDC hoist - Removable Parts A RP Single Goodrich Category 1 electrical 28VDC hoist - Removable Parts A RP Hoist instructor control pendant - Removable Parts A CI External beam on left side and 6 hooks On request A FP Mounting points for cabin door corner (4 per door) and foreword On request cabin window (4 per window) - Fixed Parts A RP Mounting points for cabin door corner (4 per door) and foreword On request cabin window (4 per window) - Removable Parts A CI Front cabin sea tray On request A CI Rear cabin sea tray for Public Services Configuration On request A RP Cargo sling - Removable Parts A RP External hailers - Removable Parts On request B CI Dual mode white & IR Retractable and swiveling front landing lights On request instead of HID retractable and swiveling front LH landing light A RP High intensity search light TRAKKA A800 - Removable Parts A FP High intensity search light TRAKKA A800 with LASER pointer - Fixed Parts, instead of High intensity search light TRAKKA A800 - Fixed Parts A RP High intensity search light TRAKKA A800 with LASER pointer - Removable Parts A RP Cabin operator console wtih Euronav 7 control command and display On request - Removable Parts A RP Chin mounted EOS Ultra Force 350 HD - Removable Parts A CI Complementary option: Laser illuminator option for UF350 HD A CI Complementary option: Laser pointer option for UF350 HD A FP Hoisting HD video camera - Fixed Parts A RP Hoisting HD video camera - Removable Parts A RP Sling hook video camera - Removable Parts A RP Tail skid video camera - Removable Parts A RP Emergency floatation gear - Removable Parts On request A RP External RFD liferafts installation (2*14 pax) (including PLB space provisions) - Removable Parts A CI Life vest (Qty 1) On request A CI HR Smith serie ADELT with GPS connection A CI Personal Locator Beacon HR Smith (121.5 & 406 MHz) for external life raft (Qty 2) A CI NVG compatible formation lighting A CI Certified NVG operation (cabin) Interior Layout A CI Seat with foldable seat pan (Qty 1) A CI Energy absorbing seat (Qty 1) A CI Energy absorbing cabin operator swivelling seat (Qty 1) A CI Water protection cover for energy absorbing seat (Qty 1) A CI Water protection cover for seat with foldable seat pan (Qty 1) A RP Black curtain between cabin and cockpit - Removable Parts A CI Public services storage system in cargo compartment - Removable Parts A FP Medical wall - Fixed Parts On request A RP Medical wall (Qty 1) - Removable Parts On request A CI Foldable stretcher (Qty 1) A CI Set of quick release mounts for longitudinal stretcher (stretcher not On request included) (Qty 1) A CI Set of quick release mounts for transversal stretcher (stretcher not On request 175 B E 33

36 Document reference Avionics Commercial reference Description A CI Single Pilot IFR (SPIFR) 0.0 For date of availability, please refer to a sales representative A CI NAT - NPX138 VHF/FM-H A CI Chelton TETRA radio O A CI VHF/AM Rockwell-Collins VHF-4000 F n 1 - Extended frequency 5.2 range, instead of VHF/AM Rockwell-Collins VHF-4000 n A CI VHF/AM Rockwell-Collins VHF-4000 F n 2 - Extended frequency 3.4 range, instead of VHF/AM Rockwell-Collins VHF-4000 n A CI V/UHF AM/FM Chelton RT5000 O A CI V/UHF AM/FM Chelton RT5000 with P25 option O A FP VISLINK - Microwave video downlink - Fixed Parts O A RP VISLINK - Microwave video downlink - Removable Parts O A CI SKY CONNECT (EMS) fleet tracking system (including SatCom: 5.4 voice and text) A CI SKYTRAC fleet tracking system (including SatCom) A CI Cabin ICS extension (up to 18 jack US plugs ) A CI Cabin ICS extension (up to 18 jack EU plugs ) A CI Automatic briefing unit Avionics Innovations DMP A CI David Clark H10-13 H headsets (US jacks - Qty 1) O A CI David Clark H10-13 H headsets (EU jacks - Qty 1) O B CI Automatic Identification System SaaB R4-AIS via Euronav 7 O A CI VOR/ILS/MKR/ADF - Collins NAV-4000 n 1, instead of 5.9 VOR/ILS/MKR - Collins NAV-4500 n B RP Direction Finder Chelton DF V/UHF - Removable Parts A CI Telephonics RDR-1600 Weather / Search Radar instead of 0.0 Telephonics RDR-1700A Weather / Search Radar A CI Telephonics RDR-1700A Weather / Search Radar - control panel for 0.0 cabin operator console A CI Automatic transition and hover modes (complement cabin) A CI Video recorder in cabin operator console A CI Video recorder in cockpit 0.0 Operational Protection A FP Operational protection for cockpit - Fixed Parts O A RP Operational protection for cockpit - Removable Parts O A CI Operational protection for cabin O kg B E

37 4.2.4 Mission Performance Search and Rescue (SAR) Mission The following diagram presents the number of rescues / radius of action performance for an H175 in SAR configuration: Configuration Summary Public Services mission configuration ( CI) additionally equipped with: EOS UF 350 HD Searchlight Trakka A800 Dual hoist installation Floatation system, life rafts and PLB and Direction Finder Cabin operator console and energy absorbing swiveling seat 6 energy absorbing seats 1 foldable stretcher Equipped Empty Weight for SAR mission Mission profile 5,026 kg 1 11,080 lb Take off at Maximum Take Off Weight (Cat A Clear Area, sea level), 2 crew, 2 operators (85 kg each) Outbound flight: climb up to 5,000 ft, cruise at Best Range Speed - Radius of Action Search operation: 15 min at Best Endurance Speed 1,500 ft Hoisting operation: 5 min per rescue (95 kg) at sea level - Number of Rescues Inbound flight: climb up to 5,000 ft, cruise at Best Range Speed - Radius of Action Reserve: 30 min at Best Endurance Speed 1,500 ft Number of Rescuees / Radius of Action in Search & Rescue (SAR) configuration Number of Rescuees (95 kg / rescuee) ISA ISA+20 Radius of Action (NM) 1 The actual empty weight may vary within ±2 % 175 B E 35

38 Law Enforcement Mission The following diagram presents the payload / radius of action performance for an H175 in Law Enforcement configuration: Configuration Summary Public Services mission configuration ( CI) additionally equipped with: Cable cutter system Searchlight Trakka A800 Cabin operator console and energy absorbing swiveling seat 12 energy absorbing seats Equipped Empty Weight for Law Enforcement mission Mission profile 4,727 kg 1 10,421 lb Take off at Maximum Take Off Weight (Cat A Clear Area, sea level), 2 crew and 1 operator (85 kg each) Outbound flight: climb up to 5,000 ft, cruise at Best Range Speed - Radius of Action Hover / landing to unload passengers, 2 min - Payload Inbound flight: with 2 crew & 1 operator climb up to 5,000 ft, cruise at Best Range Speed - Radius of Action Reserve: 30 min at Best Endurance Speed 1,500 ft Number of Rescues / Radius of Action in Lax enforcement configuration Payload (kg) Radius of Action (NM) 1 The actual empty weight may vary within ±2 % B E

39 4.3 Private & Business Aviation Benefiting from the largest cabin size in its class, H175 offers a range of luxurious cabin configurations from ACH Line (11 or 16 pax) to ACH Exclusive (7 to 12 pax). ACH Line (11-seat arrangement) The basic quiet comfort of H175 with very low level of vibration with no need of Active Vibration Control System is further enhanced for the Exclusive version with upholstery design with enhanced soundproofing, integrating double-glazing cabin windows, hinged doors and electrical footsteps, cockpit / cabin partition, advanced IFE and Cabin Management System. The APU mode (declutch capability) allows the aircraft to be air conditioned on the ground with the rotors stopped. 175 B E 37

40 Several cabin arrangements are proposed to offer the most customized ACH Exclusive seats layout. Example of Exclusive 10-seat layout Example of Exclusive 7-seat layout The soundproofing is further improved regarding Offshore configuration for maximum passenger comfort in the ACH Exclusive configuration. The quietest in its class for external and internal sound level. Cabin lighting is constituted of: Indirect cabin lighting (LED technology ramps) provides a smooth ambient lighting. Individual LED lights and ventilation for each passenger. ACH Exclusive Cabin Layout B E

41 lb On request On request On request On request On request On request On request Technical Data ACH Line Favorite ACH Line Favorite Configuration Document reference Commercial reference Description kg A CI ACH Line Mission Configuration A CI H175 Baseline Aircraft as per 175 B E A CI Customized external polyurethane paint scheme A CI First aid kit - EASA OPS compatible A CI De-clutching system A CI Windshield washer A CI Cargo compartment step ladder (on RH side door) A CI Dual-zone regulated air conditioning system A CI DC emergency electrical generator A CI Ground pressure refuelling A CI Airworthy mooring rings for moderate weather A FP Goodrich Category 1 electrical 28VDC hoist (290ft, 600lb) - Fixed Parts A FP Cargo sling - Fixed Parts A CI HID retractable and swiveling front LH landing light A CI Tail fin video camera A CI Cockpit video camera with embedded recorder A FP Tail skid video camera - Fixed Parts A FP Emergency floatation gear - Fixed Parts A FP External RFD liferafts installation (2*12 pax) (including PLB space provisions) - Fixed Parts A CI Helicopter Emergency Egress Lighting (HEEL) A CI HR Smith serie ADELT with GPS connection B CI Comfort cabin lining A CI VHF/AM Rockwell-Collins VHF-4000 n A CI VHF/AM Rockwell-Collins VHF-4000 n A CI NAT - NPX138 VHF/FM-H A FP Wireless intercom system Telephonics Trulink (rescuer communication) - Fixed Parts A CI NAT DACS ICS - Basic set: 2 control panels in cockpit A FP NAT DACS ICS - Control panel on right side of the cabin - Fixed Parts A CI NAT 251 passenger address C CI Thales - AHV Radio altimeter B CI Thales - AHV1600-2nd Radio altimeter A CI Collins - Transponder TDR94D with Mode A / C / S (ELS & EHS) / Flight identification / ADS-B Out A CI DME Collins DME A CI VOR/ILS/MKR - Collins NAV-4500 n A CI VOR/ILS/MKR - Collins NAV-4500 n A CI Telephonics RDR-1600 Weather / Search Radar B CI Rockwell Collins TTR4100 ACAS II A CI Helicopter Terrain Awareness Warning System (HTAWS) - Helionix A CI Second Canadian Marconi - CMA GPS receiver A CI Dual Flight Management System installation (2 x FMS CMA9000 and 1 x GPS CMA 5024) including Radio Control with Backup A CI Required Navigation Performance Approach (RNP APCH), up to LPV A CI Rig'N Fly B CI Solid State Cockpit Voice and Flight Data Recorder (CVFDR) L3-COM with Recorder Independent Power Supply (RIPS) A CI Usage Monitoring System (UMS) A CI Health Monitoring System (HMS) A CI Flight Data Continuous Recorder (FDCR) for HFDM (HOMP) application 175 B E 39

42 On req uest On req uest lb On request On request On request On request On request On request Technical Data Mandatory Equipment Document reference Interior Layout Commercial reference Description kg A CI 11-seat cabin installation including: 2 armchairs with folding table in the armrest 9 energy absorbing comfort seats Specific cabin floor accommodation Cabin carpet A CI 16-seat cabin installation For date of availability, please refer to a sales representative including: 16 energy absorbing comfort seats Cabin carpet lb Further Available Equipment Document reference General Equipment Commercial reference Description kg A CI Cable cutter system A FP Engine Air Particle Separator - Fixed Parts A RP Engine Air Particle Separator - Removable Parts A CI Kit for flight in limited icing conditions Certification for flight in limited icing conditions, approved by EASA A CI Windshield heating control A CI Icing detector with severity indication A CI Horizontal stabiliser protective cover B CI Kit for Full Ice Protection System For date of availability, please refer to a sales representative A CI Main / tail rotor blade de-icing / anti-icing systems, with two AC alternators A CI Windshield heating control A CI Icing detector with severity indication A CI Horizontal stabiliser protective cover A CI Windshield heating control A CI Icing detector with severity indication A CI Horizontal stabiliser protective cover A CI 10 kva AC alternator Specific Mission Equipment A CI High energy absorbing landing gear For date of availability, please refer to a sales representative A FP Sling hook video camera - Fixed Parts A RP Emergency floatation gear - Removable Parts A RP External RFD liferafts installation (2*12 pax) (including PLB space provisions) - Removable Parts A CI Emergency Locator Transmitter Kannad Integra 406 with embedded GPS A CI Personal Locator Beacon HR Smith (121.5 & 406 MHz) for external life raft (Qty 2) Interior Layout A CI Cargo hold net and separation device kit A CI Protective over-carpet, machine made (loose equipment) B E

43 lb On request Technical Data Document reference Avionics Commercial reference Description kg A CI Single Pilot IFR (SPIFR) For date of availability, please refer to a sales representative C FP HF/SSB Collins - HF Fixed Parts C RP HF/SSB Collins - HF Removable Parts A CI VHF/AM Rockwell-Collins VHF-4000 F n 1 - Extended frequency range, instead of VHF/AM Rockwell-Collins VHF-4000 n CI VHF/AM Rockwell-Collins VHF-4000 F n 2 - Extended frequency range, instead of VHF/AM Rockwell-Collins VHF-4000 n A CI SKY CONNECT (EMS) fleet tracking system (including SatCom: voice and text) A CI SKYTRAC fleet tracking system (including SatCom) A CI NAT DACS ICS - Control panel on rear right and left side of cabin (1 each side) For date of availability, please refer to a sales representative A CI David Clark H10-13 H headsets (US jacks - Qty 2) CI David Clark H10-13 H headsets (EU jacks - Qty 2) A CI Active Noise Reduction headset for cockpit crew (Qty 2) For date of availability, please refer to a arepresentative A CI VOR/ILS/MKR/ADF - Collins NAV-4000 n 1, instead of VOR/ILS/MKR - Collins NAV-4500 n B E 41

44 lb On requ est On requ est On requ est On requ est Technical Data ACH Exclusive Favorite ACH Exclusive Favorite Configuration Document reference Commercial reference Description kg A CI ACH Exclusive Configuration A CI H175 Baseline Aircraft as per 175 B E A CI Customized enhanced external paint scheme A CI De-clutching system A CI Double-glazed cabin windows A CI Electro shading cabin windows A CI Windshield washer A CI Cabin floor for VIP configuration A CI Cargo compartment step ladder (on RH side door) A CI Two electrical cabin footsteps for hinged doors A CI Dual-zone regulated air conditioning system for VIP configuration A CI DC emergency electrical generator A CI Ground pressure refuelling A CI Airworthy mooring rings for moderate weather A CI HID retractable and swiveling front LH landing light A CI Tail fin video camera A CI Cockpit video camera with embedded recorder A FP Tail skid video camera - Fixed Parts A RP Tail skid video camera - Removable Parts A CI Emergency Locator Transmitter Kannad Integra 406 with embedded GPS A CI Hinged door both sides with double-glazed windows A CI VHF/AM Rockwell-Collins VHF-4000 n A CI VHF/AM Rockwell-Collins VHF-4000 n A CI NAT DACS ICS - Basic set: 2 control panels in cockpit A CI NAT 251 passenger address for VIP configuration C CI Thales - AHV Radio altimeter A CI Collins - Transponder TDR94D with Mode A / C / S (ELS & EHS) / Flight identification / ADS-B Out A CI DME Collins DME A CI VOR/ILS/MKR - Collins NAV-4500 n A CI VOR/ILS/MKR - Collins NAV-4500 n A CI Telephonics RDR-1600 Weather / Search Radar B CI Rockwell Collins TTR4100 ACAS II A CI Helicopter Terrain Awareness Warning System (HTAWS) - Helionix A CI Second Canadian Marconi - CMA GPS receiver A CI Dual Flight Management System installation (2 x FMS CMA9000 and 1 x GPS CMA 5024) including Radio Control with Backup A CI Required Navigation Performance Approach (RNP APCH), up to LPV B CI Solid State Cockpit Voice and Flight Data Recorder (CVFDR) L3-COM with Recorder Independent Power Supply (RIPS) A CI Usage Monitoring System (UMS) A CI Health Monitoring System (HMS) A CI Flight Data Continuous Recorder (FDCR) for HFDM (HOMP) application B E

45 lb kg On r equ est On r equ est On r equ est On r equ est On r equ est On r equ est Technical Data Mandatory Equipment Document reference Interior Layout Commercial reference Description kg A CI 7-seat VIP installation including: Front armchairs lounge for four passengers IFE and Cabin Management System Cabin/cockpit partition, with electrical window (electro shading) Associated finishing of the cockpit A CI 7-seat VIP installation with larger armchairs including: Front armchairs lounge for four passengers IFE and Cabin Management System Cabin/cockpit partition, with electrical window (electro shading) Associated finishing of the cockpit A CI 8-seat VIP installation including: Front lounge for five passengers IFE and Cabin Management System Cabin/cockpit partition, with electrical window (electro shading) Associated finishing of the cockpit A CI 10-seat VIP installation including: Ten VIP seats IFE and Cabin Management System Cabin/cockpit partition, with electrical window (electro shading) Harmonized finishing of the cockpit A CI 10-seat VIP installation with 2 club-seating including: Ten VIP seats IFE and Cabin Management System Cabin/cockpit partition, with electrical window (electro shading) Harmonized finishing of the cockpit A CI 12-seat VIP installation including: Twelve VIP seats IFE and Cabin Management System Cabin/cockpit partition, with electrical window (electro shading) Harmonized finishing of the cockpit ACH Exclusive Cabin Harmony Document reference Interior Layout Commercial reference A CI Rhapsody style (cabin and cockpit) A CI Symphony style (cabin and cockpit) A CI Allegory style (cabin and cockpit) Description 175 B E 43

46 lb On request On request On request On request On request On request On request On request On request On request On request On request On request On request Technical Data Further Available Equipment Document reference Commercial reference Description kg General Equipment A CI Cable cutter system A FP Engine Air Particle Separator - Fixed Parts A RP Engine Air Particle Separator - Removable Parts A CI Kit for flight in limited icing conditions Certification for flight in limited icing conditions, approved by EASA A CI Windshield heating control A CI Icing detector with severity indication A CI Horizontal stabiliser protective cover B CI Kit for Full Ice Protection System For date of availability, please refer to a sales representative A CI Main / tail rotor blade de-icing / anti-icing systems, with two AC alternators A CI Windshield heating control A CI Icing detector with severity indication A CI Horizontal stabiliser protective cover A CI Windshield heating control A CI Icing detector with severity indication A CI Horizontal stabiliser protective cover A CI 10 kva AC alternator Specific Mission Equipment A CI High energy absorbing landing gear For date of availability, please refer to a sales representative B FP Emergency floatation gear and Helicopter Emergency Egress Lighting (HEEL) - Fixed Parts B RP Emergency floatation gear - Removable Parts A FP External RFD liferafts installation (2*12 pax) (including PLB space provisions) - Fixed Parts A RP External RFD liferafts installation (2*12 pax) (including PLB space provisions) - Removable Parts A CI HR Smith serie ADELT with GPS connection A CI Personal Locator Beacon HR Smith (121.5 & 406 MHz) for external life raft (Qty 2) Interior Layout A CI Cargo hold net and separation device kit A CI Wing backrest for armchairs A CI Table cushion for central, rear seat A CI Cabinet for 7 layout cabin (in the middle of the front seat row) A CI Protective over-carpet, machine made (loose equipment) Avionics A CI Single Pilot IFR (SPIFR) For date of availability, please refer to a sales representative C FP HF/SSB Collins - HF Fixed Parts C RP HF/SSB Collins - HF Removable Parts A CI NAT - NPX138 VHF/FM-H A CI VHF/AM Rockwell-Collins VHF-4000 F n 1 - Extended frequency range, instead of VHF/AM Rockwell-Collins VHF-4000 n A CI VHF/AM Rockwell-Collins VHF-4000 F n 2 - Extended frequency range, instead of VHF/AM Rockwell-Collins VHF-4000 n A CI SKY CONNECT satcom with Complementary VIP pack A CI David Clark H10-13 H headsets (US jacks - Qty 2) A CI David Clark H10-13 H headsets (EU jacks - Qty 2) A CI Active Noise Reduction headset for cockpit crew (Qty 2) For date of availability, please refer to a sales representative A CI Wireless headsets - Oxytronic ANR - for 7-seat installation A CI Wireless headsets - Oxytronic ANR - for 8-seat installation A CI Wireless headsets - Oxytronic ANR - for 10-seat installation A CI Wireless headsets - Oxytronic ANR - for 12-seat installation A CI VOR/ILS/MKR/ADF - Collins NAV-4000 n 1, instead of VOR/ILS/MKR - Collins NAV-4500 n B E

47 7-seat VIP installation 8-seat VIP installation 10-seat VIP installation 175 B E 45

48 ACH Exclusive Mission Performance Benefiting from the largest cabin size in its class, H175 offers a very high level of comfort. The quiet comfort of the H175 is further enhanced with an adapted interior design providing an even smoother ride. The following diagram presents the payload / range performance for an H175 in ACH Exclusive configuration: Configuration Summary ACH Exclusive mission configuration ( CI) and the 7 seat VIP cabin layout ( CI) Equipped Empty Weight in ACH Exclusive 7 seat configuration 5,365 kg 1 11,828 lb Mission profile Take off at Maximum Take Off Weight (Category A Clear Area, sea level) - Payload Outbound flight: climb up to 5,000 ft, cruise at Best Range Speed - Range Landing Reserve: 30 min at Best Endurance Speed 1,500 ft Payload / Range in 7-seat VIP cabin layout CAT-A Clear Area 1 The actual empty weight may vary within ±2 % B E

49 Mission profile Take off at Maximum Take Off Weight (Category A Helipad, sea level) - Payload Outbound flight: climb up to 5,000 ft, cruise at Best Range Speed - Range Landing Reserve: 30 min at Best Endurance Speed 1,500 ft Payload / Range in 7-seat VIP cabin layout CAT-A Helipad 175 B E 47

50 Blank B E

51 5 Main Performance The following performance figures and charts are average values obtained with new engines. Unless otherwise specified, performance is established for the H175 in a clean configuration (Offshore configuration as defined in 4.1.1) in zero wind, sea level, standard atmospheric conditions, Environmental Control System (ECS) off. The performance provided hereafter is computed within the flight domain indicated in Aircraft Performance Performance on 2 engines, All Engines Operative (AEO) Gross Weight kg lb 6,500 14,330 7,000 15,432 7,500 16,535 7,800 17,196 Max. speed, VNE [5] kts km/hr Fast cruise speed kts (sea level) km/hr Recommended cruise speed kts (sea level) km/hr Recommended cruise speed kts (5,000 ft) km/hr Best Range speed kts (sea level) km/hr Best Range speed kts (5,000 ft) km/hr Fuel consumption at recommended cruise speed kg/hr (sea level) lb/h 1,144 1,169 1,198 1,219 Fuel consumption at recommended cruise speed kg/hr (5,000 ft) lb/h 1,044 1,079 1,120 1,140 Fuel consumption at Best Range speed kg/hr (sea level) lb/h Fuel consumption at Best Range speed kg/hr (5,000 ft) lb/h Hover ceiling I.G.E. 8ft at Take-Off Power [1] [1] ft 13,000 13,000 11,766 10,528 m 3,962 3,962 3,586 3,209 Hover ceiling O.G.E. at Take-Off Power ft 13,000 11,647 9,460 5,432 m 3,962 3,550 2,883 1,656 Service ceiling (Vz = 0,5 m/sec ft/min) at Maximum Continuous Power, 80kt ft m [2] 15,000 4,572 [2] 15,000 4,572 [2] 15,000 4,572 [2] 15,000 4,572 [1] 13,000 ft density altitude limitation [2] 15,000 ft density altitude limitation [3] EEW = 4,717 kg Crew = 170 kg Fuel = 2,067 kg (Fuel capacity with pressure refuelling) [4] EEW = 4,717 kg Crew = 170 kg Fuel = 2,001 kg (Fuel capacity without pressure refuelling) [5] CAS = IAS = 175 kts TAS = 175 kts 175 B E 49

52 Performance on 2 engines, All Engines Operative (AEO) (continued) Gross Weight Maximum range (without fuel reserve at best range speed) with pressure refuelling [3] without pressure refuelling [4] kg lb n.m km n.m km 6,500 14, ,000 15, , ,097 7,500 16, , ,073 7,800 17, , ,056 Maximum range (without fuel reserve at recommended cruise speed) with pressure refuelling [3] n.m km , , ,062 without pressure refuelling [4] n.m km , , ,026 Maximum endurance (without reserve at Best Endurance Speed 80 kts) with pressure refuelling [3] h:min 4:51 6:03 5:52 5:45 without pressure refuelling [4] h:min 4:51 5:50 5:40 5:33 [1] 13,000 ft density altitude limitation [2] 15,000 ft density altitude limitation [3] EEW = 4,717 kg Crew = 170 kg Fuel = 2,067 kg (Fuel capacity with pressure refuelling) [4] EEW = 4,717 kg Crew = 170 kg Fuel = 2,001 kg (Fuel capacity without pressure refuelling) [5] CAS = IAS = 175 kts TAS = 175 kts Performance one Engine Inoperative (OEI) Gross Weight Rate of climb at OEI Continuous power, 80 kt Service ceiling (Vz = 0,5 m/sec ft/min) at OEI Continuous power, 80 kt kg lb 6,500 14,330 7,000 15,432 7,500 16,535 7,800 17,196 ft/min m/sec ft 13,645 11,361 9,227 8,001 m 4,159 3,463 2,812 2,439 Elevated Heliport Minimum helideck height for PC1/PC2DLE performance in ISA condition (no wind): Gross Weight kg lb 7,200 15,873 Minimum Helideck height ft 35 (PC1) 7,400 16, (PC1) 7,600 16, (PC1) 7,800 17, (PC2DLE, TTET = 0s) m B E

53 5.2 Operating Limitations The aircraft is cleared to operate within the following altitude and temperature limitations (refer to the Flight Manual for complementary information): Maximum altitude: In flight Take-off and landing Minimum altitude: 15,000 ft density altitude 13,000 ft density altitude - 1,500 ft pressure altitude Temperature: Maximum ISA + 40 C limited to + 50 C Minimum - 40 C, limited to -15 C for MTOW >7,500 kg Flight envelop in limited icing conditions only available with Kit for flight in limited icing conditions (Commercial reference: CI): MTOW: 7,800 kg Maximum pressure altitude: 8,000 ft Minimum temperature: -6 C with no time limit or/and between - 6 and -10 C (duration 5 min. max). At the current certification stage, a positive air temperature band of 500 ft height, into which the aircraft can descend, must be available. 175 B E 51

54 Blank B E

55 5.3 Performance Charts Unless otherwise specified, the performance charts presented hereafter are established for the aircraft in a clean configuration (Offshore configuration as defined in 4.1.1), zero wind, sea level, standard atmospheric conditions. The performance data provided hereafter is computed within the flight domain indicated in 5.2. Take-Off Weight in Hover In Ground Effect (IGE), AEO, TOP 55 Maximum weight in Hover Out of Ground Effect (OGE), AEO, TOP 56 Category A Maximum Take-Off Weight, Clear Area, Long Runway 57 Category A Maximum Take-Off Weight, Helipad 58 Maximum Rate of Climb Twin-engine at Maximum Continuous Power (MCP), TAS = 80 kts, ISA 59 Maximum Rate of Climb Twin-engine at Maximum Continuous Power (MCP), TAS = 80 kts, ISA + 20 C 60 Maximum Rate of Climb Twin-engine at Maximum Continuous Power (MCP), TAS = 80 kts, ISA + 35 C 61 Maximum Rate of Climb One Engine Inoperative (OEI) at Continuous Power Rating, TAS = 80 kts, ISA 62 Maximum Rate of Climb One Engine Inoperative (OEI) at Continuous Power Rating, TAS = 80 kts, ISA + 20 C 63 Maximum Rate of Climb One engine inoperative (OEI) at Continuous Power Rating, TAS = 80 kts, ISA + 35 C 64 Fast Cruise Speed in Level flight Twin-engine at Maximum Continuous Power (MCP), ISA 65 Fast Cruise Speed in Level Flight Twin-engine at Maximum Continuous Power (MCP), ISA + 20 C 66 Fast Cruise Speed in Level Flight Twin-engine at Maximum Continuous Power (MCP), ISA + 35 C 67 Hourly Fuel Consumption in Level Flight Pressure Altitude = 0 ft, ISA (temperature = 15 C) 68 Hourly Fuel Consumption in Level Flight Pressure Altitude = 2,500 ft, ISA (temperature = 10 C) 69 Hourly Fuel Consumption in Level Flight Pressure Altitude = 5,000 ft, ISA (temperature = 5 C) 70 Hourly Fuel Consumption in Level Flight Pressure Altitude = 0 ft, ISA + 20 C (temperature = 35 C) 71 Hourly Fuel Consumption in Level Flight Pressure Altitude = 2,500 ft, ISA + 20 C (temperature = 30 C) 72 Page 175 B E 53

56 Hourly Fuel Consumption in Level Flight Pressure Altitude = 5,000 ft, ISA + 20 C (temperature = 25 C) 73 Hourly Fuel Consumption in Level Flight Pressure Altitude = 0 ft, ISA + 35 C (temperature = 50 C) 74 Hourly Fuel Consumption in Level Flight Pressure Altitude = 2,500 ft, ISA + 35 C (temperature = 45 C) 75 Hourly Fuel Consumption in Level Flight Pressure Altitude = 5,000 ft, ISA + 35 C (temperature = 40 C) 76 Page B E

57 Take-Off Weight in Hover In Ground Effect (IGE) AEO, TOP Pressure altitude (ft) ISO-Outside air temperature ( C) Max Hsigma ISA Kg ISA ISA Weight (kg) 175 B E 55

58 Maximum Weight in Hover Out of Ground Effect (OGE) AEO, TOP Pressure altitude (ft) ISO-Outside air temperature ( C) ISA Max Hsigma kg ISA Weight (kg) ISA B E

59 Category A Maximum Take-Off Weight Clear Area, Long Runway Pressure altitude (ft) ISO-Outside air temperature ( C) ISA+ 40 Max Hsigma kg ISA ISA Weight (kg). 175 B E 57

60 40 Technical Data Category A Maximum Take-Off Weight, Helipad Pressure altitude (ft) ISO-Outside air temperature ( C) 7500kg ISA ISA+ 40 Max Hsigma ISA-20 ISA Weight (kg) B E

61 Maximum Rate of Climb Twin-engine at Maximum Continuous Power (MCP), TAS = 80 kts, ISA Pressure altitude (ft) ISO-Weight (kg) Vertical speed (ft/mn) 0 10 (m/s) 175 B E 59

62 Maximum Rate of Climb Twin-engine at Maximum Continuous Power (MCP), TAS = 80 kts, ISA + 20 C Pressure altitude (ft) ISO-Weight (kg) Vertical speed (ft/mn) 0 10 (m/s) B E

63 Maximum Rate of Climb Twin-engine at Maximum Continuous Power (MCP), TAS = 80 kts, ISA + 35 C Pressure altitude (ft) ISO-Weight (kg) Vertical speed (ft/mn) 0 10 (m/s) 175 B E 61

64 Maximum Rate of Climb One Engine Inoperative (OEI) at Continuous Power Rating, TAS = 80 kts, ISA Pressure altitude (ft) ISO-Weight (kg) (m) Vertical speed (ft/mn) -2 5 (m/s) B E

65 Maximum Rate of Climb One Engine Inoperative (OEI) at Continuous Power Rating, TAS = 80 kts, ISA + 20 C Pressure altitude (ft) ISO-Weight (kg) (m) Vertical speed (ft/mn) -2 5 (m/s) 175 B E 63

66 Maximum Rate of Climb One Engine Inoperative (OEI) at Continuous Power Rating, TAS = 80 kts, ISA + 35 C Pressure altitude (ft) ISO-Weight (kg) Vertical speed (ft/mn) B E

67 Fast Cruise Speed in Level Flight Twin-engine at Maximum Continuous Power (MCP), ISA 7800 kg lb kg lb Pressure altitude (ft) (m) kg lb 6000 kg lb 6500 kg lb 7000 kg lb VNE True Air Speed (kt) (km/h) 175 B E 65

68 Fast Cruise Speed in Level Flight Twin-engine at Maximum Continuous Power (MCP), ISA + 20 C 7500 kg lb 7800 kg lb Pressure altitude (ft) (m) VNE kg lb 6500 kg lb 5500 kg lb 6000 kg lb True Air Speed (kt) (m/s) B E

69 Fast Cruise Speed in Level Flight Twin-engine at Maximum Continuous Power (MCP), ISA + 35 C 7500 kg lb 7000 kg lb 6500 kg lb Pressure altitude (ft) (m) kg lb VNE kg lb 5500 kg lb True Air Speed (kt) (km/h) 175 B E 67

70 Hourly Fuel Consumption in Level Flight Pressure Altitude = 0 ft, ISA (temperature = 15 C) B E

71 Hourly Fuel Consumption in Level Flight Pressure Altitude = 2,500 ft, ISA (temperature = 10 C) 600 Fuel Flow (kg/h) kg lb 7500 kg lb Vmax Vreco kg lb kg lb 6000 kg lb 5500 kg lb Vbr True Air Speed (kt) (km/h) 175 B E 69

72 Hourly Fuel Consumption in Level Flight Pressure Altitude = 5,000 ft, ISA (temperature = 5 C) 600 Fuel Flow (kg/h) kg lb Vmax kg lb 7000 kg lb kg lb 6000 kg lb Vreco 5500 kg lb 400 Vbr True Air Speed (kt) (km/h) B E

73 Hourly Fuel Consumption in Level Flight Pressure Altitude = 0 ft, ISA + 20 C (temperature = 35 C) 650 Fuel Flow (kg/h) ISO-Weight (kg) Vreco Vmax Vbr True Air Speed (kt) (km/h) 175 B E 71

74 Hourly Fuel Consumption in Level Flight Pressure Altitude = 2,500 ft, ISA + 20 C (temperature = 30 C) 650 Fuel Flow (kg/h) 600 Vmax kg lb 7500 kg lb Vreco kg lb 6500 kg lb kg lb 5500 kg lb Vbr True Air Speed (kt) (km/h) B E

75 Hourly Fuel Consumption in Level Flight Pressure Altitude = 5,000 ft, ISA + 20 C (temperature = 25 C) 650 Fuel Flow (kg/h) kg lb 7500 kg lb Vmax kg lb 6500 kg lb 6000 kg lb 5500 kg lb Vreco 400 Vbr True Air Speed (kt) (km/h) 175 B E 73

76 Hourly Fuel Consumption in Level Flight Pressure Altitude = 0 ft, ISA + 35 C (temperature = 50 C) 650 Fuel Flow (kg/h) ISO-Weight (kg) Vreco Vmax Vbr True Air Speed (kt) (km/h) B E

77 Hourly Fuel Consumption in Level Flight Pressure Altitude = 2,500 ft, ISA + 35 C (temperature = 45 C) Fuel Flow (kg/h) 7800 kg lb kg lb kg lb 6500 kg lb Vmax=Vreco kg lb 5500 kg lb Vbr True Air Speed (kt) (km/h) 175 B E 75

78 Hourly Fuel Consumption in Level Flight Pressure Altitude = 5,000 ft, ISA + 35 C (temperature = 40 C) 650 Fuel Flow (kg/h) kg lb kg lb kg lb 6500 kg lb 6000 kg lb Vmax=Vreco Vbr kg lb True Air Speed (kt) (km/h) B E

79 6 Support & Services Airbus global customer service network works around the clock in more than 150 countries, bringing tailor-made and competitive solutions to more than 3000 customers that collectively log more than three million flight hours annually. Through the HCare service offer, Airbus keeps businesses on track and rotorcraft in the skies. Spanning material management, helicopter maintenance, technical support, training & flights ops and connected services, HCare ensures that each flight is a success and performed with the highest levels of safety. As operators requirements evolve and their missions become more demanding, Airbus continuously adapts its service portfolio to fit customers needs. Airbus remains 100% at the service of its customers. The company is committed to achieving: 100 % of spare part planned orders delivered on time 100 % of customers visited by an Airbus representative to discuss their business and needs 100 % of HUMS red alarm queries answered within 24 hours 100 % around-the-clock availability for all customer support queries 175 B E 77

80 6.1 Material Management Airbus provides a comprehensive initial provisioning package. It includes spare parts, tools, test equipment, etc. to sustain helicopter operations for a defined initial period of time. The dimension of the package is tailored to the number of helicopters, number of operating bases, flight hours per year and requested availability. On top of this initial provisioning list, Airbus material management service is dedicated to ensure parts availability through spare part supply or components repair and overhaul of all rotorcraft within its product range, keeping customers operating at top performance levels. Three levels of Material Management services are available to ensure the availability of all rotorcraft in the company s product range HCare Easy HCare Easy is Airbus series of on-request catalogue services related to the repair, exchange, rental and ordering of helicopter spare parts and components. With this support concept the customer bears the responsibility to monitor repairs; manage obsolescence and procure the right mix and quantity of components and spare parts HCare Smart HCare Smart s by-the-hour programs offer a solution for all operator types, from low to high frequency fliers. With a fixed rate per flight hour, it enables budget planning and control, enhanced helicopter availability and more simple management thanks to a unique contract HCare Infinite The HCare Infinite program provides a fleet availability commitment from Airbus to customers. It is a turnkey solution, adapted to customer needs, enabling customer to focus on flights while Airbus takes care of supporting the customer fleet. The program comprises material support, logistic management and technical services B E

81 6.2 Helicopter Maintenance H175 scheduled maintenance program has been elaborated according to the MSG-3 (Maintenance Steering Group 3rd issue) method approved by the EASA. The MSG-3 method includes a Living Maintenance Review Board (MRB) process based on a collaborative work between Airbus and a representative sample of operators to organize the in service feedback experience. Thanks to the continuous exchange with operators, the scheduled maintenance program can be permanently optimized with the objective of increasing cost effectiveness while preserving safety. Consequently, the maintenance program is at least yearly updated Scheduled Inspections 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 their own specific organization, provided it 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 special tools and / or test equipment. 175 B E 79

82 Depot Level (D-Level) The Depot 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 special overhaul and repair tools, as well as test benches (if required) according to repair manuals or instructions. Scheduled airframe inspections Maintenance level Estimated mean man hours Flight Related Check O Level - Pre-Flight check O Level - 50 FH inspection I Level FH inspection I Level FH inspection I Level FH inspection I Level 308 1,600 FH inspection I Level year inspection I Level - 9 year inspection I Level - 12 year inspection I Level - 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 Servicing Manual (MSM). The announced mean man hours are post sampling program and without incoming flight, work preparation, reworking, servicing, Service Bulletin (SB) implementation, unscheduled maintenance. The following table provides an overview of all engine inspections. Each inspection has to be performed for the respective time frame. PT6C-67E Scheduled Inspections (per engine) Maintenance level Estimated man hours 15 h Engine oil quantity through sight glass O - Level h Engine Power Assurance Check O - Level h I - Level 16 Compressor & Turbine desalanisation wash frequency based on operating environment I - Level 1.25 Note: For further details on the engine inspections and the respective D-Level maintenance please refer to the applicable engine maintenance manual B E

83 6.2.2 Time limits Components must be removed the latest when limits are reached. Limits are determined according to component type. The terms Service Life Limit (SLL), Operational Time Limitation (OTL) or Time Between Overhauls (TBO) are used. PT6C-67E overhauls TBO as per Engine EMM rev 8 Complete engine Hot Section Inspection (HSI) 5,000 FH on-condition Airframe main components TBO as per MSM Rev. 008 Main Rotor Hub Tail Rotor Hub Main Gear Box Main Module Main Gear Box Epicyclic Module MGB Accessory drive Gear Box LH MGB Accessory drive Gear Box RH Tail Gear Box Intermediate Gear Box Main Servo Control Tail Servo Control On Condition On Condition 5,000 FH or 6 Years* (a) 5,000 FH or 6 Years* (a) 5,000 FH or 6 Years* (a) 5,000 FH or 6 Years* (a) 5,000 FH or 6 Years* (a) 5,000 FH or 6 Years* (a) 5,000 FH (a) 5,000 FH (a) Note: Non exhaustive list. * First limit reached (a). TBO objective. Maturity plan in progress Aircraft maintenance, aircraft repair and on-site assistance Airbus provides a range of service levels for line, intermediate and heavy maintenance activities from dispatching experts on-site, to welcoming a rotorcraft at an Airbus-certified center. Line maintenance, which is often completed within a short period of time and does not require specialized equipment, training or facilities, can be performed either on the flight line or on-site at a customer s premises. Intermediate maintenance is more often performed at a maintenance center due to the higher level of tools, equipment and training required. Heavy maintenance and major inspections on any Airbus rotorcraft can be performed either inhouse at an Airbus-certified maintenance center or directly at the operator s facilities. The Airbus global network of approved maintenance centers is located in close proximity to customer facilities to perform these services. 175 B E 81

84 6.2.4 Upgrades and retrofit Airbus knows that a rotorcraft may lead multiple lives adapting to new needs and expectations. This is why the company proposes tailored solutions to increase a helicopter's overall performance and to reduce its maintenance cost, better preparing it to perform future missions. A large range of conversions and mid-life upgrades is available to maintain aircraft at the latest version, benefitting from innovations and advanced technology, perfectly adapted to your aircraft configuration and defined by our experienced design office teams. 6.3 Technical Support Airbus provides several levels of technical support and resources to ensure the appropriate response to each query or expectation: Technical expertise & assistance Technical publications Continuing airworthiness management services FlyScan 24/7 technical support hotline All technical requests can be placed online via the erequests tool on Keycopter and tracked online via the Technical Request Management tool Technical Expertise A team of highly skilled engineers in close and daily relation with the design office is committed to answer any technical question. This team is also in charge to establish technical improvements, recommendations for use, customer information (Service Bulletins, Information Notices ), and is the focal point for technical relation with Airbus. They can be contacted 24 hours/7 days B E