EC225 Technical Data 225 09.101.01 E
EC225 Technical Data SUPER PUMA (Civil Version) AS 332 C1 (MK1) AS 332 L1 (MK1) EC 225 COUGAR (Military Version) Naval version missiles/torpedoes AS 532 SC (MK1) Stretched version utility/armed AS 532 AL (MK1) Utility/armed version EC 725
Contents 1 - Foreword... 3 2 - General characteristics... 5 3 - Baseline Aircraft Definition... 12 4 - Recommended Mission Configurations... 15 5 - Optional Equipment... 23 6 - Main performance... 32 7 - Customer Service Overview... 51 Manufacturers notice Attention! EUROCOPTER, its logo, EC225, COUGAR, SUPER PUMA, SPHERIFLEX, M ARMS are trade marks of the Eurocopter group. Eurocopter s policy is one of on-going product enhancement which means that alterations in definition, pictures, weights, dimensions or performance may be made at any time without notice being included in those documents that have already been issued. This document cannot thus be taken as an offer or serve as an appendix to a contract without a prior check as to its validity and prior written agreement of EUROCOPTER. The operational or certification regulations, as defined by the local authorities, can make compulsory the installation of some of the equipment and recommended solutions, listed in this document. This list does not claim to cover the whole of the worldwide operational requirements nor the equipment not specifically related to the helicopter (for example: life jacket) or necessary for particular missions (for example: supplemental oxygen). The operator is responsible for ascertaining with his local authorities that the planned configuration of the helicopter complies with regulatory requirements for the area(s) of operations and the type(s) of mission(s) considered. 225 09.101.01 E 1
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1- Foreword The EC225 is a medium weight twin engine helicopter (11 tons class) with outstanding performance that belongs to the famous SUPER PUMA / COUGAR family. Over 702 units, with total flight time in excess of 3,775,534 Flight Hours have been delivered to date. The EC225 is a powerful and fast helicopter with long range capabilities. It has a very large useful volume and accommodates various seating arrangements up to 19 passenger crashworthy seats in a spacious cabin and 3 crew members. Technical advancements developed by EUROCOPTER on the EC225 include modular design of the mechanical assemblies, use of composite materials, state of the art avionics, including LCD Multi-Functions Displays, Vehicle Monitoring System and AFCS. The EC225 also incorporates the new generation TURBOMECA Makila 2A1 power plant that provides high performance and maximum safety, thanks to its fully redundant dual channel FADEC system and blade shedding technology. The EC225 can be equipped with a full de-icing system compliant with FAR/JAR 29 regulations, to fly in icing conditions without limitation of severity. 225 09.101.01 E 3
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2- General Characteristics Layout Minimum flight crew VFR conditions: IFR conditions : VIP transport (in addition to the crew) : Passenger transport (in addition to the crew) up to : 1 pilot 2 pilots 8 to 12 passengers 19 crashworthy seats Weights Note : Empty weight accuracy : within ± 2.0 % kg lb Empty weight, standard aircraft (including engine oil and unusable fuel) 5,376 11,852 Useful load 5,624 12,398 Maximum all-up weight 11,000 24,251 Maximum cargo-sling load 4,500 9,921 Maximum all-up weight in external load configuration 11,200 24,690 Power plant 2 Turbomeca Makila 2A1 turboshaft engines. Engine ratings Power per engine, in standard atmosphere, at sea level : kw shp Maximum emergency power (OEI 30") 1,776 2,382 Intermediate emergency power (OEI 2') 1,667 2,236 OEI continuous power 1,608 2,156 Take-off power 1,567 2,101 Maximum continuous power 1,418 1,902 Usable Fuel capacities litres US gal. kg lb Standard energy absorbing fuel tanks 2,553 674 2,017 4,447 Optional central energy absorbing fuel tank 318 84 251 553 Optional ferry fuel tanks (1 to 5) 5 x 475 5 x 126 5 x 375 5 x 826 Pod fuel tanks 600 157 474 1045 225 09.101.01 E 5
Main dimensions 19.50 m Rotor Rotating 63.98 ft φ 16.20 m 53.14 ft dia φ 3.15 m 10.33 ft dia 4.60 m 15.09 ft 4.97 m 16.30 ft 5.25 m 17.22 ft 16.79 m 55.08 ft 2.00 m 6.56 ft 3.96 m 13.00 ft 2.12 m 6.95 ft 3.00 m 9.84 ft Dimensions with blades folded 4.10 m 13.45 ft 225 09.101.01 E 6
Dimensions of compartments and accesses Cabin main dimensions Cabin floor 225 09.101.01 E 7
Main technical improvements to increased safety: Engines: Makila 2A1 Dual channel FADEC Modular Design Pilot workload reduction Ultimate Protection (Overspeed protection & «Blade Shedding» technologies) Enhanced compressors Fadec driven bleed valve (better SFC & surge margin) Power turbine with blade shedding system Based on Makila 2A experience, a reliable engine, the Makila 2A1 incorporates two main improvements: Increased OEI performances Consumption reduction Enhanced Dual Channel FADEC Single crystal blades Main Gear Box MGB torque limitations: 100% torque corresponds to 2610 kw at 265 rpm rotor speed kw shp Super contingency power (OEI 30") 1 2,047 2,745 Maximum contingency power (OEI 2') 1 1,877 2,517 Intermediate contingency power (unlimited) 1 1,655 2 2,219 Maximum continuous power (unlimited) 2,159 2,895 Take-off power (5') 2,610 3,500 Transient power (20") 2,871 3,850 Increased power 30 minutes flight capability after total loss of oil, with back-up lubrication Spray system, compliant with JAR 29 Upgraded upper part (casing and rotor bearing) and lower part (casing, gears) 1 Limitation controlled by the Fadec for NR>255 rpm. 2 The INT contingency power is 1593 kw at 255 rpm. 225 09.101.01 E 8
Blades 5 blades SPHERIFLEX main rotor, with upgraded servo actuators New blade profile, multibox structure, capable of flight in icing condition Avionics Advanced Helicopter Cockpit Avionics System (AHCAS), implementing: four 6 x 8 LCD Multi Function Displays (MFD) two 4 x 5 Vehicle Management System color displays (VMS) one Integrated Stand-by Instrument LCD (ISI) new Automatic Flight Control System (AFCS), Air Data Computer (ADC) and Attitude and Heading Reference System (AHRS) 1 2 6 1 3 4 5 1 2 7 9 8 7 1 Piloting, Navigation and Mission Multifunction displays 4 Warning panel 2 NR/ILS button indicator 5 VMS displays Master warning light 6 Triple tachometer General alarm 7 Automatic Flight Control Panel (AFCP) Landing gear warning light 8 ISI (Integrated Stand-by Instrument) 3 Stop watch 9 Provision 225 09.101.01 E 9
State of the Art Autopilot The Automatic Flight Control System is a 4-axis dual duplex digital auto-pilot, fully integrated with the avionics and offering full operationality after failure. The complete set of cruise/navigation and approach upper modes is proposed including envelope protection and extended mission effectiveness with SAR modes as an option. The AFCS comprises two (duplex architecture) Automatic Flight Control Computers (AFCCs) which are linked to the MFDs and controlled by two control panels located within close reach of each crew member, and several stick buttons. Each AFCC includes 2 separate processing units (dual architecture) which self-monitor themselves. In case of failure, the standby AFCC takes full control over the actuators and resumes the operation. Noise Reduction One of the main features on the EC225 is the overall standard of better comfort for the cabin passengers and aircrew. Vibration levels have been significantly reduced, thanks to the new 5-bladed rotor and a state-of-the-art active anti-vibration system. This system uses a computer to generate anti-vibrations, i.e. 180 out of phase with the vibrations detected in the 3 most sensitive areas of the helicopter. Thanks to this system, the EC225 has by far the lowest vibration level of all the helicopters in its class. 225 09.101.01 E 10
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3 EC225 Baseline Aircraft Definition 225 09.100.02 E 12
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4 Recommended Mission Configurations EUROCOPTER proposes different mission configurations for its helicopters. This pre-selected list of optional equipment should be regarded as a recommended minimum equipment list and can be complemented by additional equipment from the optional equipment list in chapter 5. Please take note that there can be incompatibilities between optional equipments. Any modification and/or complement of the proposed mission configuration must be done in with assistance of a EUROCOPTER sales representative. The proposed mission configurations are done by EUROCOPTER using its years of experience in making helicopters and in coordination with different operators of the EC225 around the world. For the EC225 the recommended mission configurations are: Offshore mission SAR mission 4.1 Recommended Offshore configuration The EC225 Offshore is designed to carry 19 passengers over long distances with the standard reserves. Its built-in power reserve guarantees high performance within the framework of the future regulatory changes. The seat backrests are fitted with a removable head-rest, a 4 point harness and a net for life vest (under the seat). 19 crashworthy seats fitted on a reinforced cabin floor can be proposed as well as other seats configuration. The seats can be removed very quickly, so that a large area of the cabin floor can be used for load transportation. This enables to convert within few minutes any passenger transport helicopter into a cargo transport or into a composite version. 225 09.101.01 E 15
Mission configuration Document reference Commercial reference Name 00-10029-A 00-10029-00-CI EC225 Baseline Aircraft 00-50013-A 00-50013-00-CI "EC225 Offshore" package including: General Equipment 05-03006-A 05-03006-00-CI First aid kit - JAR OPS 3 compatible 05-26007-A 05-26007-00-CI Dinol AV30 re-inforced anti-corrosive treatment 05-31052-A 05-31052-00-CI Enlarged Cabin grey tinted windows 05-35002-A 05-35002-00-CI Cabin floor for crashworthy seats 05-36025-A 05-36025-00-CI Enlarged footstep cockpit 05-36026-A 05-36026-00-CI Enlarged footstep cabin 05-39002-A 05-39002-00-CI Illuminated Map Holder - JAR OPS 3 compatible 05-50003-A 05-50003-00-CI Kit for flight in limited icing conditions 05-51001-A 05-51001-00-CI De-iced cockpit center pane with wiper 05-52006-A 05-52006-00-CI Goodrich Icing severity indicator 05-65000-A 05-65000-00-CI Hydro electric group 05-81031-A 05-81031-00-CI Energy Absorbing central auxiliary fuel tank 318 l (84 US gal) 05-82005-A 05-82005-00-CI Pressure refuelling on the ground with Energy Absorbing self-sealing sponson fuel tanks Specific Mission Equipment 06-21015-A 06-21015-00-FP Goodrich 28V electrical hoist (290ft, 600lb) - Fixed parts 06-26006-B 06-26006-01-FP External mirrors (including one electrical) - Fixed Parts 06-27013-A 06-27013-00-FP Cargo sling with dynamometer 3,8 Tons - Fixed parts 06-41003-A 06-41003-00-CI Hella anti collision strobe light system (instead of standard one) 06-41004-A 06-41004-00-CI Soderberg anti collision light (belly mounted) 06-42012-A 06-42012-00-CI Fixed lights in the sponsons 06-60004-A 06-60004-00-CI 2 Life rafts - 18 to 27 pax - in the multipurpose sponsons with jettison control in cockpit 06-61011-A 06-61011-00-FP Emergency floatation gear with automatic firing - Fixed parts 06-61011-A 06-61011-00-RP Emergency floatation gear with automatic firing - Removable parts 06-65008-A 06-65008-00-CI 3rd hand held fire extinguisher - JAR OPS 3 compatible 06-65010-A 06-65010-00-CI 2 Flashlights - JAR OPS 3 compatible 06-66004-A 06-66004-00-CI Helicopter Emergency Egress Lighting (HEEL) 06-67023-A 06-67023-00-CI HR Smith series 503 ADELT Configuration continued on next page 225 09.101.01 E 16
Document Commercial reference reference Interior Layout Name 07-10009-A 07-10009-00-FP 3rd crew man seat - Fixed parts 07-15009-A 07-15009-00-CI Pilot and copilot crashworthy seats 07-27002-A 07-27002-00-CI 19 crashworthy seat installation 07-37007-A 07-30007-00-CI Comfort upholstery with improved soundproofing 07-60016-A 07-60016-00-CI Luggage compartment in the intermediate structure Avionics 08-00016-A 08-00016-02-CI Civil Use minimum equipment (IFR dual pilot) including: Collins - Proline21 - VHF/AM #1 Collins - Proline21 - VHF/AM #2 NAT DACS ICS - Basic set : 3 control panels in cockpit Collins - TDR94D - 008 Collins - Proline21 - DME Collins - Proline21 VOR/ILS/MKR #2 Collins - Proline21 VOR/ILS/MKR/ADF #1 Serpe - IESM Kannad 406 AP - Emergency Locator Transmitter 08-10016-A 08-10016-00-CB Collins - HF 9X00 - HF/SSB - Capabilities 08-12025-A 08-12025-00-CI NAT - NPX138 VHF/FM-H 08-16026-A 08-16026-00-CI NAT DACS ICS - Complementary set : 4th control panel 08-17049-A 08-17049-00-CI NAT- Passenger Address 08-27008-A 08-27008-00-CI Chelton System 7 - (121,5) VHF/FM Marine dual frequency homer 08-31039-A 08-31039-00-CI Telephonics 1600 Weather Radar, displayed on AHCAS 08-35009-A 08-35009-01-CI TCAS - GOODRICH - HP 899 integrated to AHCAS 08-35015-A 08-35015-00-CI EGPWS - HONEYWELL - MKXXII integrated to AHCAS 08-41012-A 08-41012-00-CI Canadian Marconi - CMA3024 - GPS receiver 08-44040-A 08-44040-00-CI Canadian Marconi - CMA9000 - Flight Management System 08-83004-A 08-83004-01-CI M'ARMS Health & Usage Monitoring System (HUMS) with HOMP & Allied Combi-lite CVFDR 225 09.101.01 E 17
4.2 Recommended SAR Configuration The EC225 SAR standard helicopter is an aircraft configuration built by and with inputs and recommendations of major civil SAR operators, in order to define the most performing helicopter for the SAR missions. The helicopter proposed by EUROCOPTER will be civil certified by European Authorities. The EC225 SAR, as proposed, is the latest generation aircraft for the endurance, the equipments, safety and mission reliability and capability. It offers a state-of-the-art and much integrated cockpit avionics suite for both communication and navigation purposes, an AFCS with specific SAR modes considered as a worldwide reference, and includes an integrated SAR mission system including all search and rescue necessary equipments (HD FLIR, search radar, R4AIS, Chelton DF935, digital moving map). The large EC225 cabin is perfectly suited to accommodate a comprehensive SAR cabin arrangement, including FLIR cabin console and operator seat, hoistman and cabin crew or rescues seats (up to 20) and up to 6 super imposed stretchers. A typical SAR layout is given as a reference. It comes with: 1 FLIR Console and its associated operator sliding crashworthy seat 1 medical kit which consists of 1 unit of 2 foldable stretchers, which can be easily installed and removed. 7 wall mounted foldable seat installation 2 operator sliding crashworthy seats Additional 4 wall mounted seats (in place of medical kit when not installed). Example of SAR interior layout 225 09.101.01 E 18
Mission configuration Document reference Commercial reference Name 00-10029-A 00-10029-00-CI EC225 Baseline Aircraft General Equipment 05-03006-A 05-03006-00-CI First aid kit - JAR OPS 3 compatible 05-26007-A 05-26007-00-CI Dinol AV30 re-inforced anti-corrosive treatment 05-31039-A 05-31039-00-CI 2 observation bubble windows on cabin plug-in doors 05-31052-A 05-31052-00-CI Enlarged cabin grey tinted windows 05-35005-A 05-35005-00-CI Multipurpose Integrated Crashworthy Floor 05-39002-A 05-39002-00-CI Illuminated Map Holder - JAR OPS 3 compatible 05-50003-A 05-50003-00-CI Kit for flight in limited icing conditions 05-51001-A 05-51001-00-CI De-iced cockpit center pane with wiper 05-52006-A 05-52006-00-CI Goodrich Icing severity indicator 05-65000-A 05-65000-00-CI Hydro electric group 05-81031-A 05-81031-00-CI Energy Absorbing central auxiliary fuel tank 318 l (84 US gal) 05-82005-A 05-82005-00-CI Pressure refuelling on the ground with Energy Absorbing self-sealing sponson fuel tanks Specific Mission Equipment 06-20003-A 06-20003-00-FP Double hoist installation - Fixed Parts 06-20003-A 06-20003-00-RP1 Double hoist installation - Removable Parts (Main Hoist & Beam) 06-20003-A 06-20003-00-RP2 Double hoist installation - Removable Parts (Backup Hoist) 06-26006-B 06-26006-01-FP External mirrors (including one electrical) - Fixed Parts 06-27013-A 06-27013-00-FP Cargo sling with dynamometer 3,8 Tons - Fixed Parts 06-31018-B 06-31018-01-FP Electrical hailer installation (Qty 1) - Fixed Parts 06-31018-B 06-31018-01-RP Electrical hailer installation (Qty 1) - Removable Parts 06-41004-A 06-41004-00-CI Soderberg anti collision light (belly mounted) 06-42012-A 06-42012-00-CI Fixed lights in the sponsons 06-43001-A 06-43001-00-CI Swivelable light under right sponson 06-43001-A 06-43001-01-CI Swivelable light under left sponson 06-43005-A 06-43005-00-CI Vertical light for hoisting and sling operation surveillance 06-45061-A 06-45061-00-FP Trakka Search light with infrared filter in-flight changeover - Fixed Parts 06-45061-A 06-45061-00-RP Trakka Search light with infrared filter in-flight changeover - Removable Parts 06-45062-A 06-45062-00-CI FLIR Mx15i HD / Trakka Slaving Unit 06-51030-A 06-51030-00-FP Flir Operator console - Fixed Parts 06-51030-A 06-51030-00-RP Flir Operator console - Removable Parts 06-51140-A 06-51140-00-FP Nose mounted FLIR WESCAM MX15i HD - Fixed Parts 06-51140-A 06-51140-00-RP Nose mounted FLIR WESCAM MX15i HD - Removable Parts Configuration continued on next page 225 09.101.01 E 19
Document Commercial reference reference Specific Mission Equipment Name Technical Data 06-60004-A 06-60004-00-CI 2 Life rafts - 18 to 27 pax - in the multipurpose sponsons with jettison control in cockpit 06-61011-A 06-61011-00-FP Emergency floatation gear with automatic firing - Fixed Parts 06-61011-A 06-61011-00-RP Emergency floatation gear with automatic firing - Removable Parts 06-65008-A 06-65008-00-CI 3rd hand held fire extinguisher - JAR OPS 3 compatible 06-65010-A 06-65010-00-CI 2 Flashlights - JAR OPS 3 compatible 06-66004-A 06-66004-00-CI Helicopter Emergency Egress Lighting (HEEL). 06-67001-A 06-67001-00-CI 2 Portable ELT 406 MHz HR SMITH Personal Locator Serie 500 in liferafts 06-67023-A 06-67023-00-CI HR Smith serie 503 - ADELT 06-70008-A 06-70008-00-CI NVG compatible cockpit lighting 06-70013-A 06-70013-00-CI NVG compatible cabin lighting 06-70014-A 06-70014-00-CI NVG compatible external lighting Interior Layout 07-10009-A 07-10009-00-FP 3rd man crew seat - Fixed parts 07-15009-A 07-15009-00-CI Pilot and copilot crashworthy seats 07-22005-A 07-22005-00-FP 14 crashworthy wall mounted foldable seat installation - Fixed Parts 07-22005-A 07-22005-00-RP 14 crashworthy wall mounted foldable seat installation - Removable Parts 07-24008-A 07-24008-00-FP Operator sliding crashworthy seat- Fixed parts 07-24008-A 07-24008-00-RP Operator sliding crashworthy seat- Removable Parts 07-24010-A 07-24010-00-FP Second operator sliding crashworthy seat - Fixed Parts 07-24010-A 07-24010-00-RP Second operator sliding crashworthy seat - Removable Parts 07-30007-A 07-30007-00-CI Comfort upholstery with improved sound-proofing 07-60006-A 07-60006-00-CI SAR Layout in the intermediate structure with bulkhead 07-70012-A 07-70012-00-CI Life Port medical mount package 07-72022-A 07-72022-00-CI Life Port provisions deck Avionics 08-00016-A 08-00016-02-CI Civil Use minimum equipment (IFR dual pilot) including: Collins - Proline21 - VHF/AM #1 Collins - Proline21 - VHF/AM #2 NAT DACS ICS - Basic set : 3 control panels in cockpit Collins - TDR94D - 008 Collins - Proline21 - DME Collins - Proline21 VOR/ILS/MKR #2 Collins - Proline21 VOR/ILS/MKR/ADF #1 Serpe - IESM Kannad 406 AP - Emergency Locator Transmitter 08-10016-A 08-10016-00-CI Collins - HF9X00 HF/SSB 08-12025-A 08-12025-00-CI NAT - NPX138 VHF/FM-H 08-16026-A 08-16026-00-CI NAT DACS ICS - Complementary set : 4th control panel 08-16027-A 08-16027-00-CI NAT DACS ICS - Complementary set : 5th control panel 08-17049-A 08-17049-00-CI NAT - Passenger Adress Configuration continued on next page 225 09.101.01 E 20
Document reference Avionics Commercial reference Name Technical Data 08-20001-A 08-20001-01-CI SAR Modes navigation package with centralized radio management system including: Thales - AHV16-2nd Radio altimeter Canadian Marconi - CMA5024 - GPS receiver Second Canadian Marconi - CMA5024 - GPS receiver Canadian Marconi - CMA9000 - Flight Management System, with SAR modes Second Canadian Marconi - CMA9000 - Flight Management System, with SAR modes Automatic transition and hover modes Centralized radio management system by FMS 08-22041-A 08-22041-00-CI R4 AIS Transponder 08-27039-A 08-27039-00-CI Chelton DF935 V/UHF DF 08-31039-A 08-31039-00-CI Telephonics 1600 Weather Radar, displayed on AHCAS 08-35009-A 08-35009-01-CI TCAS - GOODRICH - HP 899 integrated to AHCAS 08-35015-A 08-35015-00-CI EGPWS - HONEYWELL - MKXXII integrated to AHCAS 08-46005-A 08-46005-00-CI Moving map EUROAVIONICS EURONAV V linked to GPS 08-65305-A 08-65035-00-CI Skyquest 20" HD display 08-83004-A 08-83004-01-CI M'ARMS Health & Usage Monitoring System (HUMS) with HOMP & Allied Combi-lite CVFDR 08-85008-A 08-85008-00-CI VDRV 3000 - Airborne Video / Data Digital Recorder 225 09.101.01 E 21
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5- Optional equipment Note: weight breakdown values are given for information and shall not be considered as contractual. Document reference Commercial reference Name kg lb General equipment 05-03006-A 05-03006-00-CI First aid kit - JAR OPS 3 compatible 1.6 3.5 05-21011-A 05-21011-00-FP Wire strike protection system - Fixed Parts 2.1 4.6 05-21011-A 05-21011-00-RP Wire strike protection system - Removable Parts 11.2 24.6 05-22001-A 05-22001-00-CI Multipurpose engine air intakes (anti-sand and anti-ice filters) 05-25014-A 05-25014-00-CI Main rotor blades re-inforced sand erosion protection strip (loose equipment delivered separately) 05-25015-A 05-25015-00-CI Tail rotor blades re-inforced sand erosion protection strip (loose equipment delivered separately) 72.7 160.2 0.4 0.8 0.2 0.4 05-26007-A 05-26007-00-CI Dinol AV30 re-inforced anti-corrosive treatment 14.6 32.1 05-31052-A 05-31052-00-CI Enlarged cabin grey tinted windows 16.4 36.1 05-31039-A 05-31039-00-CI 2 observation bubble windows on cabin plug-in doors 1.0 2.2 05-35002-A 05-35002-00-CI Cabin floor for crashworthy seats 38.9 85.7 05-39002-A 05-39002-00-CI Illuminated Map Holder - JAR OPS 3 compatible 1.0 2.2 05-42021-A 05-42021-00-FP Air conditioning system - Fixed Parts (for cockpit and cabin) 43.5 95.9 05-42021-A 05-42021-00-RP1 Air conditioning system - Removable Parts 1 (cabin power unit) 05-42021-A 05-42021-00-RP2 Air conditioning system - Removable Parts 2 (cockpit power unit) 41.1 90.6 40.7 89.7 05-50001-A 05-50001-00-CI Installation for flight in icing conditions 164.8 363.3 05-50002-A 05-50002-00-CI Installation for flight in extreme cold weather On request 05-50003-A 05-50003-00-CI Kit for flight in limited icing conditions (submitted approval by local Airworthiness Authority) 2.0 4.4 05-51001-A 05-51001-00-CI De-iced cockpit center pane with wiper 5.2 11.4 05-52006-A 05-52006-00-CI Goodrich Icing severity indicator 3.0 6.6 225 09.101.01 E 23
Document reference Commercial reference Name kg lb General equipment (continued) 05-64000-A 05-64000-00-CI Auxiliary Power Unit 117.1 258.1 05-65000-A 05-65000-00-CI Hydro electric group 19.0 41.8 05-67003-A 05-67003-00-CI 220 V / 50 Hz AC power socket in cabin 0.8 1.7 05-81004-A 05-81004-00-FP Additional Energy Absorbing pod fuel tanks - Fixed Parts 98.3 26.8 05-81004-A 05-81004-00-RP Additional Energy Absorbing pod fuel tanks - Removable Parts 98.3 216.7 05-81031-A 05-81031-00-CI Energy absorbing central auxiliary fuel tank 318 l (84 US gal) 27.5 60.6 05-82005-A 05-82005-00-CI Pressure refuelling on the ground 24.3 53.7 05-82005-A 05-82005-01-CI Pressure refuelling on the ground (air conditioning compatible) 24.3 53.7 05-92014-A 05-92014-00-FP Main rotor blade folding system - Fixed Parts 3.2 7.0 05-92014-A 05-92014-00-RP Main rotor blade folding system - Removable Parts 81.3 178.5 05-93004-A 05-93004-00-CI Naval mooring 3.7 8.2 05-93006-A 05-93006-00-CI Lashing rings for main landing gear 0.9 1.9 Specific mission equipment 06-20003-A 06-20003-00-FP Double hoist installation - Fixed Parts 15.0 33.1 06-20003-A 06-20003-A 06-20003-00-RP1 Double hoist installation - Removable Parts (Main Hoist & Beam) 06-20003-00-RP2 Double hoist installation - Removable Parts (Backup Hoist) 112.3 247.5 35.0 77.1 06-21015-A 06-21015-00-FP Goodrich 28V electrical hoist (290ft, 600lb) - Fixed Parts 15.0 33.0 06-21015-A 06-21015-00-RP Goodrich 28V electrical hoist (290ft, 600lb) - Removable Parts 99.2 218.6 06-24007-A 06-24007-00-FP Fast roping installation on both sides - Fixed Parts 5.7 12.6 06-24007-A 06-24007-00-RP Fast roping installation on both sides - Removable Parts 1 71.5 157.6 06-25004-A 06-25004-00-CI Drip tub 7.0 15.4 06-26006-B 06-26006-01-FP External mirrors (including 1 electrical) - Fixed parts 0,3 0.6 06-26006-B 06-26006-01-RP External mirrors (including 1 electrical) - Removable Parts 5,6 12.3 06-27013-A 06-27013-00-FP Cargo sling with dynamometer 3,8 Tons - Fixed Parts 8.5 18.7 06-27013-A 06-27013-00-RP Cargo sling with dynamometer 3,8 Tons - Removable Parts 27.7 61.1 1 Removable Parts of this installation are not certified. 225 09.101.01 E 24
Document reference Commercial reference Name kg lb Specific mission equipment (continued) 06-27020-A 06-27020-00-FP Cargo sling with dynamometer 4,5 Tons - Fixed Parts 4.4 9.7 06-27020-A 06-41003-A 06-27020-00-RP Cargo sling with dynamometer 4,5 Tons - Removable Parts 1 06-41003-00-CI Hella anti collision strobe light system (instead of standard one) 28.2 62.2 6.5 14.3 06-41004-A 06-41004-00-CI Soderberg anti collision light (belly mounted) 1.0 2.2 06-42012-A 06-42012-00-CI Fixed lights in the sponsons 5 11.0 06-43005-A 06-43005-00-CI Vertical light for hoisting and sling operation surveillance 6.7 14.8 06-45017-A 06-45017-00-FP Search light Spectrolab SX 16 - Fixed Parts 4.9 10.8 06-45017-A 06-45017-00-RP Search light Spectrolab SX 16 - Removable Parts 24.0 52.9 06-45043-A 06-45043-00-FP Trakka Search Light - Fixed Parts 6.2 13.6 06-45043-A 06-45043-00-RP Trakka Search Light - Removable Parts 25.9 57.0 06-51xxx-A 06-51xxx-00-CI FLIR On request 06-60004-A 06-61011-A 06-60004-00-CI 2 Life rafts - 18 to 27 pax - in the multipurpose sponsons with jettison control in cockpit 2 06-61011-00-FP Emergency floatation gear with automatic firing - Fixed Parts 125.0 275.6 23.1 50.9 06-61011-A 06-61011-00-RP Emergency floatation gear with automatic firing - Removable Parts 151.3 333.5 06-64002-A 06-64002-00-CI Sea anchor 2.9 6.4 06-65008-A 06-65008-00-CI 3rd hand held fire extinguisher - JAR OPS 3 compatible 2.2 4.9 06-65010-A 06-65010-00-CI 2 Flashlights - JAR OPS 3 compatible 1.2 2.6 06-66004-A 06-66004-00-CI Helicopter Emergency Egress Lighting (HEEL) 5.3 11.7 06-67023-A 06-67023-00-CI HR Smith serie 503 - ADELT 8.2 18.1 06-68008-A 06-68008-00-CI Dukane DK120 Underwater Acoustic Beacon 0.5 1.1 06-69002-A 06-69002-00-CI Automatic Voice Alarm Device (AVAD) 3 1.5 3.3 06-70008-A 06-70008-00-CI NVG compatible cockpit lighting 6.7 14.77 06-81018-A 06-81018-00-CI Fire fighting kit (up to 4000 liters) 475.0 1047.1 1 Requires to remove the central auxiliary fuel tank if it has been selected by the user. 2 Required for JAR OPS 3. 3 Incompatible with EGPWS optional. 225 09.101.01 E 25
Document reference Commercial reference Name kg lb Interior Layout 07-10008-A 07-10008-00-CI Pilot and copilot Airline seats leader type 18.2 40.1 07-10009-A 07-10009-00-FP 3rd man crew seat - Fixed Parts 0.2 0.4 07-10009-A 07-10009-00-RP 3rd man crew seat - Removable Parts 6.2 13.7 07-15009-A 07-15009-00-CI Pilot and copilot crashworthy seats 6.7 14.7 07-27002-A 07-27002-00-CI 19 crashworthy seat installation 219.1 483.03 07-30007-A 07-30007-00-CI Comfort upholstery with improved sound proofing 93.4 205.9 07-30008-A 07-30008-00-CI "De Luxe" upholstery with enhanced sound proofing On request 07-50014-A 07-50014-00-CI Special RH double door 7.0 15.4 07-50017-A 07-50017-00-CI Special LH door with built-in steps 15.0 33.1 07-60009-A 07-60009-00-FP Lugage Compartment in Pod Fixed Parts 3.4 7.5 07-60009-A 07-60009-00-RP Lugage Compartment in Pod Removable Parts 30 66.1 07-60016-A 07-60016-00-CI Luggage compartment in the intermediate structure 70.3 154.9 07-70002-A 07-70002-00-CI Self Contained Medical Unit 243.0 535.8 07-70003-A 07-71013-A 07-74007-A 07-70003-00-CI Air Ambulance Technology EMS quick conversion kit (2 units of 3 stretchers each) 07-71013-02-CI Casualty carrying installation for 11 stretchers (without stretchers and seats) 1 07-74007-00-CI Stretcher (NATO type) (loose equipment delivered separately) 2 On request 22.6 49.82 8.3 18.3 07-80002-A 07-80002-00-CI 10 + 1 crashworthy seats VIP installation with bar and toilet On Request 07-80008-A 07-80008-00-CI 12 crashworthy seats VIP installation with bar and toilet On Request 07-80020-A 07-80021-A 07-80020-00-CI 8 + 1 crashworthy seats VIP installation with bar and toilet (1 lounge) 07-80021-00-CI 8 + 1 crashworthy seats VIP installation with bar and toilet (2 lounges) On Request On Request 07-82001-A 07-82001-00-CI Retractable armrests On request 07-82002-A 07-82002-00-CI Lombar adjustment On request 07-83002-A 07-83002-00-CI Electric curtains On request 07-84001-A 07-84001-00-CI Customized inlaid wood table On request 07-85001-A 07-85001-00-CI Transparent central partition with storage compartment On request 07-91002-A 07-91002-00-CI Gold finishing of cabin visible metallic parts On request 1 Removable Parts of this installation are not certified. 2 Equipment is not certified. 225 09.101.01 E 26
Various Possibilities of the EC225 Cabin Installation Passenger transport Crew Change Corporate VIP 8 + 1 VIP crashworthy seats with bar and toilet (with 1 or 2 lounges) or Seating 19 crashworthy seats 10 + 1 VIP crashworthy seats with bar and toilet or 12 VIP crashworthy seats with bar and toilet Upholstery Standard upholstery or Comfort upholstery De Luxe upholstery Doors Standard sliding doors Special LH door with built-in steps and Special RH double door Rear Luggage compartment with standard rear access door Standard rear access door 225 09.101.01 E 27
Document reference Commercial reference Name kg lb Avionics 08-00016-A 08-00016-02-CI Civil Uses minimum equipment (IFR dual pilot) 65 143.3 including: Collins - Proline21 - VHF/AM #1 Collins - Proline21 - VHF/AM #2 NAT DACS ICS - Basic set : 3 control panels in cockpit Collins - TDR94D - 008 Collins - Proline21 - DME Collins - Proline21 VOR/ILS/MKR #2 Collins - Proline21 VOR/ILS/MKR/ADF #1 Serpe - IESM Kannad 406 AP - Emergency Locator Transmitter 1 08-16016-A 08-10016-00-CB Collins - HF 9X00 - HF/SSB - Capabilities 11.3 24.9 08-10016-A 08-10016-00-CI Collins - HF 9X00 - HF/SSB 24.3 53.6 08-12025-A 08-12025-00-CI NAT - NPX138 VHF/FM-H 5.0 11.0 08-13008-A 08-13008-00-CI Chelton - 805-1 UHF #1 6.0 13.2 08-15510-A 08-15510-00-CI AIRCELL 3100 Satcom System integrated to ICS 10.4 22.9 08-16026-A 08-16026-00-CI NAT DACS ICS - Complementary set : 4th control panel 3.8 8.37 08-17009-A 08-17033-A 08-17009-00-CI Cabin entertainment System (CD+DVD) with 4 personal LCD 08-17033-00-CI Cabin entertainment System (CD+DVD) with 8 personal LCD 14.0 30.8 22.0 48.5 08-17037-A 08-17037-00-CI VIP interphone 8.3 18.3 08-17049-A 08-17049-00-CI NAT passenger adress 18.4 40.56 08-18020-A 08-18020-00-CI David Clark H10-13H - Headset 0.5 1.1 08-20001-A 08-20001-00-CI SAR Modes navigation package including: 47.3 104.2 Thales - AHV16-2nd Radio altimeter Canadian Marconi - CMA5024 - GPS receiver Second Canadian Marconi - CMA5024 - GPS receiver Canadian Marconi - CMA9000 - Flight Management System, with SAR modes Second Canadian Marconi - CMA9000 - Flight Management System, with SAR modes Automatic transition and hover modes 1 Acceptance by local airworthiness authorities to be checked. 225 09.101.01 E 28
Document reference Commercial reference Name kg lb 08-20001-A 08-20001-01-CI SAR Modes navigation package with centralized radio management system including: Thales - AHV16-2nd Radio altimeter Canadian Marconi - CMA5024 - GPS receiver Second Canadian Marconi - CMA5024 - GPS receiver Canadian Marconi - CMA9000 - Flight Management System, with SAR modes Second Canadian Marconi - CMA9000 - Flight Management System, with SAR modes Automatic transition and hover modes Centralized radio management system by FMS 60,6 133.6 08-21006-A 08-21006-00-CI Thales - AHV16-2nd Radio altimeter 5.8 12.7 08-24007-A 08-24007-00-CI Collins - Proline 21 - ADF #2 6.2 13.6 08-27039-A 08-27039-00-CI Chelton DF935 V/UHF DF 9.9 21.8 08-31039-A 08-31039-00-CI Telephonics 1600 Weather Radar, displayed on AHCAS 24.0 52.9 08-35009-A 08-35009-01-CI TCAS - GOODRICH - HP 899 integrated to AHCAS 8.8 19.4 08-35015-A 08-35015-00-CI EGPWS - HONEYWELL - MKXXII integrated to AHCAS 1 8.6 18.9 08-41012-A 08-41012-00-CI Canadian Marconi - CMA3024 - GPS receiver 4.9 10.8 1 Incompatible with optional item Automatic Voice Alarm Device (AVAD). 225 09.101.01 E 29
Document reference Commercial reference Name kg lb Avionics (continued) 08-44040-A 08-44043-A 08-44040-00-CI Canadian Marconi - CMA9000 - Flight Management System 08-44043-00-CI Canadian Marconi - CMA9000 - Flight Management System, with SAR modes 8.3 18.2 12.3 27.1 08-47008-A 08-47008-00-CI Marconi - ANV 353 - Doppler radar 11.7 25.7 08-74007-A 08-74007-00-CI Automatic transition and hover modes 4.0 8.8 08-81007-A 08-81007-00-CI CV/FDR Allied Signal + MFDAU - Crash recorder 1 35.0 77.2 08-83004-A 08-83004-A 08-83004-00-CI M'ARMS Health & Usage Monitoring System (HUMS) with Allied Combi-lite CVFDR 1 2 3 08-83004-01-CI M'ARMS Health & Usage Monitoring System (HUMS) with HOMP & Allied Combi-lite CVFDR 1 2 3 34.9 76.9 42.0 92.6 Operational Protection 10-45002-A 10-45002-00-CI Missile Warning System On request 10-51013-A 10-51013-00-FP Chaff and flares dispenser installation - Fixed Parts On request 10-51013-A 10-51013-00-RP Chaff and flares dispenser installation - Removable Parts On request 1 Compatible with JAR OPS-3 regulation. 2 The toolings of the installation are not included in the price. 3 At least one ground station per helicopter base must be purchased. 225 09.101.01 E 30
Blank 225 09.101.01 E 31
6- Main performance The following performance values and figures refer to an EC225, equipped with new engines Makila 2A1. Unless otherwise specified, the values and figures refer to a clean helicopter at Sea Level (SL), in International Standard Atmosphere (ISA) and zero wind condition. Performance on 2 engines Gross Weight kg 9,000 9,500 10,000 10,500 11,000 lb 19,842 20,944 22,046 23,149 24,251 Maximum speed, VNE km/h 324 324 324 324 324 kts 175 175 175 175 175 Maximum cruise speed (at MCP) km/h 275 273 270 266 262 kts 149 148 146 144 142 Recommended cruise speed km/h 261 262 263 265 262 kts 141 141 142 143 142 Fuel consumption at recommended cruise speed kg/h 608 620 632 649 655 lb/h 1,340 1,367 1,393 1,431 1,444 Rate of climb (80kt, 2 engines at MCP) m/s 8.7 7.8 6.9 6.1 5.4 ft/mn 1,709 1,529 1,362 1,208 1,064 Hover Ceiling IGE (at Take-off power, 10 ft) ISA m 3,888 3,370 2,874 2,396 1,935 ft 12,756 11,058 9,431 7,861 6,350 ISA+20 m 3,197 2,679 2,178 1,648 1,141 ft 10,487 8,788 7,144 5,407 3,743 Hover Ceiling OGE (at Take-off power) ISA m 3,099 2,572 2,065 1,578 792 ft 10,166 8,438 6,776 5,176 2,600 ISA+20 m 2,389 1,812 1,261 731 93 ft 7,838 5,946 4,138 2,398 305 Service ceiling (Vz=0.508m/s = 100ft/mn) m 5,918 5,413 4,933 4,469 4,041 ft 19,417 17,760 16,185 14,661 13,257 225 09.101.01 E 32
Gross Weight kg 9,000 9,500 10,000 10,500 11,000 lb 19,842 20,944 22,046 23,149 24,251 Maximum range (without reserve, at economical cruise speed) standard tanks km 887 876 865 852 838 nm 479 473 467 460 452 standard + central tanks km 1,000 988 976 961 946 nm 540 534 527 519 511 standard + central tanks + pod km 1,197 1,185 1,169 1,152 1,135 nm 646 640 631 622 613 Maximum endurance without reserve, at 148km/h = 80kts) standard tanks h:mn 4:32 4:24 4:17 4:11 4:5 standard + central tanks h:mn 5:08 4:59 4:51 4:44 4:37 standard + central tanks + pod h:mn 6:16 6:05 5:55 5:46 5:38 225 09.101.01 E 33
Performance on 1 engine Gross Weight kg 9,000 9,500 10,000 10,500 11,000 lb 19,842 20,944 22,046 23,149 24,251 Rate of climb (80kt, 1 engines at OEI unlimited) m/s 4.3 3.6 2.9 2.3 1.7 ft/mn 850 709 577 453 334 Service ceiling (80kt, 1 engines at OEI unlimited) m 3,066 2,519 1,971 1,453 970 Vz=0.508m/s = 100ft/mn ft 10,061 8,265 6,465 4,768 3,184 Operating limitations The helicopter is cleared to be operated within the following altitude and temperature limitations (according to Flight Manual). For complementary information, refer to Flight Manual: Maximum altitude Flight Take-off and landing 6,095 m 20,000 ft (PA) 3,353 m 11,000 ft (DA) Maximum temperature ISA + 40 C limited to 50 C Minimum temperature -30 C (standard configuration) -45 C (requires the installation of kit for flight in extreme cold weather to be contracted separately) Abbreviations AEO : All Engines Operative SL : Sea Level DA : Density Altitude TAS True Air Speed IGE : In Ground Effect VNE : Never Exceed Speed ISA : International Standard Atmosphere Vz : Rate-of-climb MCP : Maximum Continuous Power Zp : Barometric Altitude OEI : One Engine Inoperative Vp : Airspeed OGE : Out of Ground Effect Vmax : Maximum cruise speed PA : Pressure Altitude Vreco : Economical cruise speed Units nm : nautical miles hr:min : hours:minutes kts: knots kg : kilograms ft/min : feet/minute lb : pounds m/sec : meters per seconds km : kilometres C : degrees Celsius kg/hr : kilograms per hour 225 09.101.01 E 34
Performance charts The performance charts presented hereafter apply to a clean aircraft as per the standard definition, with external sponsons. Take-off weight in hover IGE, AEO 5 min (10 ft, on 2 engines, at take-off power, no wind) Take-off weight in hover OGE, AEO 5 min (on 2 engines, at take-off power, no wind) Page 36 Page 37 Take-off weight from a clear area (EASA Category A) Page 38 Fast cruise speed Zp = 0, ISA (on 2 engines at maximum continuous power) Fast cruise speed Zp = 0, ISA + 20 C (on 2 engines at maximum continuous power) Rate of climb in oblique flight (on 2 engines at maximum continuous power - ISA; T.A.S. = 80 kts) Rate of climb in oblique flight (on 2 engines at maximum continuous power ISA + 20 C; T.A.S. = 80 kts) Rate of climb in oblique flight (on 1 engine OEI unlimited, ISA ; T.A.S = 80 kts) Rate of climb in oblique flight (on 1 engine OEI unlimited, ISA + 20 C ; T.A.S = 80 kts) Page 39 Page 40 Page 41 Page 42 Page 43 Page 44 Hourly fuel consumption (SL, ISA) Page 45 Hourly fuel consumption (SL, ISA + 20 C) Page 46 Hourly fuel consumption (Zp = 5000ft, ISA) Page 47 Hourly fuel consumption (Zp = 5000ft, ISA + 20 C) Page 48 Payload / Range Chart (SL, ISA) Page 49 Payload / Range Chart (SL, ISA + 20 C) Page 50 225 09.101.01 E 35
11000 Technical Data Take-off weight in hover IGE, AEO 5 min 10 ft, on 2 engines, at take-off power 20000 Pressure altitude (ft) ISO-Weight (kg) 7500 7000 ISA ISA+ 20 8000 15000 8500 ISA+ 35 9000 ISA-20 9500 10000 10000 10500 5000 0-30 -20-10 0 10 20 30 40 50 OAT ( C) 225 09.101.01 E 36
Take-off weight in hover OGE, AEO 5 min on 2 engines, at take-off power 20000 Pressure altitude (ft) ISO-Weight (kg) 7000 ISA ISA+ 20 7500 15000 8000 ISA+ 35 8500 ISA-20 9000 10000 9500 10000 10500 5000 11000 0-30 -20-10 0 10 20 30 40 50 OAT ( C) 225 09.101.01 E 37
Take-off weight from a clear area (EASA Category A) 20000 Pressure altitude (ft) ISA+ 35 ISO-Weight (kg) 7000 ISA+ 20 6500 15000 7500 8000 ISA 8500 ISA-20 9000 10000 9500 10000 10500 11000 5000 0-30 -20-10 0 10 20 30 40 50 OAT ( C) 225 09.101.01 E 38
Fast cruise speed Zp = 0, ISA on 2 engines, at maximum continuous power 11000 Weight (kg) (lb) 24000 10000 22000 9000 20000 8000 18000 7000 16000 140 150 T.A.S (kt) 265 275 285 (km/h) 225 09.101.01 E 39
Fast cruise speed Zp = 0, ISA + 20 on 2 engines, at maximum continuous power 11000 Weight (kg) (lb) 24000 10000 22000 9000 20000 8000 18000 7000 16000 140 150 T.A.S (kt) 265 275 285 (km/h) 225 09.101.01 E 40
9500 9000 8500 8000 Technical Data Rate of climb in oblique flight ISA T.A.S. = 80 kts on 2 engines, at maximum continuous power 20000 Pressure Altitude (ft) ISO-Weight (kg) 15000 10000 11000 10500 10000 7500 7000 6500 5000 0 0 500 1000 1500 2000 2500 3000 Rate of climb (ft/mn) 225 09.101.01 E 41
Rate of climb in oblique flight ISA + 20 - T.A.S. = 80 kts on 2 engines, at maximum continuous power 20000 Pressure Altitude (ft) ISO-Weight (kg) 15000 10000 11000 10500 10000 9500 9000 8500 8000 7500 7000 6500 5000 0 0 500 1000 1500 2000 2500 3000 Rate of climb (ft/mn) 225 09.101.01 E 42
Rate of climb in oblique flight ISA - T.A.S. = 80 kts on 1 engine, OEI unlimited Pressure altitude (ft) 20000 ISO-WEIGHT (kg) (m) 6000 15000 5000 4000 10000 3000 5000 2000 11000 10500 10000 1000 9500 9000 8000 8500 7500 7000 6500 0 0 0 500 1000 1500 2000 Rate of climb (ft/mn) 0 10 1 (m/s) 225 09.101.01 E 43
Pressure altitude (ft) 20000 Rate of climb in oblique flight ISA + 20 - T.A.S. = 80 kts on 1 engine, OEI unlimited ISO-WEIGHT (kg) (m) 6000 15000 5000 4000 10000 3000 5000 2000 1000 0 11000 10500 10000 9500 9000 8000 8500 7500 7000 6500 0 0 500 1000 1500 2000 Rate of climb (ft/mn) 0 10 1 (m/s) 225 09.101.01 E 44
Hourly fuel consumption SL, ISA 700 Hourly fuel consumption (kg/h) ISO-Weight (kg) (lb/h) 650 Vmax 1450 600 1350 550 11000 Vreco 1250 10500 1150 500 10000 9500 9000 8500 1050 450 8000 7500 7000 950 6500 400 60 80 100 120 140 160 T.A.S (kt) 150 200 250 (km/h) 225 09.101.01 E 45
Hourly fuel consumption SL, ISA + 20 700 Hourly fuel consumption (kg/h) ISO-Weight (kg) (lb/h) 650 Vmax 1450 600 550 11000 Vreco 1350 1250 10500 10000 1150 500 9500 9000 8500 1050 450 8000 7500 7000 950 6500 400 60 80 100 120 140 160 T.A.S (kt) 150 200 250 (km/h) 225 09.101.01 E 46
8000 Technical Data Hourly fuel consumption Zp = 5000 ft, ISA Hourly fuel consumption (kg/h) 650 ISO-WEIGHT (kg) Vmax 600 Vreco 550 500 11000 10500 10000 9500 450 9000 8500 400 7500 7000 6500 350 60 80 100 120 140 160 T.A.S (kt) 225 09.101.01 E 47
Hourly fuel consumption Zp = 5000 ft, ISA + 20 Hourly fuel consumption (kg/h) 650 ISO-WEIGHT (kg) Vmax 600 Vreco 550 11000 500 10500 10000 9500 450 9000 8500 8000 400 7500 7000 6500 350 60 80 100 120 140 160 T.A.S (kt) 225 09.101.01 E 48
(1) (2) (3) Technical Data PAYLOAD / RANGE CHART SL ISA Payload (kg) MTOW=11000 kg MTOW=11000 kg MTOW=11000kg 5000 4000 3000 2000 1000 0 0 100 200 300 400 500 600 Range (nm) with pilot and copilot ( 160 kg ), no taxying, no reserve. 1 : Standard tanks 2 : Standard tanks + central energy absorbing fuel tank 3 : Standard tanks + central energy absorbing fuel tank + pod fuel tanks 225 09.101.01 E 49
(1) (2) (3) Technical Data PAYLOAD / RANGE CHART SL ISA + 20 C Payload (kg) MTOW=11000kg kg MTOW=11000 kg 5000 4000 3000 2000 1000 0 0 100 200 300 400 500 600 Range (nm) with pilot and copilot ( 160 kg ), no taxying, no reserve. 1 : Standard tanks 2 : Standard tanks + central energy absorbing fuel tank 3 : Standard tanks + central energy absorbing fuel tank + pod fuel tanks 225 09.101.01 E 50
7- Customer Service Overview Assets Proven reliability and availability based on experience EUROCOPTER s helicopter production programs have developed a strong reputation world-wide for being fully committed to providing customers with operational, capable aircraft that achieve high availability combined with cost-effective support systems. To achieve this record of performance, EUROCOPTER has stressed the importance of working together with its customers to ensure constant feedback on their demonstrated in-service Reliability, Availability and Maintainability/Testability (RAM) data. The main objective is to reach the most optimized operational cost ensuring the highest flight safety. EUROCOPTER has built and delivered SUPER PUMA and COUGAR variants for more than twenty five years. The combined population of the SUPER PUMA and COUGAR family is close to 702 helicopters in service world-wide. The total flight hours accumulated at this date are about 3,775,534 hours. The lead the fleet aircraft has accumulated 37,000 flight hours. 225 09.101.01 E 51
Inspection Program The Maintenance Program, as described in the Maintenance Manual, is to be considered as a basis for each customer individual program set up. The Maintenance Program specifies the intervals between maintenance operations that are recommended by EUROCOPTER, 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. The following table provides an overview of all inspections. Scheduled inspections with shorter time intervals have to be added to those with longer time intervals. Scheduled Airframe Inspection Daily checks : Flight Related Checks 15 flight hrs or 7 days Estimated Man Hour Pilot s task 0,75 MMH 75 flight hrs periodicity tasks 13,30 MMH 750 flight hrs or 24 months periodicity tasks 210 MMH Airframe Major Inspection Estimated Man Hour 16 years periodicity tasks 1200 MMH Scheduled Engine Inspection MAKILA 2A1 Estimated Man Hour 15 flight hrs periodicity tasks 75 flight hrs periodicity tasks 0,1168 MMH per FH MMH: Mean Man Hour 750 flight hrs periodicity tasks Note : All the hands-on aircraft values mentioned here above are given on the basis of a 20 000 flight hours 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 Man Hours are without incoming flight, work preparation, reworking, servicing, Service Bulletin implementation and unscheduled maintenance. 225 09.101.01 E 52
Main components Time Between Overhaul (TBO) / Service Life Limit (SLL) 1 Main Components TBO (h) as per MSM 2008 Ed. ALTERNATOR 40 KVA 3000 TBO (h) Target Value * SLL (h) as per MSM 2008 Ed. AUXILARY HYDRAULIC PUMP 3000 5000 MAIN ROTOR AND TAIL ROTOR BLADES 20000 MAIN ROTOR HUB OC BENDIX ENGINE-MGB COUPLING SHAFT ASSY 4800 MGB MAIN MODULE 2000 3000 MGB EPYCICLIC MODULE 2000 3000 MGB ACCESSORY DRIVE GEAR BOX LH 2000 3000 MGB ACCESSORY DRIVE GEAR BOX RH 3000 4000 MGB SUPPORT FLEX PLATE 6200 TAIL GEAR BOX 3000** INTERMEDIATE GEAR BOX 3000** MAIN SERVO CONTROL 3750 5000 TAIL SERVO CONTROL 3000 ** 5000 MAKILA 2A1 2750** 3750 * : Target value within the Maturity Plan under progress. ** = in MSM first half 2009 Engines TBO (h) as per MSM rev RT003b TBO (h) Target Value * MAKILA 2A1 2500 3000 * : Target value within the Maturity Plan under progress. SLL (h) as per MSM rev RT003b Time Between Overhauls (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. A TBO is granted with a 10 % operational margin, limited at +300 hours. Some subcomponents may have a Service Life limit, rated above the TBO limit. Service Life Limited (SLL): The service life limit is an airworthiness limit. The component in question must be removed from service when it reaches the limit indicated. 1 Main component values are given for information purposes only. The reference document is the aircraft Maintenance Program Manual. 225 09.101.01 E 53
Eurocopter Maintenance Support Programs EUROCOPTER offers its clients a comprehensive array of repair and overhaul services to ensure availability and costs control. This array of services ranges from basic OEM repair and overhaul services up to comprehensive Parts By the Hour (PBH) maintenance programs. The different services are each tailored for one different user profiles and demands, such as customers : with a high number of flight hours, with a low number of flight hours, looking for immediate component availability, that wish budget control, To respond to the different customers demands EUROCOPTER offers the following flexible and modular services: Classic Support Maintenance, Repair and Overhaul Standard exchange Guaranteed Direct Maintenance Costs (DMC) Unscheduled Maintenance Insurance Plan Parts by the Hour service On request, EUROCOPTER is able to propose extensive services adapted to specific mission and customer expectations, as stock and maintenance management. Classic Support The classic support consists of a comprehensive Initial Provisioning package to sustain aircraft operation. This package includes Spare Parts, Tools, Test Equipment, etc... The required level of operational availability determines the quantity and therefore the investment required. With this support package the Customer bears the responsibility to monitor their repair; manage obsolescence and to procure the right mix and quantity of components and spare parts. Maintenance, Repair and Overhaul EUROCOPTER offers a complete range of industry-leading inspection, repair and overhaul capabilities for the full range of EUROCOPTER helicopters, with guaranteed turn-around times and cost-efficiency. Approved by the most stringent airworthiness authorities in the world, our industrial facilities ensure the highest quality for the maintenance, repair and upgrading works. EUROCOPTER Maintenance Repair and Overhaul covers the four major following areas: - Blades - Equipment - Dynamic component - Maintenance & upgrades 225 09.101.01 E 54
Standard Exchange The Standard Exchange consists in replacing a defective part with a serviceable and interchangeable part within 48 hours subject to availability. This service is available for equipment, blades and dynamic components. Guaranteed DMC (Repair By the Hour) The Guaranteed DMC services offers guaranteed repair and overhaul TATs as well as guaranteed prices. This addition to the classic repair and overhaul enables the customer to best size its inventory. Price for this service is calculated per flight hour, thus enabling the customer to spread and predict both his scheduled as unscheduled maintenance expenses. The guaranteed DMC service is available for dynamic components, blades and basic equipment Unscheduled Maintenance Insurance Plan (UMIP) With the UMIP, EUROCOPTER gives the customer the option to secure unscheduled maintenance costs while remaining responsible for the scheduled events (overhaul, life limited part replacement). Price for this service is calculated per flight hour. The UMIP service includes component unscheduled repairs and guaranteed parts replacement within 24H through Standard Exchange based on a dedicated inventory. This service is available for dynamic components, blades and basic equipment 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, reduced inventory and minimized helicopter downtime. 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. The PBH service includes component unscheduled repairs component overhauls as well as Life Limited part replacement. Parts replacement is guaranteed within 24H through Standard Exchange based on a dedicated inventory. This service is available for dynamic components, blades and equipment. 225 09.101.01 E 55