EC225. Technical Data E

Transcription

1 EC225 Technical Data E

2 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

3 Contents 1 - Foreword General characteristics Baseline Aircraft Definition Recommended Mission Configurations Optional Equipment Main performance Customer Service Overview 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 E 1

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5 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 E 3

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7 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, ,017 4,447 Optional central energy absorbing fuel tank Optional ferry fuel tanks (1 to 5) 5 x x x x 826 Pod fuel tanks E 5

8 Main dimensions m Rotor Rotating ft φ m ft dia φ 3.15 m ft dia 4.60 m ft 4.97 m ft 5.25 m ft m ft 2.00 m 6.56 ft 3.96 m ft 2.12 m 6.95 ft 3.00 m 9.84 ft Dimensions with blades folded 4.10 m ft E 6

9 Dimensions of compartments and accesses Cabin main dimensions Cabin floor E 7

10 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, ,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 E 8

11 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) 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 E 9

12 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 E 10

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14 3 EC225 Baseline Aircraft Definition E 12

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17 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 E 15

18 Mission configuration Document reference Commercial reference Name A CI EC225 Baseline Aircraft A CI "EC225 Offshore" package including: General Equipment A CI First aid kit - JAR OPS 3 compatible A CI Dinol AV30 re-inforced anti-corrosive treatment A CI Enlarged Cabin grey tinted windows A CI Cabin floor for crashworthy seats A CI Enlarged footstep cockpit A CI Enlarged footstep cabin A CI Illuminated Map Holder - JAR OPS 3 compatible A CI Kit for flight in limited icing conditions A CI De-iced cockpit center pane with wiper A CI Goodrich Icing severity indicator A CI Hydro electric group A CI Energy Absorbing central auxiliary fuel tank 318 l (84 US gal) A CI Pressure refuelling on the ground with Energy Absorbing self-sealing sponson fuel tanks Specific Mission Equipment A FP Goodrich 28V electrical hoist (290ft, 600lb) - Fixed parts B FP External mirrors (including one electrical) - Fixed Parts A FP Cargo sling with dynamometer 3,8 Tons - Fixed parts A CI Hella anti collision strobe light system (instead of standard one) A CI Soderberg anti collision light (belly mounted) A CI Fixed lights in the sponsons A CI 2 Life rafts - 18 to 27 pax - in the multipurpose sponsons with jettison control in cockpit A FP Emergency floatation gear with automatic firing - Fixed parts A RP Emergency floatation gear with automatic firing - Removable parts A CI 3rd hand held fire extinguisher - JAR OPS 3 compatible A CI 2 Flashlights - JAR OPS 3 compatible A CI Helicopter Emergency Egress Lighting (HEEL) A CI HR Smith series 503 ADELT Configuration continued on next page E 16

19 Document Commercial reference reference Interior Layout Name A FP 3rd crew man seat - Fixed parts A CI Pilot and copilot crashworthy seats A CI 19 crashworthy seat installation A CI Comfort upholstery with improved soundproofing A CI Luggage compartment in the intermediate structure Avionics A 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 Collins - Proline21 - DME Collins - Proline21 VOR/ILS/MKR #2 Collins - Proline21 VOR/ILS/MKR/ADF #1 Serpe - IESM Kannad 406 AP - Emergency Locator Transmitter A CB Collins - HF 9X00 - HF/SSB - Capabilities A CI NAT - NPX138 VHF/FM-H A CI NAT DACS ICS - Complementary set : 4th control panel A CI NAT- Passenger Address A CI Chelton System 7 - (121,5) VHF/FM Marine dual frequency homer A CI Telephonics 1600 Weather Radar, displayed on AHCAS A CI TCAS - GOODRICH - HP 899 integrated to AHCAS A CI EGPWS - HONEYWELL - MKXXII integrated to AHCAS A CI Canadian Marconi - CMA GPS receiver A CI Canadian Marconi - CMA Flight Management System A CI M'ARMS Health & Usage Monitoring System (HUMS) with HOMP & Allied Combi-lite CVFDR E 17

20 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 E 18

21 Mission configuration Document reference Commercial reference Name A CI EC225 Baseline Aircraft General Equipment A CI First aid kit - JAR OPS 3 compatible A CI Dinol AV30 re-inforced anti-corrosive treatment A CI 2 observation bubble windows on cabin plug-in doors A CI Enlarged cabin grey tinted windows A CI Multipurpose Integrated Crashworthy Floor A CI Illuminated Map Holder - JAR OPS 3 compatible A CI Kit for flight in limited icing conditions A CI De-iced cockpit center pane with wiper A CI Goodrich Icing severity indicator A CI Hydro electric group A CI Energy Absorbing central auxiliary fuel tank 318 l (84 US gal) A CI Pressure refuelling on the ground with Energy Absorbing self-sealing sponson fuel tanks Specific Mission Equipment A FP Double hoist installation - Fixed Parts A RP1 Double hoist installation - Removable Parts (Main Hoist & Beam) A RP2 Double hoist installation - Removable Parts (Backup Hoist) B FP External mirrors (including one electrical) - Fixed Parts A FP Cargo sling with dynamometer 3,8 Tons - Fixed Parts B FP Electrical hailer installation (Qty 1) - Fixed Parts B RP Electrical hailer installation (Qty 1) - Removable Parts A CI Soderberg anti collision light (belly mounted) A CI Fixed lights in the sponsons A CI Swivelable light under right sponson A CI Swivelable light under left sponson A CI Vertical light for hoisting and sling operation surveillance A FP Trakka Search light with infrared filter in-flight changeover - Fixed Parts A RP Trakka Search light with infrared filter in-flight changeover - Removable Parts A CI FLIR Mx15i HD / Trakka Slaving Unit A FP Flir Operator console - Fixed Parts A RP Flir Operator console - Removable Parts A FP Nose mounted FLIR WESCAM MX15i HD - Fixed Parts A RP Nose mounted FLIR WESCAM MX15i HD - Removable Parts Configuration continued on next page E 19

22 Document Commercial reference reference Specific Mission Equipment Name Technical Data A CI 2 Life rafts - 18 to 27 pax - in the multipurpose sponsons with jettison control in cockpit A FP Emergency floatation gear with automatic firing - Fixed Parts A RP Emergency floatation gear with automatic firing - Removable Parts A CI 3rd hand held fire extinguisher - JAR OPS 3 compatible A CI 2 Flashlights - JAR OPS 3 compatible A CI Helicopter Emergency Egress Lighting (HEEL) A CI 2 Portable ELT 406 MHz HR SMITH Personal Locator Serie 500 in liferafts A CI HR Smith serie ADELT A CI NVG compatible cockpit lighting A CI NVG compatible cabin lighting A CI NVG compatible external lighting Interior Layout A FP 3rd man crew seat - Fixed parts A CI Pilot and copilot crashworthy seats A FP 14 crashworthy wall mounted foldable seat installation - Fixed Parts A RP 14 crashworthy wall mounted foldable seat installation - Removable Parts A FP Operator sliding crashworthy seat- Fixed parts A RP Operator sliding crashworthy seat- Removable Parts A FP Second operator sliding crashworthy seat - Fixed Parts A RP Second operator sliding crashworthy seat - Removable Parts A CI Comfort upholstery with improved sound-proofing A CI SAR Layout in the intermediate structure with bulkhead A CI Life Port medical mount package A CI Life Port provisions deck Avionics A 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 Collins - Proline21 - DME Collins - Proline21 VOR/ILS/MKR #2 Collins - Proline21 VOR/ILS/MKR/ADF #1 Serpe - IESM Kannad 406 AP - Emergency Locator Transmitter A CI Collins - HF9X00 HF/SSB A CI NAT - NPX138 VHF/FM-H A CI NAT DACS ICS - Complementary set : 4th control panel A CI NAT DACS ICS - Complementary set : 5th control panel A CI NAT - Passenger Adress Configuration continued on next page E 20

23 Document reference Avionics Commercial reference Name Technical Data A CI SAR Modes navigation package with centralized radio management system including: Thales - AHV16-2nd Radio altimeter Canadian Marconi - CMA GPS receiver Second Canadian Marconi - CMA GPS receiver Canadian Marconi - CMA Flight Management System, with SAR modes Second Canadian Marconi - CMA Flight Management System, with SAR modes Automatic transition and hover modes Centralized radio management system by FMS A CI R4 AIS Transponder A CI Chelton DF935 V/UHF DF A CI Telephonics 1600 Weather Radar, displayed on AHCAS A CI TCAS - GOODRICH - HP 899 integrated to AHCAS A CI EGPWS - HONEYWELL - MKXXII integrated to AHCAS A CI Moving map EUROAVIONICS EURONAV V linked to GPS A CI Skyquest 20" HD display A CI M'ARMS Health & Usage Monitoring System (HUMS) with HOMP & Allied Combi-lite CVFDR A CI VDRV Airborne Video / Data Digital Recorder E 21

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25 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 A CI First aid kit - JAR OPS 3 compatible A FP Wire strike protection system - Fixed Parts A RP Wire strike protection system - Removable Parts A CI Multipurpose engine air intakes (anti-sand and anti-ice filters) A CI Main rotor blades re-inforced sand erosion protection strip (loose equipment delivered separately) A CI Tail rotor blades re-inforced sand erosion protection strip (loose equipment delivered separately) A CI Dinol AV30 re-inforced anti-corrosive treatment A CI Enlarged cabin grey tinted windows A CI 2 observation bubble windows on cabin plug-in doors A CI Cabin floor for crashworthy seats A CI Illuminated Map Holder - JAR OPS 3 compatible A FP Air conditioning system - Fixed Parts (for cockpit and cabin) A RP1 Air conditioning system - Removable Parts 1 (cabin power unit) A RP2 Air conditioning system - Removable Parts 2 (cockpit power unit) A CI Installation for flight in icing conditions A CI Installation for flight in extreme cold weather On request A CI Kit for flight in limited icing conditions (submitted approval by local Airworthiness Authority) A CI De-iced cockpit center pane with wiper A CI Goodrich Icing severity indicator E 23

26 Document reference Commercial reference Name kg lb General equipment (continued) A CI Auxiliary Power Unit A CI Hydro electric group A CI 220 V / 50 Hz AC power socket in cabin A FP Additional Energy Absorbing pod fuel tanks - Fixed Parts A RP Additional Energy Absorbing pod fuel tanks - Removable Parts A CI Energy absorbing central auxiliary fuel tank 318 l (84 US gal) A CI Pressure refuelling on the ground A CI Pressure refuelling on the ground (air conditioning compatible) A FP Main rotor blade folding system - Fixed Parts A RP Main rotor blade folding system - Removable Parts A CI Naval mooring A CI Lashing rings for main landing gear Specific mission equipment A FP Double hoist installation - Fixed Parts A A RP1 Double hoist installation - Removable Parts (Main Hoist & Beam) RP2 Double hoist installation - Removable Parts (Backup Hoist) A FP Goodrich 28V electrical hoist (290ft, 600lb) - Fixed Parts A RP Goodrich 28V electrical hoist (290ft, 600lb) - Removable Parts A FP Fast roping installation on both sides - Fixed Parts A RP Fast roping installation on both sides - Removable Parts A CI Drip tub B FP External mirrors (including 1 electrical) - Fixed parts 0, B RP External mirrors (including 1 electrical) - Removable Parts 5, A FP Cargo sling with dynamometer 3,8 Tons - Fixed Parts A RP Cargo sling with dynamometer 3,8 Tons - Removable Parts Removable Parts of this installation are not certified E 24

27 Document reference Commercial reference Name kg lb Specific mission equipment (continued) A FP Cargo sling with dynamometer 4,5 Tons - Fixed Parts A A RP Cargo sling with dynamometer 4,5 Tons - Removable Parts CI Hella anti collision strobe light system (instead of standard one) A CI Soderberg anti collision light (belly mounted) A CI Fixed lights in the sponsons A CI Vertical light for hoisting and sling operation surveillance A FP Search light Spectrolab SX 16 - Fixed Parts A RP Search light Spectrolab SX 16 - Removable Parts A FP Trakka Search Light - Fixed Parts A RP Trakka Search Light - Removable Parts xxx-A 06-51xxx-00-CI FLIR On request A A CI 2 Life rafts - 18 to 27 pax - in the multipurpose sponsons with jettison control in cockpit FP Emergency floatation gear with automatic firing - Fixed Parts A RP Emergency floatation gear with automatic firing - Removable Parts A CI Sea anchor A CI 3rd hand held fire extinguisher - JAR OPS 3 compatible A CI 2 Flashlights - JAR OPS 3 compatible A CI Helicopter Emergency Egress Lighting (HEEL) A CI HR Smith serie ADELT A CI Dukane DK120 Underwater Acoustic Beacon A CI Automatic Voice Alarm Device (AVAD) A CI NVG compatible cockpit lighting A CI Fire fighting kit (up to 4000 liters) 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 E 25

28 Document reference Commercial reference Name kg lb Interior Layout A CI Pilot and copilot Airline seats leader type A FP 3rd man crew seat - Fixed Parts A RP 3rd man crew seat - Removable Parts A CI Pilot and copilot crashworthy seats A CI 19 crashworthy seat installation A CI Comfort upholstery with improved sound proofing A CI "De Luxe" upholstery with enhanced sound proofing On request A CI Special RH double door A CI Special LH door with built-in steps A FP Lugage Compartment in Pod Fixed Parts A RP Lugage Compartment in Pod Removable Parts A CI Luggage compartment in the intermediate structure A CI Self Contained Medical Unit A A A CI Air Ambulance Technology EMS quick conversion kit (2 units of 3 stretchers each) CI Casualty carrying installation for 11 stretchers (without stretchers and seats) CI Stretcher (NATO type) (loose equipment delivered separately) 2 On request A CI crashworthy seats VIP installation with bar and toilet On Request A CI 12 crashworthy seats VIP installation with bar and toilet On Request A A CI crashworthy seats VIP installation with bar and toilet (1 lounge) CI crashworthy seats VIP installation with bar and toilet (2 lounges) On Request On Request A CI Retractable armrests On request A CI Lombar adjustment On request A CI Electric curtains On request A CI Customized inlaid wood table On request A CI Transparent central partition with storage compartment On request A CI Gold finishing of cabin visible metallic parts On request 1 Removable Parts of this installation are not certified. 2 Equipment is not certified E 26

29 Various Possibilities of the EC225 Cabin Installation Passenger transport Crew Change Corporate VIP VIP crashworthy seats with bar and toilet (with 1 or 2 lounges) or Seating 19 crashworthy seats 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 E 27

30 Document reference Commercial reference Name kg lb Avionics A CI Civil Uses 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 Collins - Proline21 - DME Collins - Proline21 VOR/ILS/MKR #2 Collins - Proline21 VOR/ILS/MKR/ADF #1 Serpe - IESM Kannad 406 AP - Emergency Locator Transmitter A CB Collins - HF 9X00 - HF/SSB - Capabilities A CI Collins - HF 9X00 - HF/SSB A CI NAT - NPX138 VHF/FM-H A CI Chelton UHF # A CI AIRCELL 3100 Satcom System integrated to ICS A CI NAT DACS ICS - Complementary set : 4th control panel A A CI Cabin entertainment System (CD+DVD) with 4 personal LCD CI Cabin entertainment System (CD+DVD) with 8 personal LCD A CI VIP interphone A CI NAT passenger adress A CI David Clark H10-13H - Headset A CI SAR Modes navigation package including: Thales - AHV16-2nd Radio altimeter Canadian Marconi - CMA GPS receiver Second Canadian Marconi - CMA GPS receiver Canadian Marconi - CMA Flight Management System, with SAR modes Second Canadian Marconi - CMA Flight Management System, with SAR modes Automatic transition and hover modes 1 Acceptance by local airworthiness authorities to be checked E 28

31 Document reference Commercial reference Name kg lb A CI SAR Modes navigation package with centralized radio management system including: Thales - AHV16-2nd Radio altimeter Canadian Marconi - CMA GPS receiver Second Canadian Marconi - CMA GPS receiver Canadian Marconi - CMA Flight Management System, with SAR modes Second Canadian Marconi - CMA Flight Management System, with SAR modes Automatic transition and hover modes Centralized radio management system by FMS 60, A CI Thales - AHV16-2nd Radio altimeter A CI Collins - Proline 21 - ADF # A CI Chelton DF935 V/UHF DF A CI Telephonics 1600 Weather Radar, displayed on AHCAS A CI TCAS - GOODRICH - HP 899 integrated to AHCAS A CI EGPWS - HONEYWELL - MKXXII integrated to AHCAS A CI Canadian Marconi - CMA GPS receiver Incompatible with optional item Automatic Voice Alarm Device (AVAD) E 29

32 Document reference Commercial reference Name kg lb Avionics (continued) A A CI Canadian Marconi - CMA Flight Management System CI Canadian Marconi - CMA Flight Management System, with SAR modes A CI Marconi - ANV Doppler radar A CI Automatic transition and hover modes A CI CV/FDR Allied Signal + MFDAU - Crash recorder A A CI M'ARMS Health & Usage Monitoring System (HUMS) with Allied Combi-lite CVFDR CI M'ARMS Health & Usage Monitoring System (HUMS) with HOMP & Allied Combi-lite CVFDR Operational Protection A CI Missile Warning System On request A FP Chaff and flares dispenser installation - Fixed Parts On request A 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 E 30

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34 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 kts Maximum cruise speed (at MCP) km/h kts Recommended cruise speed km/h kts Fuel consumption at recommended cruise speed kg/h lb/h 1,340 1,367 1,393 1,431 1,444 Rate of climb (80kt, 2 engines at MCP) m/s 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, ft 10,166 8,438 6,776 5,176 2,600 ISA+20 m 2,389 1,812 1, ft 7,838 5,946 4,138 2, 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, E 32

35 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 nm standard + central tanks km 1, nm standard + central tanks + pod km 1,197 1,185 1,169 1,152 1,135 nm 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: E 33

36 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 ft/mn Service ceiling (80kt, 1 engines at OEI unlimited) m 3,066 2,519 1,971 1, 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 E 34

37 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 E 35

38 11000 Technical Data Take-off weight in hover IGE, AEO 5 min 10 ft, on 2 engines, at take-off power Pressure altitude (ft) ISO-Weight (kg) ISA ISA ISA ISA OAT ( C) E 36

39 Take-off weight in hover OGE, AEO 5 min on 2 engines, at take-off power Pressure altitude (ft) ISO-Weight (kg) 7000 ISA ISA ISA ISA OAT ( C) E 37

40 Take-off weight from a clear area (EASA Category A) Pressure altitude (ft) ISA+ 35 ISO-Weight (kg) 7000 ISA ISA 8500 ISA OAT ( C) E 38

41 Fast cruise speed Zp = 0, ISA on 2 engines, at maximum continuous power Weight (kg) (lb) T.A.S (kt) (km/h) E 39

42 Fast cruise speed Zp = 0, ISA + 20 on 2 engines, at maximum continuous power Weight (kg) (lb) T.A.S (kt) (km/h) E 40

43 Technical Data Rate of climb in oblique flight ISA T.A.S. = 80 kts on 2 engines, at maximum continuous power Pressure Altitude (ft) ISO-Weight (kg) Rate of climb (ft/mn) E 41

44 Rate of climb in oblique flight ISA T.A.S. = 80 kts on 2 engines, at maximum continuous power Pressure Altitude (ft) ISO-Weight (kg) Rate of climb (ft/mn) E 42

45 Rate of climb in oblique flight ISA - T.A.S. = 80 kts on 1 engine, OEI unlimited Pressure altitude (ft) ISO-WEIGHT (kg) (m) Rate of climb (ft/mn) (m/s) E 43

46 Pressure altitude (ft) Rate of climb in oblique flight ISA T.A.S. = 80 kts on 1 engine, OEI unlimited ISO-WEIGHT (kg) (m) Rate of climb (ft/mn) (m/s) E 44

47 Hourly fuel consumption SL, ISA 700 Hourly fuel consumption (kg/h) ISO-Weight (kg) (lb/h) 650 Vmax Vreco T.A.S (kt) (km/h) E 45

48 Hourly fuel consumption SL, ISA Hourly fuel consumption (kg/h) ISO-Weight (kg) (lb/h) 650 Vmax Vreco T.A.S (kt) (km/h) E 46

49 8000 Technical Data Hourly fuel consumption Zp = 5000 ft, ISA Hourly fuel consumption (kg/h) 650 ISO-WEIGHT (kg) Vmax 600 Vreco T.A.S (kt) E 47

50 Hourly fuel consumption Zp = 5000 ft, ISA + 20 Hourly fuel consumption (kg/h) 650 ISO-WEIGHT (kg) Vmax 600 Vreco T.A.S (kt) E 48

51 (1) (2) (3) Technical Data PAYLOAD / RANGE CHART SL ISA Payload (kg) MTOW=11000 kg MTOW=11000 kg MTOW=11000kg 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 E 49

52 (1) (2) (3) Technical Data PAYLOAD / RANGE CHART SL ISA + 20 C Payload (kg) MTOW=11000kg kg MTOW=11000 kg 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 E 50

53 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 E 51

54 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 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 E 52

55 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 MAIN ROTOR AND TAIL ROTOR BLADES MAIN ROTOR HUB OC BENDIX ENGINE-MGB COUPLING SHAFT ASSY 4800 MGB MAIN MODULE MGB EPYCICLIC MODULE MGB ACCESSORY DRIVE GEAR BOX LH MGB ACCESSORY DRIVE GEAR BOX RH MGB SUPPORT FLEX PLATE 6200 TAIL GEAR BOX 3000** INTERMEDIATE GEAR BOX 3000** MAIN SERVO CONTROL 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 2A * : 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 E 53

56 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 E 54

57 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 E 55