ec225-tech_data_2009

EC225  Technical Data

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EC225  Tech Te ch nic al Data Data

SUPER PUMA (Civil Version)

 AS 332 L1 (MK1)

 AS 332 C1 (MK1)

EC 225

COUGAR (Military Version)

Naval version missiles/torpedoes

Stretched version utility/armed

 AS 532 SC (MK1)

 AS 532 AL (MK1)

Utility/armed version

EC 725

EC225  Tech Te ch nic al Data Data

SUPER PUMA (Civil Version)

 AS 332 L1 (MK1)

 AS 332 C1 (MK1)

EC 225

COUGAR (Military Version)

Naval version missiles/torpedoes

Stretched version utility/armed

 AS 532 SC (MK1)

 AS 532 AL (MK1)

Utility/armed version

EC 725

Technical Data

Contents 1 - Foreword............................. Foreword ............................. .............................. .............................. ................ 3 2 - General characteristics characteristics ............................ .............................. ....................... 5 3 - Baseline Aircraft Definition ............................... .............................. ............ 12 4 - Recommended Recommended Mission Mission Configurations........................... 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 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 configuration of the helicopter helicopter complies with regulatory regulatory requirements requirements for the area(s) of operations and the type(s) of mission(s) considered.

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance performance data and operating operating limitations,reference limitations,reference must be made to the the approved flight flight manual and all all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER EUROCOPTER  - 2009

Technical Data

Blank

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data

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 .

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data

Blank

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data

2- General Characteristics Layout 





Minimum flight crew 

VFR conditions:

1 pilot



IFR conditions :

2 pilots

VIP transport (in addition to the crew) :

8 to 12 passengers

Passenger transport (in addition to the crew) up to :

19 crashworthy seats

Weights kg

lb

5,376

11,852

5,624 11,000 4,500 11,200

12,398 24,251 9,921 24,690

Note : Empty weight accuracy : within ±  2.0 % 

   

Empty weight, standard aircraft (including engine oil and unusable fuel) Useful load Maximum all-up weight Maximum cargo-sling load Maximum all-up weight in external load configuration

Power plant 2 Turbomeca Makila 2A1 turboshaft engines.

Engine ratings kW

Power per engine, in standard atmosphere, at sea level :

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 

Standard energy absorbing fuel tanks

 

Optional central energy absorbing fuel tank Optional ferry fuel tanks (1 to 5)



Pod fuel tanks

US gal.

kg

lb

2,553

674

2,017

4,447

318 5 x 475

84 5 x 126

251 5 x 375

553 5 x 826

600

157

474

1045

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data

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

4.97 m

15.09 ft

16.30 ft

5.25 m 17.22 ft

16.79 m 55.08 ft

3.96 m 13.00 ft 2.00 m 6.56 ft 2.12m 6.95 ft

3.00 m 9.84 ft

Dimensions with blades folded

4.10 m 13.45 f 

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data

Dimensions of compartments and accesses Cabin main dimensions

Cabin floor

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data

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

Power turbine with blade shedding system

Single crystal blades

Based on Makila 2A experience, a reliable engine, the Makila 2A1 incorporates two main improvements: Increased OEI performances   Consumption reduction



Fadec driven bleed valve (better SFC & surge margin)

Enhanced Dual Channel FADEC

Main Gear Box MGB torque limitations:

100% torque corresponds to 2610 kw at 265 rpm rotor speed

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









1 2 

kW

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)

Limitation controlled by the Fadec for NR>255 rpm. The INT contingency power is 1593 kw at 255 rpm. The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data   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

7

2

6

1

3

4

5

1

2

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)

Stop watch

9

Provision

3

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data



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.

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data

Blank

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data

3 – EC225  Baseline Aircraft Definition

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data

Blank

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data

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.

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data Mission configuration Document reference

Commercial reference

00-10029-A

00-10029-00-CI

EC225 Baseline Aircraft

00-50013-A

00-50013-00-CI

"EC225  Offshore" package including:

Name

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…

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data

Commercial reference

Document reference

Name

Interior Layout 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

08-00016-02-CI

Civil Use minimum equipment (IFR dual pilot) including:

Avionics 08-00016-A

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

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data 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 The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data Mission configuration Document reference

Commercial reference

00-10029-A

00-10029-00-CI

Name 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…

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data Document reference

Commercial reference

Name

Specific Mission Equipment 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

08-00016-02-CI

Civil Use minimum equipment (IFR dual pilot)

Avionics 08-00016-A

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

08-10016-00-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

08-10016-A

Configuration continued on next page…

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data Document reference

Commercial reference

Name

Avionics 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

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data

Blank

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data

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)

72.7

160.2

05-25014-A

05-25014-00-CI

Main rotor blades re-inforced sand erosion protection strip (loose equipment delivered separately)

0.4

0.8

05-25015-A

05-25015-00-CI

Tail rotor blades re-inforced sand erosion protection strip (loose equipment delivered separately)

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)

41.1

90.6

05-42021-A

05-42021-00-RP2  Air conditioning system - Removable Parts 2 (cockpit power unit)

40.7

89.7

164.8

363.3

05-50001-A

05-50001-00-CI

Installation for flight in icing conditions

05-50002-A

05-50002-00-CI

Installation for flight in extreme cold weather

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

On request

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data Document reference

Name

Commercial reference

kg

lb

117.1

258.1

19.0

41.8

0.8

1.7

General equipment (continued) 05-64000-A

05-64000-00-CI  Auxiliary Power Unit

05-65000-A

05-65000-00-CI

Hydro electric group

05-67003-A

05-67003-00-CI

220 V / 50 Hz AC power socket in cabin

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

Double hoist installation - Fixed Parts

15.0

33.1

06-20003-A

06-20003-00-RP1 Double hoist installation - Removable Parts (Main Hoist & Beam)

112.3

247.5

06-20003-A

06-20003-00-RP2 Double hoist installation - Removable Parts (Backup Hoist)

35.0

77.1

Specific mission equipment 06-20003-A

1

06-20003-00-FP

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

5.7

12.6

06-24007-A

06-24007-00-RP Fast roping installation on bot h 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

Fast roping installation on both sides - Fixed Parts

Removable Parts of this installation are not certified. The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data Document reference

Name

Commercial reference

kg

lb

Specific mission equipment (continued)

1 2  3

06-27020-A

06-27020-00-FP Cargo sling with dynamometer 4,5 Tons - Fixed Parts

4.4

9.7

06-27020-A

06-27020-00-RP Cargo sling with dynamometer 4,5 Tons - Removable Parts 1

28.2

62.2

06-41003-A

06-41003-00-CI Hella anti collision strobe light system (instead of standard one)

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

06-60004-00-CI 2 Life rafts - 18 to 27 pax - in the multipurpose sponsons with jettison control in cockpit 2 

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

06-64002-A

125.0

275.6

23.1

50.9

151.3

333.5

06-64002-00-CI Sea anchor

2.9

6.4

06-65008-A

06-65008-00-CI 3rd hand held f ire 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

Requires to remove the central auxiliary fuel tank if it has been selected by the user. Required for JAR OPS 3. Incompatible with EGPWS optional. The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data Document reference

Name

Commercial reference

kg

lb

Interior Layout

1 2 

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

07-50017-A

07-50017-00-CI Special LH door with built-in steps

07-60009-A

7.0

15.4

15.0

33.1

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

07-70003-00-CI  Air Ambulance Technology EMS quick conversion kit (2 units of 3 stretchers each)

On request

07-71013-A

07-71013-02-CI Casualty carrying installation for 11 stretchers (without stretchers and seats) 1

22.6

49.82

07-74007-A

07-74007-00-CI Stretcher (NATO type) (loose equipment delivered separately) 2 

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 toil et

On Request

07-80020-A

07-80020-00-CI 8 + 1 crashworthy seats VIP installation with bar and toilet (1 lounge)

On Request

07-80021-A

07-80021-00-CI 8 + 1 crashworthy seats VIP installation with bar and toilet (2 lounges)

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

Removable Parts of this installation are not certified. Equipment is not certified. The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data

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   g   n    i    t   a   e    S

19 crashworthy seats

10 + 1 VIP crashworthy seats with bar and toilet or 12 VIP crashworthy seats with bar and toilet

  y   r   e    t   s    l   o    h   p    U

Standard upholstery “De Luxe” upholstery

or Comfort upholstery

Special LH door with built-in steps   s   r   o   o    D

Standard sliding doors

and Special RH double door

Luggage compartment with standard rear access door

  r   a   e    R

Standard rear access door

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data 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

08-17009-00-CI Cabin entertainment System (CD+DVD) with 4 personal LCD

14.0

30.8

08-17033-A

08-17033-00-CI Cabin entertainment System (CD+DVD) with 8 personal LCD

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. The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data Document reference 08-20001-A

Commercial reference

Name

kg

08-20001-01-CI SAR Modes navigation package with centralized radio management system

lb

60,6

133.6

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

1

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

Incompatible with optional item Automatic Voice Alarm Device (AVAD). The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data

Document reference

Commercial reference

Name

kg

lb

Avionics (continued) 08-44040-A

08-44040-00-CI Canadian Marconi - CMA9000 - Flight Management System

8.3

18.2

08-44043-A

08-44043-00-CI Canadian Marconi - CMA9000 - Flight Management System, with SAR modes

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

08-83004-00-CI M'ARMS Health & Usage Monitoring System (HUMS) with  Allied Combi-lite CVFDR 1 2 3

34.9

76.9

08-83004-A

08-83004-01-CI M'ARMS Health & Usage Monitoring System (HUMS) with HOMP & Allied Combi-lite CVFDR 1 2 3

42.0

92.6

Operational Protection

1 2  3

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

Compatible with JAR OPS-3 regulation. The toolings of the installation are not included in the price.  At least one ground station per helicopter base must be purchased. The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data

Blank

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data

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 lb













Maximum speed, VNE

Maximum cruise speed (at MCP)

Recommended cruise speed

Fuel consumption at recommended cruise speed

Rate of climb (80kt, 2 engines at MCP)



10,000 22,046

10,500 23,149

11,000 24,251

km/h

324

324

324

324

324

kts

175

175

175

175

175

km/h

275

273

270

266

262

kts

149

148

146

144

142

km/h

261

262

263

265

262

kts

141

141

142

143

142

kg/h

608

620

632

649

655

lb/h

1,340

1,367

1,393

1,431

1,444

m/s

8.7

7.8

6.9

6.1

5.4

ft/mn

1,709

1,529

1,362

1,208

1,064

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

m

3,099

2,572

2,065

1,578

792

ft

10,166

8,438

6,776

5,176

2,600

m

2,389

1,812

1,261

731

93

ft

7,838

5,946

4,138

2,398

305

m

5,918

5,413

4,933

4,469

4,041

ft

19,417

17,760

16,185

14,661

13,257

Hover Ceiling OGE (at Take-off power) 





9,500 20,944

Hover Ceiling IGE (at Take-off power, 10 ft) 



9,000 19,842

ISA

ISA+20

Service ceiling (Vz=0.508m/s = 100ft/mn)

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data

Gross Weight 

kg lb

9,000 19,842

9,500 20,944

10,000 22,046

10,500 23,149

11,000 24,251

km

887

876

865

852

838

nm

479

473

467

460

452

km

1,000

988

976

961

946

nm

540

534

527

519

511

km

1,197

1,185

1,169

1,152

1,135

nm

646

640

631

622

613

Maximum range

(without reserve, at economical cruise speed)









standard tanks

standard + central tanks

standard + central tanks + pod

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

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data

Performance on 1 engine Gross Weight

kg lb

Rate of climb (80kt, 1 engines at OEI unlimited)

9,000 19,842

9,500 20,944

10,000 22,046

10,500 23,149

11,000 24,251

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 : DA : IGE : ISA : MCP : OEI : OGE : PA :

All Engines Operative Density Altitude In Ground Effect International Standard Atmosphere Maximum Continuous Power One Engine Inoperative Out of Ground Effect Pressure Altitude

SL : TAS VNE : Vz : Zp : Vp : Vmax : Vreco :

Sea Level True Air Speed Never Exceed Speed Rate-of-climb Barometric Altitude Airspeed Maximum cruise speed Economical cruise speed

Units nm : kts: ft/min : m/sec : °C:

nautical miles knots feet/minute meters per seconds degrees Celsius

hr:min : kg : lb : km : kg/hr :

hours:minutes kilograms pounds kilometres kilograms per hour

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data

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)

Page 36



Take-off weight in hover OGE, AEO 5 min (on 2 engines, at take-off power, no wind)

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)

Page 39



Fast cruise speed Zp = 0, ISA + 20°C (on 2 engines at maximum continuous power)

Page 40



Rate of climb in oblique flight (on 2 engines at maximum continuous power - ISA; T.A.S. = 80 kts)

Page 41



Rate of climb in oblique flight (on 2 engines at maximum continuous power – ISA + 20°C; T.A.S. = 80 kts)

Page 42



Rate of climb in oblique flight (on 1 engine OEI unlimited, ISA ; T.A.S = 80 kts)

Page 43



Rate of climb in oblique flight (on 1 engine OEI unlimited, ISA + 20°C ; T.A.S = 80 kts)

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

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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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)

20000 7  5   0 0 

7  0  I      0 0 

I      S     A    

S     A     +    2     0    

8 0  0 0 

8 5   0 0 

15000

I      S     A     +    3     5     

9 0  0 0 

I      S     A     -  2     0    

10000

9 5   0 0  1 0  0 0  0  1 0  5  0  0  1 1  0 0  0 

5000

0

-30

-20

-10

0

10

20

30

40

50

OAT (°C)

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data

Take-off weight in hover OGE, AEO 5 min on 2 engines, at take-off power

Pressure altitude (ft)

ISO-Weight (kg)

20000 7  0  I     S    0 0 

I     S     A    +    2     0    

A   

7  5  0 0 

15000

I     S     A    +    3     5    

8 0  0 0  8 5  0 0 

I     S     A    -  2     0    

10000

9 0  0 0 

9 5   0 0  1 0  0 0  0  1 0  5  0  0  1 1  0 0  0 

5000

0

-30

-2 - 20

-10

0

10

20

30

40

50

OAT (°C)

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance performance data and operating operating limitations,reference limitations,reference must be made to the the approved flight flight manual and all all appropriate documents.

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Technical Data

Take-off weight from a clear area (EASA Category A)

Pressure altitude (ft)

ISO-Weight (kg)

20000 I    S     A    +   2    0   

7 0  0 0 

6 5  0 0 

7 5  0 0 

15000

I    S     A    +   3    5   

I    S     A   

8 0  0 0  8 

5  I    S    0 0   A    -  2    9 0  0  0    0  9 5  0 0 

10000

1 0  0 0  0  1 0  5 0  0  1 1  0 0  0 

5000

0

-30

-20

-10

0

10

20

30

40

50

OAT (°C)

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance performance data and operating operating limitations,reference limitations,reference must be made to the the approved flight flight manual and all all appropriate documents.

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Technical Data

Fast cruise speed Zp = 0, ISA on 2 engines, at maximum continuous power

Weight (kg)

(lb)

11000

24000

10000

22000

9000

20000

18000

8000

16000 7000

140

150 T.A.S (kt) 265

275

285 (km/h)

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance performance data and operating operating limitations,reference limitations,reference must be made to the the approved flight flight manual and all all appropriate documents.

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Technical Data

Fast cruise speed Zp = 0, ISA + 20 on 2 engines, at maximum continuous power

Weight (kg)

(lb)

11000

24000

10000

22000

9000

20000

18000

8000

16000 7000

140

150 T.A.S (kt) 265

275

285 (km/h)

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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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)

20000

15000

10000 1      1      0     0     0    

1      0      5      0      0     

1       0      0      0      0     

9       5       0      0     

9       0       0       0      

8       5       0       0      

 8        0        0        0      

      0        0        5        7

      0       0       0       7

      0       0       5       6

5000

0

0

500

1000

1500

2000

2500

3000

Rate of climb (ft/mn)

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data

Rate of climb in oblique flight ISA + 20 - T.A.S. = 80 kts on 2 engines, at maximum continuous power

Pressure Altitude (ft)

ISO-Weight (kg)

20000

15000

10000 1    1    1    9    9     8    1    0    0    5     0     5     0    5     0    0    0     0    0    0    0    0    0     0    0    0    0   

8    0    0    0   

7     5     0    0   

7     0    0    0   

6    5    0    0   

5000

0

0

500

1000

1500

2000

2500

3000

Rate of climb (ft/mn)

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data

Rate of climb in oblique flight ISA - T.A.S. = 80 kts on 1 engine, OEI unlimited

Pressure altitude (ft)

(m) ISO-WEIGHT (kg)

20000

6000

5000 15000 4000

10000

3000

2000 5000 1000 1     1     1     9     8     8     1     0     0     9     0     5     0     0     5     0     5     0     0     0     0     0     0     0     0     0     0     0     0     0     0    

7     5     0     0    

7     0     0     0    

6     5     0     0    

0 0

500

1000

0 2000

1500

Rate of climb (ft/mn) 0

10 (m/s)

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data

Rate of climb in oblique flight ISA + 20 - T.A.S. = 80 kts on 1 engine, OEI unlimited

Pressure altitude (ft)

(m) ISO-WEIGHT (kg)

20000

6000

5000 15000 4000

10000

3000

2000 5000 1000

1     1     1     7     1     0     0     9     9     8     8     7     5     0     5     0     5     0     5     0     0     0     0     0     0     0     0     0     0     0     0     0     0     0     0     0     0     0     0    

0

0

500

1000

6    5     0    0   

0

1500

2000

Rate of climb (ft/mn) 0

10 (m/s)

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data

Hourly fuel consumption SL, ISA

Hourly fuel consumption (kg/h)

ISO-Weight (kg) (lb/h)

700

1450

Vmax

650

1350 600   o   c   e    r     V

550

500

1250

1 1  0  0   0  

1 0   5  0   0   1 0  0 0  0  9 5   0 0 

1150

9 0  0 0 

1050

8 5 0  0 

450

8 0 0  0 

7 50   0    

950

7 00   0     6500

400 60

80

100

120

140

160

T.A.S (kt) 150

200

250 (km/h)

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data

Hourly fuel consumption SL, ISA + 20

Hourly fuel consumption (kg/h)

ISO-Weight (kg) (lb/h)

700 Vmax

1450

650

1350 600

550

  o   c    r  e     V

1250

1   1   0   0   0   1   0   5    0   0  

1   0   0   0   0  

500

450

1150

9  5   0  0   9  0   0  0   8  5   0  0   8  0   0  0   7  5   0 0  7 0  0 0 

1050

950

6 5  0 0 

400 60

80

100

120

140

160

T.A.S (kt) 150

200

250 (km/h)

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data

Hourly fuel consumption Zp = 5000 ft, ISA

Hourly fuel consumption (kg/h)

ISO-WEIGHT (kg)

650 Vmax

600 V     r    e   c    o  

550

500

450

1    1    0    0    0    1    0    5     0    0    1    0    0    0    0    9    5    0    0    9    0   0   0  

8   5    0   0  

400

8  0   0  0   7  5   0  0   7  0  0 0  6  5   0 0 

350 60

80

100

120

140

160

T.A.S (kt)

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data

Hourly fuel consumption Zp = 5000 ft, ISA + 20

Hourly fuel consumption (kg/h)

ISO-WEIGHT (kg)

650 Vmax

V     r    e   c   o  

600

550

500

1    1    0    0    0    1    0    5     0    0    1    0    0    0    0    9    5    0    0   

450

9    0    0    0    8   5    0   0  

8   0   0   0  

7  5   0  0  

400

7  0   0  0   6  5   0  0  

350 60

80

100

120

140

160

T.A.S (kt)

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data

PAYLOAD / RANGE CHART SL ISA

Payload (kg)

5000

M   T   M   O W   T   O W   = 1  = 1 1 0  1 0 0 0  0 0 k k  g  g  k g 

4000

   (         1            )        

  (       2         )      

3000

  (       3         )      

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 The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data

PAYLOAD / RANGE CHART SL ISA + 20°C

Payload (kg)

5000

M   T   M   O W   T   O W   = 1  = 1 1 0  1 0 0 0  0 0 k k  g  g  k g 

4000   (       1         )      

  (       2         )      

3000

  (       3         )      

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 The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data

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.

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data 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

Estimated Man Hour 

Daily checks :

Pilot’s task

Flight Related Checks 15 flight hrs or 7 days

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 

1200 MMH 16 years periodicity tasks

Scheduled Engine Inspection Estimated Man Hour  MAKILA 2A1 15 flight hrs periodicity tasks 0,1168 MMH per FH

75 flight hrs periodicity tasks 750 flight hrs periodicity tasks MMH: Mean Man Hour

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.

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data Main components Time Between Overhaul (TBO) / Service Life Limit (SLL) 1 TBO (h) as per MSM 2008 Ed.

Main Components  ALTERNATOR 40 KVA

3000

 AUXILARY HYDRAULIC PUMP

3000

TBO (h) Target Value *

SLL (h) as per MSM 2008 Ed.

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

TBO (h) as per MSM rev RT003b

TBO (h) Target Value *

2500

3000

“*”: Target value within the Maturity Plan under progress . ** = in MSM first half 2009

Engines MAKILA 2A1

SLL (h) as per MSM rev RT003b

“*”: Target value within the Maturity Plan under progress .

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. The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data 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

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data 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.

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data Engine Maintenance program  Always looking to maximize your efficiency and reduce your costs, Turbomeca, the engine manufacturer has developed an improved service offering. Turbomeca range of services covers: Classic Repair and Overhaul Standard Exchange AOG services Support By the Hour (SBH) services • • • •

Within the Support By the Hour ® coverage Turbomeca developed specific maintenance packages, as summarized hereafter. Standard Coverage: “Classic” SBH® The “classic” Support by the Hour (SBH®) is a global support service offered to operators to enable them to maintain the best availability of their engines fleet through a contract arrangement paid by running hours. The Support by the Hour (SBH®) is operated mainly through Standard Exchange supported by Turbomeca dedicated Corporate Pool. Customized Coverage: SBH® “Mission” The new service, Support By the Hour® Mission, offers a modular series of comprehensive service and engine management packages whereby Turbomeca undertakes to guarantee its operator's engine availability and care. From basic engine support requirement to fully comprehensive range of additional services, three different types of packages are offered to operators : Pro, Prime and Privilege.

Turbomeca Internet Web Site - TOOLS Turbomeca Operator On-Line Support (TOOLS site) is entirely dedicated to helping customers. With 24/7 availability, operators can access important information when they want to from where they want to, winning precious time and staying head. TOOLS at www.turbomeca-support.com.

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data Training With more than 50 years of experience, the EUROCOPTER   training centers provide the most comprehensive, coherent and highest standard helicopter training in the world for pilots and technicians, whether civilian or military. Qualification training, allowing operators to comply with regulatory requirements, and services training, more mission oriented and tailored to the customers’ operational needs, are addressed.  All training courses are established according to the relevant civil aviation authorities’ requirements. The centers are approved by the relevant airworthiness authorities (EASA, FAA, DGAC, LBA, CAA…). We are certified ISO 9001: V2000 and regularly audited by independent organisms such as Véritas, AFAQ… EUROCOPTER   training centers provide a wide range of courses and services, from basic training up to preparation for the most sophisticated civil and military missions.  As part of the full range of services on offer, EUROCOPTER   also plays an active role in helicopter pilot development through its Ab Initio programs. Centers are equipped with multimedia classrooms. This includes computers overhead projectors and stateof-the-art means such as Computer Aided Instruction (CAI), Computer Based Training (CBT). Some centers also have self-learning laboratories. EUROCOPTER  has set up a network of 14 training centers. For detailed information refer to EUROCOPTER  specific publication.

EC225 LP - Example of basic training course COURSE T YPE

COURSE REFERENCE

THEORETICAL FLIGHT INSTRUCTION INSTRUCTION 10 days 10 hours 6 hours THEORETICAL & PRACTICAL INSTRUCTION

Type Rating Instructor Pilot Conversion (1) COURSE REFERENCE

Pilots COURSE T YPE Mechanics

Type Rating (Airframe + engine)

5 weeks

Avionics

Type Rating

4 weeks

Blades

Maintenance and repair

Up to 2 weeks

(1) Pilot already qualified on EC225 LP (15 hours mini, within last 12 months, not included in type rating) TR1: For pilot non already qualified on single engine turbine TR2: For pilot already qualified on single engine turbine. Note: Length is given as information and depends on pilot or technician qualification or experience. Additionalcourses may be required.

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009

Technical Data Technical publications EUROCOPTER   provides all the technical publications necessary for safely operating and maintaining its aircraft cost effectively. EUROCOPTER   technical publications are available on an interactive electronic medium as a standard or in hard copies as an option. The INDOC DVD-ROM includes the Maintenance Program (PRE), the. Aircraft Maintenance Manual (AMM), System Description Section (SDS), Master Servicing Manual (MSM), Illustrated Parts Catalogue (IPC) and the Wiring Diagram Manual (WDM). The component maintenance manual (CMM) is available on DVD-ROM or hard copy, depending on the Vendor.  Along with the INDOC DVD-ROM, EUROCOPTER   provides a hard copy of the Airworthiness Technical Publication (Flight Manual, Pilots Check List, Master Servicing Manual …) as well as the Service Bulletin Catalogue. The DVD-ROM is available in English or French; it includes the latest information and is updated every 6 – 9 months.

T.I.P.I. (Technical Information Publication on Internet) Description T.I.P.I. website is entirely dedicated to provide a real-time issuing service for the following publications: Telex Alert, Télex Information, Service Bulletin, Service Letter, Service Information, Technical  Information Letter List of Applicable Publications (LOAP)  List of Master Minimum Equipment List (MMEL) 

Main features Each time a publication is issued, the customer is automatically informed by an e-mail. The download of the publication in pdf format is possible either directly from the e-mail or after  logging on the T.I.P.I. website. A keywords search tool is provided (aircraft family, type of publication, date of edition...).   Address: www.eurocopter.com/services/technical publications/T.I.P.I. The publications are available in English, French or German depending on the case. A small summary, already included in the e-mail, helps the customer to understand quickly the  subject. Small icons allow the customer to identify immediately the type of information received.  

The data set forth in this document are general in nature and for information purposes only. They may vary with conditions.  For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2009