EC225
Technical
Data
225 09.101.01 E
Eurocopter reserves the right to make configuration and data changes at any time without notice.
The facts and figures contained in this document and expressed in good faith do not constitute any offer or contract with Eurocopter
PageTD225.pdf 06/10/2008 17:45:34
EC225
Technical Data
SUPER PUMA
(Civil Version)
AS 332 L1 (MK1)
AS 332 C1 (MK1)
C
EC 225
M
J
CM
MJ
CJ
CMJ
N
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......................................................................................................... 3
2 - General characteristics ................................................................................. 5
3 - Baseline Aircraft Definition ......................................................................... 12
4 - Recommended Mission Configurations..................................................... 15
5 - Optional Equipment ..................................................................................... 23
6 - Main performance ........................................................................................ 32
7 - Customer Service Overview ...................................................................... 51
Manufacturers notice
Attention !
EUROCOPTER, its logo, EC225, COUGAR, SUPER PUMA, SPHERIFLEX,
M’ARMS are trade marks of the Eurocopter group.
Eurocopter’s policy is one of on-going product enhancement which means
that alterations in definition, pictures, weights, dimensions or performance
may be made at any time without notice being included in those documents
that have already been issued.
This document cannot thus be taken as an offer or serve as an appendix to a
contract without a prior check as to its validity and prior written agreement of
EUROCOPTER.
The operational or certification regulations, as defined by the local
authorities, can make compulsory the installation of some of the equipment
and recommended solutions, listed in this document. This list does not claim
to cover the whole of the worldwide operational requirements nor the
equipment not specifically related to the helicopter (for example: life jacket) or
necessary for particular missions (for example: supplemental oxygen). The
operator is responsible for ascertaining with his local authorities that the
planned configuration of the helicopter complies with regulatory requirements
for the area(s) of operations and the type(s) of mission(s) considered.
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
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:
IFR conditions :
1 pilot
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
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
kg
lb
5,376
11,852
5,624
11,000
4,500
11,200
12,398
24,251
9,921
24,690
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
2,553
318
5 x 475
600
US gal.
674
84
5 x 126
157
kg
2,017
251
5 x 375
474
lb
4,447
553
5 x 826
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
2.12 m
6.95 ft
3.00 m
9.84 ft
Dimensions with blades folded
4.10 m
13.45 ft
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
Fadec driven bleed valve
(better SFC & surge
margin)
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
Enhanced
Dual Channel FADEC
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
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
Intermediate contingency power (unlimited) 1
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
2
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
1
2
3
2
6
1
3
4
5
1
9
2
8 7
Piloting, Navigation and Mission Multifunction displays
NR/ILS button indicator
Master warning light
General alarm
Landing gear warning light
Stop watch
4
5
6
7
8
9
Warning panel
VMS displays
Triple tachometer
Automatic Flight Control Panel (AFCP)
ISI (Integrated Stand-by Instrument)
Provision
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
00-10029-A
00-50013-A
Commercial
reference
00-10029-00-CI
00-50013-00-CI
Name
EC225 Baseline Aircraft
"EC225 Offshore" package including:
General Equipment
05-03006-A
05-03006-00-CI
First aid kit - JAR OPS 3 compatible
05-26007-A
05-26007-00-CI
Dinol AV30 re-inforced anti-corrosive treatment
05-31052-A
05-31052-00-CI
Enlarged Cabin grey tinted windows
05-35002-A
05-35002-00-CI
Cabin floor for crashworthy seats
05-36025-A
05-36025-00-CI
Enlarged footstep cockpit
05-36026-A
05-36026-00-CI
Enlarged footstep cabin
05-39002-A
05-39002-00-CI
Illuminated Map Holder - JAR OPS 3 compatible
05-50003-A
05-50003-00-CI
Kit for flight in limited icing conditions
05-51001-A
05-51001-00-CI
De-iced cockpit center pane with wiper
05-52006-A
05-52006-00-CI
Goodrich Icing severity indicator
05-65000-A
05-65000-00-CI
Hydro electric group
05-81031-A
05-81031-00-CI
Energy Absorbing central auxiliary fuel tank 318 l (84 US gal)
05-82005-A
05-82005-00-CI
Pressure refuelling on the ground with Energy Absorbing self-sealing sponson
fuel tanks
Specific Mission Equipment
06-21015-A
06-26006-B
06-21015-00-FP
06-26006-01-FP
Goodrich 28V electrical hoist (290ft, 600lb) - Fixed parts
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
Document
reference
Commercial
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
00-10029-A
Commercial
reference
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-A
06-20003-00-FP Double hoist installation - Fixed Parts
06-20003-00-RP1 Double hoist installation - Removable Parts (Main Hoist & Beam)
06-20003-A
06-26006-B
06-27013-A
06-31018-B
06-31018-B
06-41004-A
06-42012-A
06-43001-A
06-43001-A
06-43005-A
06-45061-A
06-45061-A
06-45062-A
06-51030-A
06-51030-A
06-51140-A
06-51140-A
06-20003-00-RP2
06-26006-01-FP
06-27013-00-FP
06-31018-01-FP
06-31018-01-RP
06-41004-00-CI
06-42012-00-CI
06-43001-00-CI
06-43001-01-CI
06-43005-00-CI
06-45061-00-FP
06-45061-00-RP
06-45062-00-CI
06-51030-00-FP
06-51030-00-RP
06-51140-00-FP
06-51140-00-RP
Double hoist installation - Removable Parts (Backup Hoist)
External mirrors (including one electrical) - Fixed Parts
Cargo sling with dynamometer 3,8 Tons - Fixed Parts
Electrical hailer installation (Qty 1) - Fixed Parts
Electrical hailer installation (Qty 1) - Removable Parts
Soderberg anti collision light (belly mounted)
Fixed lights in the sponsons
Swivelable light under right sponson
Swivelable light under left sponson
Vertical light for hoisting and sling operation surveillance
Trakka Search light with infrared filter in-flight changeover - Fixed Parts
Trakka Search light with infrared filter in-flight changeover - Removable Parts
FLIR Mx15i HD / Trakka Slaving Unit
Flir Operator console - Fixed Parts
Flir Operator console - Removable Parts
Nose mounted FLIR WESCAM MX15i HD - Fixed Parts
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
Commercial
reference
Document
reference
Name
Specific Mission Equipment
06-60004-A
06-60004-00-CI
06-61011-A
06-61011-A
06-65008-A
06-65010-A
06-66004-A
06-67001-A
06-67023-A
06-70008-A
06-70013-A
06-70014-A
06-61011-00-FP
06-61011-00-RP
06-65008-00-CI
06-65010-00-CI
06-66004-00-CI
06-67001-00-CI
06-67023-00-CI
06-70008-00-CI
06-70013-00-CI
06-70014-00-CI
2 Life rafts - 18 to 27 pax - in the multipurpose sponsons with jettison control
in cockpit
Emergency floatation gear with automatic firing - Fixed Parts
Emergency floatation gear with automatic firing - Removable Parts
3rd hand held fire extinguisher - JAR OPS 3 compatible
2 Flashlights - JAR OPS 3 compatible
Helicopter Emergency Egress Lighting (HEEL).
2 Portable ELT 406 MHz HR SMITH Personal Locator Serie 500 in liferafts
HR Smith serie 503 - ADELT
NVG compatible cockpit lighting
NVG compatible cabin lighting
NVG compatible external lighting
Interior Layout
07-10009-A
07-15009-A
07-22005-A
07-22005-A
07-24008-A
07-24008-A
07-24010-A
07-24010-A
07-30007-A
07-60006-A
07-70012-A
07-72022-A
07-10009-00-FP
07-15009-00-CI
07-22005-00-FP
07-22005-00-RP
07-24008-00-FP
07-24008-00-RP
07-24010-00-FP
07-24010-00-RP
07-30007-00-CI
07-60006-00-CI
07-70012-00-CI
07-72022-00-CI
3rd man crew seat - Fixed parts
Pilot and copilot crashworthy seats
14 crashworthy wall mounted foldable seat installation - Fixed Parts
14 crashworthy wall mounted foldable seat installation - Removable Parts
Operator sliding crashworthy seat- Fixed parts
Operator sliding crashworthy seat- Removable Parts
Second operator sliding crashworthy seat - Fixed Parts
Second operator sliding crashworthy seat - Removable Parts
Comfort upholstery with improved sound-proofing
SAR Layout in the intermediate structure with bulkhead
Life Port medical mount package
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-A
08-12025-A
08-16026-A
08-16027-A
08-17049-A
08-10016-00-CI
08-12025-00-CI
08-16026-00-CI
08-16027-00-CI
08-17049-00-CI
Collins - HF9X00 HF/SSB
NAT - NPX138 VHF/FM-H
NAT DACS ICS - Complementary set : 4th control panel
NAT DACS ICS - Complementary set : 5th control panel
NAT - Passenger Adress
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.
225 09.101.01 E
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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
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.
225 09.101.01 E
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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
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
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
First aid kit - JAR OPS 3 compatible
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.
225 09.101.01 E
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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
kg
lb
General equipment (continued)
05-64000-A
05-64000-00-CI
Auxiliary Power Unit
117.1
258.1
05-65000-A
05-65000-00-CI
Hydro electric group
19.0
41.8
05-67003-A
05-67003-00-CI
220 V / 50 Hz AC power socket in cabin
0.8
1.7
05-81004-A
05-81004-00-FP Additional Energy Absorbing pod fuel tanks - Fixed Parts
98.3
26.8
05-81004-A
05-81004-00-RP Additional Energy Absorbing pod fuel tanks - Removable
Parts
98.3
216.7
05-81031-A
05-81031-00-CI
Energy absorbing central auxiliary fuel tank 318 l
(84 US gal)
27.5
60.6
05-82005-A
05-82005-00-CI
Pressure refuelling on the ground
24.3
53.7
05-82005-A
05-82005-01-CI
Pressure refuelling on the ground (air conditioning
compatible)
24.3
53.7
05-92014-A
05-92014-00-FP Main rotor blade folding system - Fixed Parts
3.2
7.0
05-92014-A
05-92014-00-RP Main rotor blade folding system - Removable Parts
81.3
178.5
05-93004-A
05-93004-00-CI
Naval mooring
3.7
8.2
05-93006-A
05-93006-00-CI
Lashing rings for main landing gear
0.9
1.9
15.0
33.1
112.3
247.5
35.0
77.1
Specific mission equipment
06-20003-A
1
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)
06-21015-A
06-21015-00-FP Goodrich 28V electrical hoist (290ft, 600lb) - Fixed Parts
15.0
33.0
06-21015-A
06-21015-00-RP Goodrich 28V electrical hoist (290ft, 600lb) - Removable
Parts
99.2
218.6
06-24007-A
06-24007-00-FP Fast roping installation on both sides - Fixed Parts
5.7
12.6
06-24007-A
06-24007-00-RP Fast roping installation on both sides - Removable Parts 1
71.5
157.6
06-25004-A
06-25004-00-CI
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
Drip tub
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.
225 09.101.01 E
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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
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 fire extinguisher - JAR OPS 3 compatible
2.2
4.9
06-65010-A
06-65010-00-CI 2 Flashlights - JAR OPS 3 compatible
1.2
2.6
06-66004-A
06-66004-00-CI Helicopter Emergency Egress Lighting (HEEL)
5.3
11.7
06-67023-A
06-67023-00-CI HR Smith serie 503 - ADELT
8.2
18.1
06-68008-A
06-68008-00-CI Dukane DK120 Underwater Acoustic Beacon
0.5
1.1
06-69002-A
06-69002-00-CI Automatic Voice Alarm Device (AVAD) 3
1.5
3.3
06-70008-A
06-70008-00-CI NVG compatible cockpit lighting
6.7
14.77
06-81018-A
06-81018-00-CI Fire fighting kit (up to 4000 liters)
475.0
1047.1
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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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
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 toilet
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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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
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)
Seating
or
19 crashworthy
seats
10 + 1 VIP crashworthy seats
with bar and toilet
or
12 VIP crashworthy seats with
bar and toilet
Upholstery
Standard upholstery
“De Luxe” upholstery
or
Comfort upholstery
Doors
Special LH door with
built-in steps
Standard sliding
doors
and
Special RH double
door
Rear
Luggage
compartment with
standard rear access
door
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.
225 09.101.01 E
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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
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.
225 09.101.01 E
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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
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.
225 09.101.01 E
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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
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
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)
kg
lb
9,000
19,842
9,500
20,944
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
m
3,888
3,370
2,874
2,396
1,935
ft
12,756
11,058
9,431
7,861
6,350
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 IGE (at Take-off power, 10 ft)
ISA
ISA+20
Hover Ceiling OGE (at Take-off power)
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
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
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)
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
75
00
ISA
ISA
70
00
0
+2
80
00
ISA
85
00
15000
5
+3
90
00
ISA
-20
10000
95
10
00
00
0
10
50
0
11
00
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
0
A+
IS
A
IS
700
15000
20
750
0
35
2
AIS
0
10000
900
A+
850
IS
800
0
0
0
95
00
10
00
0
10
50
0
11
00
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 from a clear area (EASA Category A)
Pressure altitude (ft)
ISO-Weight (kg)
20000
35
20
0
800
0
A
IS
850
+
+
650
0
750
A
IS
15000
A
IS
A
IS
700
0
0
0
-2
900
0
950
10000
0
100
00
105
0
0
110
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
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 data and operating limitations,reference must be made to the approved flight manual and 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
8000
8500
9000
6500
9500
0
0
1000
0
0
105
00
11
7000
10000
7500
15000
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
00
65
00
70
00
00
75
80
00
0
00
85
90
0
95
0
0
00
10
0
50
10
11
00
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
00
65
00
70
00
1000
75
500
00
0
80
00
85
00
90
00
95
0
00
10
0
50
10
0
00
11
0
0
2000
1500
Rate of climb (ft/mn)
0
10
(m/s)
1
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
0
0
65
0
1000
00
70
500
00
0
75
00
80
00
85
00
90
00
95
0
00
10
0
50
10 0
00
11
0
1500
2000
Rate of climb (ft/mn)
0
10
(m/s)
1
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
Vr
ec
o
600
550
500
450
1250
11
00
0
10
50
0
10
00
0
95
00
900
0
850
0
8000
1150
1050
7500
7000
950
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
Vre
c
o
600
550
500
450
1250
11
00
10 0
50
10 0
00
95 0
00
90
00
85
00
80
00
75
00
700
0
1150
1050
950
650
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
e
Vr
co
550
11
450
400
0
0
00 050
1
500
10
00
0
95
00
90
00
85
00
80
00
75
00
70
00
65
00
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
600
co
re
550
450
400
0
0
0
0
00
5 0 00
11
10
1
500
95
00
90
00
85
00
80
00
75
00
70
00
65
350
60
00
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
MTO
TOW
W=1
=110
1000
00kkgg
kg
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
MTO
TOW
W=1
=110
1000
00kkgg
kg
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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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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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
TYPE
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
TYPE
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. Additional courses
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
EC225
Technical
Data
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Eurocopter reserves the right to make configuration and data changes at any time without notice.
The facts and figures contained in this document and expressed in good faith do not constitute any offer or contract with Eurocopter