-
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
TechnicalData
225 09.101.01 E
EC225
-
SUPER PUMA(Civil Version)
COUGAR(Military Version)
Naval versionmissiles/torpedoesAS 532 SC (MK1)
Stretched versionutility/armed
AS 532 AL (MK1)
Utility/armed versionEC 725
AS 332 C1 (MK1)
Technical Data
AS 332 L1 (MK1)
EC 225
EC225
C
M
J
CM
MJ
CJ
CMJ
N
PageTD225.pdf 06/10/2008 17:45:34
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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.
225 09.101.01 E 1 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
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,
MARMS are trade marks of the Eurocopter group. Eurocopters 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.
-
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.
225 09.101.01 E 2 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
Blank
-
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.
225 09.101.01 E 3 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
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.
-
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.
225 09.101.01 E 4 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
Blank
-
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.
225 09.101.01 E 5 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
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 Note : Empty weight accuracy : within 2.0 % kg lb
Empty weight, standard aircraft (including engine oil and
unusable fuel) 5,376 11,852
Useful load 5,624 12,398 Maximum all-up weight 11,000 24,251
Maximum cargo-sling load 4,500 9,921 Maximum all-up weight in
external load configuration 11,200 24,690
Power plant 2 Turbomeca Makila 2A1 turboshaft engines.
Engine ratings Power per engine, in standard atmosphere, at sea
level : kW shp
Maximum emergency power (OEI 30") 1,776 2,382 Intermediate
emergency power (OEI 2') 1,667 2,236 OEI continuous power 1,608
2,156 Take-off power 1,567 2,101 Maximum continuous power 1,418
1,902
Usable Fuel capacities litres US gal. kg lb
Standard energy absorbing fuel tanks 2,553 674 2,017 4,447
Optional central energy absorbing fuel tank 318 84 251 553 Optional
ferry fuel tanks (1 to 5) 5 x 475 5 x 126 5 x 375 5 x 826 Pod fuel
tanks 600 157 474 1045
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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.
225 09.101.01 E 6 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
Main dimensions
2.12 m6.95 ft
3.96 m13.00 ft
4.60 m15.09 ft
4.97 m16.30 ft
16.20 m53.14 ft dia
3.15 m10.33 ft dia
19.50 m Rotor Rotating63.98 ft
2.00 m6.56 ft
3.00 m9.84 ft
5.25 m17.22 ft 16.79 m
55.08 ft
Dimensions with blades folded
4.10 m13.45 ft
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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.
225 09.101.01 E 7 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
Dimensions of compartments and accesses Cabin main
dimensions
Cabin floor
-
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.
225 09.101.01 E 8 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
Main technical improvements to increased safety:
Engines: Makila 2A1
Dual channel FADEC Modular Design Pilot workload reduction
Ultimate Protection (Overspeed
protection & Blade Shedding technologies)
Based on Makila 2A experience, a reliable engine, the Makila 2A1
incorporates two main improvements:
Increased OEI performances Consumption reduction
Main Gear Box
MGB torque limitations:
100% torque corresponds to 2610 kw at 265 rpm rotor speed kW shp
Super contingency power (OEI 30") 1 2,047 2,745 Maximum contingency
power (OEI 2') 1 1,877 2,517
Intermediate contingency power (unlimited) 1 1,655 2 2,219
Maximum continuous power (unlimited) 2,159 2,895
Take-off power (5') 2,610 3,500
Transient power (20") 2,871 3,850
Increased power 30 minutes flight capability after total loss of
oil,
with back-up lubrication Spray system, compliant with JAR 29
Upgraded upper part (casing and rotor bearing)
and lower part (casing, gears)
1 Limitation controlled by the Fadec for NR>255 rpm. 2 The
INT contingency power is 1593 kw at 255 rpm.
Enhancedcompressors
Single crystal blades
Fadec driven bleed valve (better SFC & surge
margin)
Enhanced Dual Channel FADEC
Power turbine with blade shedding system
-
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.
225 09.101.01 E 9 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
Blades
5 blades SPHERIFLEX main rotor, with upgraded servo
actuators
New blade profile, multibox structure, capable of flight in
icing condition
Avionics
Advanced Helicopter Cockpit Avionics System (AHCAS),
implementing: four 6 x 8 LCD Multi Function Displays (MFD) two 4 x
5 Vehicle Management System color displays (VMS) one Integrated
Stand-by Instrument LCD (ISI) new Automatic Flight Control System
(AFCS), Air Data Computer (ADC) and Attitude and
Heading Reference System (AHRS)
1 2 6 1 3 4 5 1 2
7 9 8 7
1 Piloting, Navigation and Mission Multifunction displays 4
Warning panel 2 NR/ILS button indicator 5 VMS displays Master
warning light 6 Triple tachometer General alarm 7 Automatic Flight
Control Panel (AFCP) Landing gear warning light 8 ISI (Integrated
Stand-by Instrument)
3 Stop watch 9 Provision
-
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.
225 09.101.01 E 10 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
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.
-
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.
225 09.101.01 E 11 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
Blank
-
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.
225 09.100.02 E 12 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
3 EC225 Baseline Aircraft Definition
-
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.
225 09.100.02 E 13 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.
225 09.101.01 E 14 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
Blank
-
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.
225 09.101.01 E 15 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
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.
-
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.
225 09.101.01 E 16 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
Mission configuration
Document reference
Commercial reference
Name
00-10029-A 00-10029-00-CI EC225 Baseline Aircraft 00-50013-A
00-50013-00-CI "EC225 Offshore" package including:
General Equipment 05-03006-A 05-03006-00-CI First aid kit - JAR
OPS 3 compatible 05-26007-A 05-26007-00-CI Dinol AV30 re-inforced
anti-corrosive treatment 05-31052-A 05-31052-00-CI Enlarged Cabin
grey tinted windows 05-35002-A 05-35002-00-CI Cabin floor for
crashworthy seats 05-36025-A 05-36025-00-CI Enlarged footstep
cockpit 05-36026-A 05-36026-00-CI Enlarged footstep cabin
05-39002-A 05-39002-00-CI Illuminated Map Holder - JAR OPS 3
compatible 05-50003-A 05-50003-00-CI Kit for flight in limited
icing conditions 05-51001-A 05-51001-00-CI De-iced cockpit center
pane with wiper 05-52006-A 05-52006-00-CI Goodrich Icing severity
indicator 05-65000-A 05-65000-00-CI Hydro electric group 05-81031-A
05-81031-00-CI Energy Absorbing central auxiliary fuel tank 318 l
(84 US gal) 05-82005-A 05-82005-00-CI Pressure refuelling on the
ground with Energy Absorbing self-sealing sponson
fuel tanks
Specific Mission Equipment 06-21015-A 06-21015-00-FP Goodrich
28V electrical hoist (290ft, 600lb) - Fixed parts 06-26006-B
06-26006-01-FP External mirrors (including one electrical) - Fixed
Parts 06-27013-A 06-27013-00-FP Cargo sling with dynamometer 3,8
Tons - Fixed parts 06-41003-A 06-41003-00-CI Hella anti collision
strobe light system (instead of standard one) 06-41004-A
06-41004-00-CI Soderberg anti collision light (belly mounted)
06-42012-A 06-42012-00-CI Fixed lights in the sponsons 06-60004-A
06-60004-00-CI 2 Life rafts - 18 to 27 pax - in the multipurpose
sponsons with jettison control
in cockpit 06-61011-A 06-61011-00-FP Emergency floatation gear
with automatic firing - Fixed parts 06-61011-A 06-61011-00-RP
Emergency floatation gear with automatic firing - Removable parts
06-65008-A 06-65008-00-CI 3rd hand held fire extinguisher - JAR OPS
3 compatible 06-65010-A 06-65010-00-CI 2 Flashlights - JAR OPS 3
compatible 06-66004-A 06-66004-00-CI Helicopter Emergency Egress
Lighting (HEEL) 06-67023-A 06-67023-00-CI HR Smith series 503 ADELT
Configuration continued on next page
-
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.
225 09.101.01 E 17 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
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 Avionics 08-00016-A 08-00016-02-CI Civil Use
minimum equipment (IFR dual pilot) including:
Collins - Proline21 - VHF/AM #1 Collins - Proline21 - VHF/AM
#2
NAT DACS ICS - Basic set : 3 control panels in cockpit Collins -
TDR94D - 008 Collins - Proline21 - DME Collins - Proline21
VOR/ILS/MKR #2 Collins - Proline21 VOR/ILS/MKR/ADF #1 Serpe - IESM
Kannad 406 AP - Emergency Locator Transmitter
08-10016-A 08-10016-00-CB Collins - HF 9X00 - HF/SSB -
Capabilities
08-12025-A 08-12025-00-CI NAT - NPX138 VHF/FM-H
08-16026-A 08-16026-00-CI NAT DACS ICS - Complementary set : 4th
control panel
08-17049-A 08-17049-00-CI NAT- Passenger Address
08-27008-A 08-27008-00-CI Chelton System 7 - (121,5) VHF/FM
Marine dual frequency homer
08-31039-A 08-31039-00-CI Telephonics 1600 Weather Radar,
displayed on AHCAS
08-35009-A 08-35009-01-CI TCAS - GOODRICH - HP 899 integrated to
AHCAS
08-35015-A 08-35015-00-CI EGPWS - HONEYWELL - MKXXII integrated
to AHCAS
08-41012-A 08-41012-00-CI Canadian Marconi - CMA3024 - GPS
receiver
08-44040-A 08-44040-00-CI Canadian Marconi - CMA9000 - Flight
Management System
08-83004-A 08-83004-01-CI M'ARMS Health & Usage Monitoring
System (HUMS) with HOMP & Allied Combi-lite CVFDR
-
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.
225 09.101.01 E 18 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
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
-
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.
225 09.101.01 E 19 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
Mission configuration
Document reference
Commercial reference
Name
00-10029-A 00-10029-00-CI EC225 Baseline Aircraft
General Equipment 05-03006-A 05-03006-00-CI First aid kit - JAR
OPS 3 compatible 05-26007-A 05-26007-00-CI Dinol AV30 re-inforced
anti-corrosive treatment 05-31039-A 05-31039-00-CI 2 observation
bubble windows on cabin plug-in doors 05-31052-A 05-31052-00-CI
Enlarged cabin grey tinted windows 05-35005-A 05-35005-00-CI
Multipurpose Integrated Crashworthy Floor 05-39002-A 05-39002-00-CI
Illuminated Map Holder - JAR OPS 3 compatible 05-50003-A
05-50003-00-CI Kit for flight in limited icing conditions
05-51001-A 05-51001-00-CI De-iced cockpit center pane with wiper
05-52006-A 05-52006-00-CI Goodrich Icing severity indicator
05-65000-A 05-65000-00-CI Hydro electric group 05-81031-A
05-81031-00-CI Energy Absorbing central auxiliary fuel tank 318 l
(84 US gal) 05-82005-A 05-82005-00-CI Pressure refuelling on the
ground with Energy Absorbing self-sealing sponson
fuel tanks
Specific Mission Equipment
06-20003-A 06-20003-00-FP Double hoist installation - Fixed
Parts 06-20003-A 06-20003-00-RP1 Double hoist installation -
Removable Parts (Main Hoist & Beam) 06-20003-A 06-20003-00-RP2
Double hoist installation - Removable Parts (Backup Hoist)
06-26006-B 06-26006-01-FP External mirrors (including one
electrical) - Fixed Parts 06-27013-A 06-27013-00-FP Cargo sling
with dynamometer 3,8 Tons - Fixed Parts 06-31018-B 06-31018-01-FP
Electrical hailer installation (Qty 1) - Fixed Parts 06-31018-B
06-31018-01-RP Electrical hailer installation (Qty 1) - Removable
Parts 06-41004-A 06-41004-00-CI Soderberg anti collision light
(belly mounted) 06-42012-A 06-42012-00-CI Fixed lights in the
sponsons 06-43001-A 06-43001-00-CI Swivelable light under right
sponson 06-43001-A 06-43001-01-CI Swivelable light under left
sponson 06-43005-A 06-43005-00-CI Vertical light for hoisting and
sling operation surveillance 06-45061-A 06-45061-00-FP Trakka
Search light with infrared filter in-flight changeover - Fixed
Parts 06-45061-A 06-45061-00-RP Trakka Search light with infrared
filter in-flight changeover - Removable Parts 06-45062-A
06-45062-00-CI FLIR Mx15i HD / Trakka Slaving Unit 06-51030-A
06-51030-00-FP Flir Operator console - Fixed Parts 06-51030-A
06-51030-00-RP Flir Operator console - Removable Parts 06-51140-A
06-51140-00-FP Nose mounted FLIR WESCAM MX15i HD - Fixed Parts
06-51140-A 06-51140-00-RP Nose mounted FLIR WESCAM MX15i HD -
Removable Parts Configuration continued on next page
-
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.
225 09.101.01 E 20 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
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 Avionics 08-00016-A
08-00016-02-CI Civil Use minimum equipment (IFR dual pilot)
including: Collins - Proline21 - VHF/AM #1
Collins - Proline21 - VHF/AM #2
NAT DACS ICS - Basic set : 3 control panels in cockpit Collins -
TDR94D - 008 Collins - Proline21 - DME Collins - Proline21
VOR/ILS/MKR #2 Collins - Proline21 VOR/ILS/MKR/ADF #1 Serpe - IESM
Kannad 406 AP - Emergency Locator Transmitter
08-10016-A 08-10016-00-CI Collins - HF9X00 HF/SSB 08-12025-A
08-12025-00-CI NAT - NPX138 VHF/FM-H 08-16026-A 08-16026-00-CI NAT
DACS ICS - Complementary set : 4th control panel 08-16027-A
08-16027-00-CI NAT DACS ICS - Complementary set : 5th control panel
08-17049-A 08-17049-00-CI NAT - Passenger Adress Configuration
continued on next page
-
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.
225 09.101.01 E 21 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
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
-
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.
225 09.101.01 E 22 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
Blank
-
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.
225 09.101.01 E 23 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
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
05-50001-A 05-50001-00-CI Installation for flight in icing
conditions 164.8 363.3
05-50002-A 05-50002-00-CI Installation for flight in extreme
cold weather On request
05-50003-A 05-50003-00-CI Kit for flight in limited icing
conditions (submitted approval by local Airworthiness
Authority)
2.0 4.4
05-51001-A 05-51001-00-CI De-iced cockpit center pane with wiper
5.2 11.4
05-52006-A 05-52006-00-CI Goodrich Icing severity indicator 3.0
6.6
-
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.
225 09.101.01 E 24 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
Document reference
Commercial reference
Name kg lb
General equipment (continued)
05-64000-A 05-64000-00-CI Auxiliary Power Unit 117.1 258.1
05-65000-A 05-65000-00-CI Hydro electric group 19.0 41.8
05-67003-A 05-67003-00-CI 220 V / 50 Hz AC power socket in cabin
0.8 1.7
05-81004-A 05-81004-00-FP Additional Energy Absorbing pod fuel
tanks - Fixed Parts 98.3 26.8
05-81004-A 05-81004-00-RP Additional Energy Absorbing pod fuel
tanks - Removable Parts
98.3 216.7
05-81031-A 05-81031-00-CI Energy absorbing central auxiliary
fuel tank 318 l (84 US gal)
27.5 60.6
05-82005-A 05-82005-00-CI Pressure refuelling on the ground 24.3
53.7
05-82005-A 05-82005-01-CI Pressure refuelling on the ground (air
conditioning compatible)
24.3 53.7
05-92014-A 05-92014-00-FP Main rotor blade folding system -
Fixed Parts 3.2 7.0
05-92014-A 05-92014-00-RP Main rotor blade folding system -
Removable Parts 81.3 178.5
05-93004-A 05-93004-00-CI Naval mooring 3.7 8.2
05-93006-A 05-93006-00-CI Lashing rings for main landing gear
0.9 1.9
Specific mission equipment
06-20003-A 06-20003-00-FP Double hoist installation - Fixed
Parts 15.0 33.1
06-20003-A 06-20003-00-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
06-21015-A 06-21015-00-FP Goodrich 28V electrical hoist (290ft,
600lb) - Fixed Parts 15.0 33.0
06-21015-A 06-21015-00-RP Goodrich 28V electrical hoist (290ft,
600lb) - Removable Parts
99.2 218.6
06-24007-A 06-24007-00-FP Fast roping installation on both sides
- Fixed Parts 5.7 12.6
06-24007-A 06-24007-00-RP Fast roping installation on both sides
- Removable Parts 1 71.5 157.6
06-25004-A 06-25004-00-CI Drip tub 7.0 15.4
06-26006-B 06-26006-01-FP External mirrors (including 1
electrical) - Fixed parts 0,3 0.6
06-26006-B 06-26006-01-RP External mirrors (including 1
electrical) - Removable Parts 5,6 12.3
06-27013-A 06-27013-00-FP Cargo sling with dynamometer 3,8 Tons
- Fixed Parts 8.5 18.7
06-27013-A 06-27013-00-RP Cargo sling with dynamometer 3,8 Tons
- Removable Parts
27.7 61.1
1 Removable Parts of this installation are not certified.
-
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.
225 09.101.01 E 25 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
Document reference
Commercial reference
Name kg lb
Specific mission equipment (continued)
06-27020-A 06-27020-00-FP Cargo sling with dynamometer 4,5 Tons
- Fixed Parts 4.4 9.7
06-27020-A 06-27020-00-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
125.0 275.6
06-61011-A 06-61011-00-FP Emergency floatation gear with
automatic firing - Fixed Parts
23.1 50.9
06-61011-A 06-61011-00-RP Emergency floatation gear with
automatic firing - Removable Parts
151.3 333.5
06-64002-A 06-64002-00-CI Sea anchor 2.9 6.4
06-65008-A 06-65008-00-CI 3rd hand held fire extinguisher - JAR
OPS 3 compatible 2.2 4.9
06-65010-A 06-65010-00-CI 2 Flashlights - JAR OPS 3 compatible
1.2 2.6
06-66004-A 06-66004-00-CI Helicopter Emergency Egress Lighting
(HEEL) 5.3 11.7
06-67023-A 06-67023-00-CI HR Smith serie 503 - ADELT 8.2
18.1
06-68008-A 06-68008-00-CI Dukane DK120 Underwater Acoustic
Beacon 0.5 1.1
06-69002-A 06-69002-00-CI Automatic Voice Alarm Device (AVAD) 3
1.5 3.3
06-70008-A 06-70008-00-CI NVG compatible cockpit lighting 6.7
14.77
06-81018-A 06-81018-00-CI Fire fighting kit (up to 4000 liters)
475.0 1047.1
1 Requires to remove the central auxiliary fuel tank if it has
been selected by the user. 2 Required for JAR OPS 3. 3 Incompatible
with EGPWS optional.
-
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.
225 09.101.01 E 26 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
Document reference
Commercial reference
Name kg lb
Interior Layout
07-10008-A 07-10008-00-CI Pilot and copilot Airline seats leader
type 18.2 40.1
07-10009-A 07-10009-00-FP 3rd man crew seat - Fixed Parts 0.2
0.4
07-10009-A 07-10009-00-RP 3rd man crew seat - Removable Parts
6.2 13.7
07-15009-A 07-15009-00-CI Pilot and copilot crashworthy seats
6.7 14.7
07-27002-A 07-27002-00-CI 19 crashworthy seat installation 219.1
483.03
07-30007-A 07-30007-00-CI Comfort upholstery with improved sound
proofing 93.4 205.9
07-30008-A 07-30008-00-CI "De Luxe" upholstery with enhanced
sound proofing On request
07-50014-A 07-50014-00-CI Special RH double door 7.0 15.4
07-50017-A 07-50017-00-CI Special LH door with built-in steps
15.0 33.1
07-60009-A 07-60009-00-FP Lugage Compartment in Pod Fixed Parts
3.4 7.5
07-60009-A 07-60009-00-RP Lugage Compartment in Pod Removable
Parts 30 66.1
07-60016-A 07-60016-00-CI Luggage compartment in the
intermediate structure 70.3 154.9
07-70002-A 07-70002-00-CI Self Contained Medical Unit 243.0
535.8
07-70003-A 07-70003-00-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
1 Removable Parts of this installation are not certified. 2
Equipment is not certified.
-
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.
225 09.101.01 E 27 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
Corporate VIP
Special LH door with built-in steps
Special RH double door
and
Doo
rs
Standard sliding doors
Luggage compartment with
standard rear access door
Standard rear access door R
ear
Seat
ing
8 + 1 VIP crashworthy seats with bar and toilet (with 1 or 2
lounges)
12 VIP crashworthy seats with bar and toilet
or 19 crashworthy
seats
De Luxe upholstery or
Comfort upholstery
Standard upholstery
Uph
olst
ery
10 + 1 VIP crashworthy seats with bar and toilet
or
Passenger transport Crew Change
Various Possibilities of the EC225 Cabin Installation
-
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.
225 09.101.01 E 28 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
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.
-
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.
225 09.101.01 E 29 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
Document reference
Commercial reference
Name kg lb
08-20001-A 08-20001-01-CI SAR Modes navigation package with
centralized radio
management system 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
08-21006-A 08-21006-00-CI Thales - AHV16 - 2nd Radio altimeter
5.8 12.7
08-24007-A 08-24007-00-CI Collins - Proline 21 - ADF #2 6.2
13.6
08-27039-A 08-27039-00-CI Chelton DF935 V/UHF DF 9.9 21.8
08-31039-A 08-31039-00-CI Telephonics 1600 Weather Radar,
displayed on AHCAS 24.0 52.9
08-35009-A 08-35009-01-CI TCAS - GOODRICH - HP 899 integrated to
AHCAS 8.8 19.4
08-35015-A 08-35015-00-CI EGPWS - HONEYWELL - MKXXII integrated
to AHCAS 1 8.6 18.9
08-41012-A 08-41012-00-CI Canadian Marconi - CMA3024 - GPS
receiver 4.9 10.8
1 Incompatible with optional item Automatic Voice Alarm Device
(AVAD).
-
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.
225 09.101.01 E 30 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
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
10-45002-A 10-45002-00-CI Missile Warning System On request
10-51013-A 10-51013-00-FP Chaff and flares dispenser
installation - Fixed Parts On request
10-51013-A 10-51013-00-RP Chaff and flares dispenser
installation - Removable Parts On request
1 Compatible with JAR OPS-3 regulation. 2 The toolings of the
installation are not included in the price. 3 At least one ground
station per helicopter base must be purchased.
-
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.
225 09.101.01 E 31 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
Blank
-
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.
225 09.101.01 E 32 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
6- Main performance
The following performance values and figures refer to an EC225,
equipped with new engines Makila 2A1. Unless otherwise specified,
the values and figures refer to a clean helicopter at Sea Level
(SL), in International Standard Atmosphere (ISA) and zero wind
condition.
Performance on 2 engines
Gross Weight kg 9,000 9,500 10,000 10,500 11,000 lb 19,842
20,944 22,046 23,149 24,251 Maximum speed, VNE km/h 324 324 324 324
324
kts 175 175 175 175 175
Maximum cruise speed (at MCP) km/h 275 273 270 266 262
kts 149 148 146 144 142
Recommended cruise speed km/h 261 262 263 265 262
kts 141 141 142 143 142
Fuel consumption at recommended cruise speed kg/h 608 620 632
649 655
lb/h 1,340 1,367 1,393 1,431 1,444
Rate of climb (80kt, 2 engines at MCP) m/s 8.7 7.8 6.9 6.1
5.4
ft/mn 1,709 1,529 1,362 1,208 1,064
Hover Ceiling IGE (at Take-off power, 10 ft)
ISA m 3,888 3,370 2,874 2,396 1,935
ft 12,756 11,058 9,431 7,861 6,350
ISA+20 m 3,197 2,679 2,178 1,648 1,141
ft 10,487 8,788 7,144 5,407 3,743
Hover Ceiling OGE (at Take-off power)
ISA m 3,099 2,572 2,065 1,578 792
ft 10,166 8,438 6,776 5,176 2,600
ISA+20 m 2,389 1,812 1,261 731 93
ft 7,838 5,946 4,138 2,398 305
Service ceiling (Vz=0.508m/s = 100ft/mn) m 5,918 5,413 4,933
4,469 4,041
ft 19,417 17,760 16,185 14,661 13,257
-
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.
225 09.101.01 E 33 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
Gross Weight kg 9,000 9,500 10,000 10,500 11,000 lb 19,842
20,944 22,046 23,149 24,251 Maximum range
(without reserve, at economical cruise speed)
standard tanks km 887 876 865 852 838
nm 479 473 467 460 452
standard + central tanks km 1,000 988 976 961 946
nm 540 534 527 519 511
standard + central tanks + pod km 1,197 1,185 1,169 1,152
1,135
nm 646 640 631 622 613
Maximum endurance
without reserve, at 148km/h = 80kts)
standard tanks h:mn 4:32 4:24 4:17 4:11 4:5
standard + central tanks h:mn 5:08 4:59 4:51 4:44 4:37
standard + central tanks + pod h:mn 6:16 6:05 5:55 5:46 5:38
-
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.
225 09.101.01 E 34 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
Performance on 1 engine Gross Weight kg 9,000 9,500 10,000
10,500 11,000 lb 19,842 20,944 22,046 23,149 24,251Rate of climb
(80kt, 1 engines at OEI unlimited) m/s 4.3 3.6 2.9 2.3 1.7 ft/mn
850 709 577 453 334
Service ceiling (80kt, 1 engines at OEI unlimited) m 3,066 2,519
1,971 1,453 970Vz=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 6,095 m 20,000 ft (PA) Take-off and
landing 3,353 m 11,000 ft (DA)
Maximum temperature ISA + 40C limited to 50C
Minimum temperature -30C (standard configuration)
-45C (requires the installation of kit for flight in extreme
cold weather to be contracted separately)
Abbreviations AEO : All Engines Operative SL : Sea Level DA :
Density Altitude TAS True Air Speed IGE : In Ground Effect VNE :
Never Exceed Speed ISA : International Standard Atmosphere Vz :
Rate-of-climb MCP : Maximum Continuous Power Zp : Barometric
Altitude OEI : One Engine Inoperative Vp : Airspeed OGE : Out of
Ground Effect Vmax : Maximum cruise speed PA : Pressure Altitude
Vreco : Economical cruise speed
Units nm : nautical miles hr:min : hours:minutes kts: knots kg :
kilograms ft/min : feet/minute lb : pounds m/sec : meters per
seconds km : kilometres C : degrees Celsius kg/hr : kilograms per
hour
-
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.
225 09.101.01 E 35 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
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 + 20C (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 + 20C; 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
+ 20C ; T.A.S = 80 kts)
Page 44
Hourly fuel consumption (SL, ISA) Page 45
Hourly fuel consumption (SL, ISA + 20C) Page 46
Hourly fuel consumption (Zp = 5000ft, ISA) Page 47
Hourly fuel consumption (Zp = 5000ft, ISA + 20C) Page 48
Payload / Range Chart (SL, ISA) Page 49
Payload / Range Chart (SL, ISA + 20C) Page 50
-
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.
225 09.101.01 E 36 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
Take-off weight in hover IGE, AEO 5 min
10 ft, on 2 engines, at take-off power
0
5000
10000
15000
20000
-30 -20 -10 0 10 20 30 40 50
OAT (C)
Pressure altitude (ft) ISO-Weight (kg)
ISA
-20
ISA
ISA
+ 20
70007500
8000
8500
9000
9500
100001050011000
ISA
+ 35
-
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.
225 09.101.01 E 37 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
Take-off weight in hover OGE, AEO 5 min
on 2 engines, at take-off power
0
5000
10000
15000
20000
-30 -20 -10 0 10 20 30 40 50
OAT (C)
Pressure altitude (ft) ISO-Weight (kg)
ISA
-20
ISA
ISA
+ 207000
7500
8000
8500
9000
9500
1000010500
11000
ISA
+ 35
-
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.
225 09.101.01 E 38 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
Take-off weight from a clear area (EASA Category A)
0
5000
10000
15000
20000
-30 -20 -10 0 10 20 30 40 50
OAT (C)
Pressure altitude (ft) ISO-Weight (kg)
ISA
-20
ISA
ISA
+ 20
6500
7000
7500
8000
8500
9000 9500 10000 10500 11000
ISA
+ 35
-
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.
225 09.101.01 E 39 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
Fast cruise speed
Zp = 0, ISA on 2 engines, at maximum continuous power
265 275 285
16000
18000
20000
22000
24000
7000
8000
9000
10000
11000
140 150
T.A.S (kt)
(km/h)
Weight (kg) (lb)
-
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.
225 09.101.01 E 40 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
Fast cruise speed
Zp = 0, ISA + 20 on 2 engines, at maximum continuous power
265 275 285
16000
18000
20000
22000
24000
7000
8000
9000
10000
11000
140 150
T.A.S (kt)
(km/h)
Weight (kg) (lb)
-
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.
225 09.101.01 E 41 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
Rate of climb in oblique flight
ISA T.A.S. = 80 kts on 2 engines, at maximum continuous
power
0
5000
10000
15000
20000
0 500 1000 1500 2000 2500 3000
Rate of climb (ft/mn)
Pressure Altitude (ft) ISO-Weight (kg)
800
0
850
0
9000
9500
10000
10500
11000
650
0
70
00
75
00
-
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.
225 09.101.01 E 42 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
Rate of climb in oblique flight
ISA + 20 - T.A.S. = 80 kts on 2 engines, at maximum continuous
power
0
5000
10000
15000
20000
0 500 1000 1500 2000 2500 3000
Rate of climb (ft/mn)
Pressure Altitude (ft) ISO-Weight (kg)
6500
7000
7500
8000
8500
9000
9500
10000
10500
11000
-
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.
225 09.101.01 E 43 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
Rate of climb in oblique flight
ISA - T.A.S. = 80 kts on 1 engine, OEI unlimited
Pressure altitude (ft) (m) ISO-WEIGHT (kg)
00 10 1
0
1000
2000
3000
4000
5000
6000
0
5000
10000
15000
20000
0 500 1000 1500 2000
Rate of climb (ft/mn)
(m/s)
6500
7000
7500
8000
8500
9000
9500
10000
10500
11000
-
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.
225 09.101.01 E 44 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
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)
00 10 1
0
1000
2000
3000
4000
5000
6000
0
5000
10000
15000
20000
0 500 1000 1500 2000
Rate of climb (ft/mn)
(m/s)
6500
7000
7500
8000
8500
9000
9500
10000
10500
11000
-
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.
225 09.101.01 E 45 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
Hourly fuel consumption
SL, ISA
150 200 250
950
1050
1150
1250
1350
1450
400
450
500
550
600
650
700
60 80 100 120 140 160
T.A.S (kt)
(km/h)
Hourly fuel consumption (kg/h) (lb/h)ISO-Weight (kg)
6500
7000
7500
8000
8500
9000
9500
10000
10500
11000
Vmax
Vre
co
-
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.
225 09.101.01 E 46 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
Hourly fuel consumption
SL, ISA + 20
150 200 250
950
1050
1150
1250
1350
1450
400
450
500
550
600
650
700
60 80 100 120 140 160
T.A.S (kt)
(km/h)
Hourly fuel consumption (kg/h) (lb/h)ISO-Weight (kg)
6500
7000
7500
8000
8500
9000
9500
10000
10500
11000
Vmax
Vre
co
-
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.
225 09.101.01 E 47 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
Hourly fuel consumption
Zp = 5000 ft, ISA
Hourly fuel consumption (kg/h) ISO-WEIGHT (kg)
350
400
450
500
550
600
650
60 80 100 120 140 160
T.A.S (kt)
6500
7000
7500
8000
8500
9000
9500
10000
10500
11000
Vmax
Vreco
-
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.
225 09.101.01 E 48 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
Hourly fuel consumption
Zp = 5000 ft, ISA + 20
Hourly fuel consumption (kg/h) ISO-WEIGHT (kg)
350
400
450
500
550
600
650
60 80 100 120 140 160
T.A.S (kt)
6500
7000
7500
8000
8500
9000
9500
10000
10500
11000
Vmax
Vreco
-
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.
225 09.101.01 E 49 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
PAYLOAD / RANGE CHART
SL ISA
0
1000
2000
3000
4000
5000
0 100 200 300 400 500 600
Range (nm)
Payload (kg)(1
)
(2)
MTOW=11000kg
(3)
MTOW=11000 kg
MTOW=11000 kg
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
-
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.
225 09.101.01 E 50 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
PAYLOAD / RANGE CHART
SL ISA + 20C
0
1000
2000
3000
4000
5000
0 100 200 300 400 500 600
Range (nm)
Payload (kg)(1
)
(2)
MTOW=11000kg
(3)
MTOW=11000 kg
MTOW=11000 kg
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
-
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.
225 09.101.01 E 51 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
7- Customer Service Overview
Assets
Proven reliability and availability based on experience
EUROCOPTERs 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.
-
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.
225 09.101.01 E 52 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
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 : Pilots 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
16 years periodicity tasks
1200 MMH
Scheduled Engine Inspection
MAKILA 2A1
Estimated Man Hour
15 flight hrs periodicity tasks
75 flight hrs periodicity tasks
750 flight hrs periodicity tasks
0,1168 MMH per FH
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.
-
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.
225 09.101.01 E 53 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
Main components Time Between Overhaul (TBO) / Service Life Limit
(SLL) 1
Main Components
TBO (h) as per MSM
2008 Ed.
TBO (h) Target Value *
SLL (h) as per MSM
2008 Ed. ALTERNATOR 40 KVA 3000
AUXILARY HYDRAULIC PUMP 3000 5000
MAIN ROTOR AND TAIL ROTOR BLADES 20000
MAIN ROTOR HUB OC
BENDIX ENGINE-MGB COUPLING SHAFT ASSY 4800
MGB MAIN MODULE 2000 3000
MGB EPYCICLIC MODULE 2000 3000
MGB ACCESSORY DRIVE GEAR BOX LH 2000 3000
MGB ACCESSORY DRIVE GEAR BOX RH 3000 4000
MGB SUPPORT FLEX PLATE 6200
TAIL GEAR BOX 3000**
INTERMEDIATE GEAR BOX 3000**
MAIN SERVO CONTROL 3750 5000
TAIL SERVO CONTROL 3000 ** 5000
MAKILA 2A1 2750** 3750
*: Target value within the Maturity Plan under progress. ** = in
MSM first half 2009
Engines
TBO (h) as per MSMrev RT003b
TBO (h) Target Value *
SLL (h) as per MSMrev RT003b
MAKILA 2A1 2500 3000
*: 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.
-
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.
225 09.101.01 E 54 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
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
-
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.
225 09.101.01 E 55 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
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.
-
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.
225 09.101.01 E 56 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
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
