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

Technical Data

332 L1 08.101.01 E

EUROCOPTER

AS332 L1

C

M

J

CM

MJ

CJ

CMJ

N

Base_Super_Puma.ai 08/03/2006 10:05:58Base_Super_Puma.ai 08/03/2006 10:05:58

SUPER PUMA(Civil Version)

COUGAR(Military Version)

EC 225

Naval versionmissiles/torpedoesAS 532 SC (MK1)

Stretched versionutility/armed

AS 532 AL (MK1)

Utility/armed versionEC 725

Technical Data

AS 332 L1 (MK1)

EUROCOPTER

AS332 L1

AS 332 C1 (MK1)

PageTD332L1.pdf 10/01/2008 17:11:16

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.

332 L1 08.101.01 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 - 2008

Contents

1 - Foreword........................................................................................................... 3

2 - General characteristics .................................................................................. 5

3 - Baseline Aircraft Definition ............................................................................. 10

4 - Recommended Mission Configurations......................................................... 13

5 - Optional equipment ....................................................................................... 17

6 - Main performance ............................................................................................ 25

7 - Customer Service Overview............................................................................ 47

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.

332 L1 08.101.01 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 - 2008

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.

332 L1 08.101.01 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 - 2008

1- Foreword

The AS332 L1 is a medium weight twin engine helicopter (8,6 tons class) with outstanding performance that belongs to the famous Super-Puma/Cougar family. Over 661 units, with total flight time in excess of 3,500,000 Flight Hours have been delivered to date. The AS332 L1 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 seats in a spacious cabin and 3 crew members. Technical advancements developed by EUROCOPTER on the AS332 L1 include modular design of the mechanical assemblies, use of composite materials, all-weather IFR capability, even under icing conditions with a special optional equipment, “On Condition” maintenance for most of the equipment items and several transmission assemblies and improvement of the survivability in case of crash. Fitted with the appropriate equipment, the Super Puma is capable of the following missions further to the basic passenger transport mission : Internal load or external load carrying, Casualty evacuation and MEDEVAC missions, Search and rescue and VIP transport The AS 332 L1 is primarily operated in oil production fields.

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.

332 L1 08.101.01 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 - 2008

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.

332 L1 08.101.01 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 - 2008

2- General Characteristics Layout

Minimum crew (D.G.A.C Category A and B certification)

VFR : 1 pilot (< 20,000ft Pressure Altitude, with at least one lane of each autopilot channel engaged) else 2 pilots.

IFR : 2 pilots

Passenger transport (in addition to the crew)

: up to 19 comfort seats

VIP transport (in addition to the crew)

: up to 12 seats

Weights Note : Empty weight accuracy : within ± 2 % kg lb

Empty weight, standard aircraft (including engine oil) 4,515 9,954

Useful load 4,085 9,006 Maximum all-up weight 8,600 18,960 Maximum cargo-sling load 4,500 9,920 Maximum all-up weight in external load configuration 9,350 20,615

Power plant 2 Turbomeca Makila 1A1 turboshaft engines Engine ratings Power per engine, in standard atmosphere, at sea level : kW ch shp

Maximum emergency power 1,400 1,902 1,877 Intermediate emergency power 1,330 1,807 1,783 Take-off power 1,357 1,845 1,819 Maximum continuous power 1,185 1,610 1,588

Usable Fuel capacities

litres US gal. kg lb Standard fuel tanks 2,020 535 1,595 3,516 Auxiliary fuel tanks (option)

Central fuel tank 321 85 254 560 External fuel tanks 2 x 326 2 x 86 2 x 257 2 x 567 Cabin fuel tank 600 158 474 1,045 1 to 5 ferrying fuel tanks 5 x 475 5 x 126 5 x 375 5 x 827 Pod Fuel tank 600 157 474 1045

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.

332 L1 08.101.01 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 - 2008

Main dimensions

Dimensions with blades folded

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.

332 L1 08.101.01 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 - 2008

Dimensions of compartments and accesses

Cabin floor characteristics

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.

332 L1 08.101.01 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 - 2008

Main Assets

Safety (Excellent visibility, 2 large sliding doors on both sides)

Comfort (19 seating configuration)

Economic (competitive operating costs)

Performance (high speed, endurance, high availability rate)

Standard cockpit

The cockpit has been designed to accommodate all the flight instruments as well as optional radio-commutation or radio-navigation equipment enabling the aircraft to be flown in IFR conditions.

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.

332 L1 08.101.01 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 - 2008

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.

332 L1 08.100.01 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 - 2008

3- Super Puma AS332 L1 - 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.

332 L1 08.100.01 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 - 2008

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.

332 L1 08.100.01 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 - 2008

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.

332 L1 08.101.01 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 - 2008

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 AS 332L1 around the world. For the AS 332L1, the recommended mission configuration is Offshore mission. 4.1 Recommended Offshore Configuration The AS 332 L1 is primarily operated in oil production fields.

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.

332 L1 08.101.01 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 - 2008

Mission configuration

Document reference

Commercial reference

Name

00-10021-A 00-10021-00-CI AS 332 L1 Baseline aircraft as per 332 L1 08.100.01 E

General Equipment 05-01010-A 05-01010-00-CI CAA kit 05-03005-A 05-03005-00-CI First aid kit 05-26005-A 05-26005-00-CI Dinol AV30 re-inforced anti-corrosive treatment 05-31017-A 05-31017-00-CI Cockpit green tinted panes plus sun vizors with standard colourless panes in

front of the pilot and copilot 05-39001-A 05-39001-00-CI Map holder 05-50006-A 05-50006-00-CI Kit for flight in limited icing conditions (submitted approval by local Airworthiness

Authority) 05-51002-A 05-51002-00-CI De-iced cockpit center pane with wiper 05-52004-A 05-52004-00-CI Goodrich Icing severity indicator (ex-Rosemount) 05-81022-A 05-81022-00-CI Central auxiliary fuel tank 321 l (85 US gal) 05-82013-A 05-82013-00-CI Pressure refuelling on the ground usable with maritime sponsons and floatation

gear 05-93003-A 05-93003-00-CI Naval mooring 05-93005-A 05-93005-00-CI Lashing rings for main landing gear 05-52004-A 05-52004-00-CI Goodrich Icing severity indicator (ex-Rosemount)

Specific Mission Equipment 06-21012-A 06-21012-00-FP Hydraulic hoist with variable speed 75 meter cable, 272kg (246ft, 600lb) - Fixed

parts 06-27015-A 06-27015-00-FP Cargo sling with dynamometer (3 metric tons) - Fixed parts 06-42023-A 06-42023-00-CI Fixed lights in maritime sponson 06-60003-A 06-60003-00-CI 2 AERAZUR SR14 self-righting life rafts (with jettison control in cockpit and

survival aid kits) in the sponsons 06-61012-A 06-61012-00-CI Emergency floatation gear, usable without external fuel tanks 06-64001-A 06-64001-00-CI Sea anchor 06-65001-A 06-65001-00-CI 3rd hand held fire extinguisher 06-65009-A 06-65009-00-CI 2 Flashlights 06-66003-A 06-66003-00-CI Helicopter Emergency Egress Lighting (HEEL) 06-67013-A 06-67013-00-CI Serpe - IESM Kannad 406 AP - Emergency Locator Transmitter 06-67020-A 06-67020-00-CI HR Smith serie 503 ADELT 06-69001-A 06-69001-00-CI Automatic Voice Alarm Device (AVAD)

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.

332 L1 08.101.01 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 - 2008

Document reference

Commercial reference

Name

Interior Layout 07-10006-A 07-10006-00-CI Pilot and copilot Airline seats leader type 07-25020-A 07-25020-00-CI 19 comfort places with 3-place rear bench seat 07-30011-A 07-30011-00-CI Airline type upholstery with improved sound proofing 07-60003-A 07-60003-00-CI Enlarged luggage hold with 1 special step door WITH bench seat integrated in

cabin bulkhead

Avionics 08-00017-B 08-00017-01-CI Civil Use minimum items of equipment (VFR/IFR dual pilot)

08-12024-A 08-12024-00-CI NAT - NPX138 VHF/FM-H

08-16032-A 08-16032-00-CI Team ICS - Complementary set : 4th control panel CP 1976 08-17043-A 08-17043-00-CI NAT - Passenger address 08-27031-A 08-27031-00-CI Chelton System 7 - (121,5) VHF/FM Marine dual frequency homer 08-31001-A 08-31001-00-CI Telephonics 1400 C Weather Radar

08-43004-A 08-43004-00-CI Freeflight - TNL 2101 APPROACH +, GPS Navigation System linked to HSI and AFCS

08-73001-A 08-73001-00-CI Sagem Avionics - CDV 85 P3 - Flight Director Coupler

08-83006-A 08-83006-00-CI EUROHUMS

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.

332 L1 08.101.01 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 - 2008

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.

332 L1 08.101.01 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 - 2008

5- Optional equipment Note : value of the weight breakdown is given for information and shall no t be considered as contractual.

Document reference

Commercial reference

Name kg lb

General equipment

05-01010-A 05-01010-00-CI CAA kit 7.5 16.5

05-03005-A 05-03005-00-CI First aid kit - JAR OPS 3 compatible 2.0 4.4

05-21012-A 05-21012-00-FP Wire strike protection system - Fixed parts 3.0 6.6

05-21012-A 05-21012-00-RP Wire strike protection system - Removable parts 9.9 21.8

05-22009-A 05-22009-00-CI Multipurpose engine air intakes (stretched version) 1 62.0 136.7

05-25012-A 05-25012-00-CI Main rotor blades re-inforced sand-erosion protection strip (loose equipment, delivered uninstalled)

0.3 0.7

05-25013-A 05-25013-00-CI Tail rotor blades re-inforced sand-erosion protection strip (loose equipment, delivered uninstalled)

0.1 0.2

05-26005-A 05-26005-00-CI Dinol AV30 re-inforced anti-corrosive treatment 14.0 30.9

05-31017-A 05-31017-00-CI Cockpit green tinted panes plus sun vizors with standard colourless panes in front of the pilot and copilot

3.4 7.5

05-31018-A 05-31018-00-CI Cockpit green tinted upper panes plus sun vizors 3.4 7.5

05-31020-A 05-31020-00-CI Cabin green tinted windows, for stretched versions 0.0 0.0

05-31022-A 05-31022-00-CI Cabin metalized windows, for stretched versions 0.0 0.0

05-31024-A 05-31024-00-CI 2 observation bubble windows, in cabin plug-in doors (1 on each side)

1.0 2.2

05-32006-A 05-32006-00-CI Windshield washers 1.5 3.3

05-39001-A 05-39001-00-CI Map holder - JAR OPS 3 compatible 1.0 2.2

05-42009-A 05-42009-00-CI Air conditioning system with pod mounted unit (to be used with Airline-type sound proofing)

100.0 220.5

05-42009-A 05-42009-01-CI Air conditioning system with pod mounted unit (to be used with VIP-type sound proofing)

82.7 182.3

05-50004-A 05-50004-00-CI Installation for flight in icing conditions 145.0 319.6

05-50005-A 05-50005-00-CI Installation for flight in extreme cold weather 56.1 123.7

05-50006-A 05-50006-00-CI Kit for flight in limited icing conditions (submitted approval by local Airworthiness Authority)

2.0 4.4

05-51002-A 05-51002-00-CI De-iced cockpit center pane with wiper 11.0 24.3

05-52004-A 05-52004-00-CI Goodrich Icing severity indicator 3.0 6.6

05-62008-A 05-62008-00-CI Two 30/40 kVA alternators and 2nd electrical box 2 22.0 48.5

05-67006-A 05-67006-00-CI 220V/ 50Hz AC Power socket in cabin 0.0 0.0

05-80004-A 05-80004-00-CI Re-inforced floor with crashworthy fixations and crashworthy fuel tanks (longitudinal, transverse and rear)

85.8 189.2

1 Mounted in production-line instead of the standard air intakes. 2 Instead of the 20/30 kVA standard ones.

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.

332 L1 08.101.01 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 - 2008

Document reference

Commercial reference

Name kg lb

General equipment (continued)

05-81010-A 05-81010-00-CI Crashworthy central auxiliary fuel tank 318 l (84 US gal) 27.5 60.6

05-81011-A 05-81011-00-CI Crashworthy external additional fuel tanks 2 x 318 l (2 x 84 US gal)

134.5 296.5

05-81022-A 05-81022-00-CI Central auxiliary fuel tank 321 l (85 US gal) 21.9 48.3

05-81024-A 05-81024-00-CI External additional fuel tanks 2 x 326 l (2 x 86 US gal) 109.5 241.4

05-81026-A 05-81026-00-FP Additional crashworthy pod fuel tanks - Fixed parts On Request

05-81026-A 05-81026-00-RP Additional crashworthy pod fuel tanks – Removable parts On Request

05-82012-A 05-82012-00-CI Pressure refuelling on the ground usable with additional external tanks, and jettisonable plug-in cabin doors

18.1 39.9

05-82013-A 05-82013-00-CI Pressure refuelling on the ground usable with maritime sponsons and floatation gear

12.4 27.3

05-82014-A 05-82014-00-CI Pressure refuelling on the ground usable with standard sponsons

15.6 34.4

05-84006-A 05-84006-00-RP One ferrying fuel tank 475 l (126 US gal), 1 to 4 tanks per helicopter

23.9 52.7

05-84007-A 05-84007-00-CI 5th ferrying fuel tank 475 l (126 US gal) 35.5 78.3

05-86002-A 05-86002-00-CI Fuel anti icing installation (-45°C) 0.0 0.0

05-92005-A 05-92005-00-FP Main rotor blade folding system - Fixed parts 6.4 14.1

05-92005-A 05-92005-00-RP Main rotor blade folding system - Removable Parts 50.9 112.2

05-93003-A 05-93003-00-CI Naval mooring 3.7 8.2

05-93005-A 05-93005-00-CI Lashing rings for main landing gear 1.0 2.2

05-94001-A 05-94001-00-CI Main landing gear kneeling system 1 4.5 9.9

Specific mission equipment

06-20002-A 06-20002-00-FP Double hoist installation - Fixed Parts 15.0 33.1

06-20002-A 06-20002-00-RP1 Double hoist installation - Removable Parts (Main Hoist & Beam)

103.0 227.0

06-20002-A 06-20002-00-RP2 Double hoist installation - Removable Parts (Backup Hoist) 45.0 99.2

06-21012-A 06-21012-00-FP Hydraulic hoist with variable speed 75 meter cable, 272kg (246ft, 600lb) - Fixed parts

6.9 15.2

06-21012-A 06-21012-00-RP Hydraulic hoist with variable speed 75 meter cable, 272kg (246ft, 600lb) - Removable parts

47.8 105.4

06-21024-A 06-21024-00-FP Goodrich 28V electrical hoist (290ft, 600lb) - Fixed parts 13.0 28.6

06-21024-A 06-21024-00-RP Goodrich 28V electrical hoist (290ft, 600lb) - Removable parts

103.0 227.0

06-25003-A 06-25003-00-CI Drip tub 7.0 15.4

1 Needs to procure the hydraulic circuits linkage sold as reference tools n°332A.95.4000.00.

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.

332 L1 08.101.01 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 - 2008

Document reference

Commercial reference

Name kg lb

Specific mission equipment (continued)

06-26005-A 06-26005-00-CI External mirrors (recommended for sling) 6.5 14.3

06-27015-A 06-27015-00-FP Cargo sling with dynamometer (3 metric tons) - Fixed parts 8.8 19.4

06-27015-A 06-27015-00-RP Cargo sling with dynamometer (3 metric tons) - Removable parts

22.1 48.7

06-27017-A 06-27017-00-FP Cargo sling with dynamometer (4.5 metric tons)-Fixed parts 4.1 9.0

06-27017-A 06-27017-00-RP Cargo sling with dynamometer (4.5 metric tons) – Removable parts 1

23.9 52.7

06-31017-A 06-31017-00-FP Hailer installation (Qty 1) - Fixed Parts 15.1 33.0

06-31017-A 06-31017-00-RP Hailer installation (Qty 1) - Removable Parts 25.8 56.7

06-42010-A 06-42010-00-CI Second landing light 2 5.0 11.0

06-42023-A 06-42023-00-CI Fixed lights in maritime sponsons 2 3.5 7.7

06-43004-A 06-43004-00-CI Vertical light for hoisting and sling operation surveillance 6.7 14.8

06-45014-A 06-45014-00-FP Search light Spectrolab SX 16 - Fixed parts 4.9 10.8

06-45014-A 06-45014-00-RP Search light Spectrolab SX 16 - Removable parts 24.0 52.9

06-51020-A 06-51020-00-CI FLIR On Request

06-60003-A 06-60003-00-CI 2 AERAZUR SR14 self-righting life rafts (with jettison control in cockpit and survival aid kits) in the sponsons 2

128.0 282.2

06-61012-A 06-61012-00-CI Emergency floatation gear, usable without external fuel tanks 196.6 433.5

06-61014-A 06-61014-00-FP Emergency floatation gear, usable with external fuel tanks - Fixed parts

25.9 57.1

06-61014-A 06-61014-00-RP Emergency floatation gear, usable with external fuel tanks - Removable parts

151.5 334.0

06-64001-A 06-64001-00-CI Sea anchor 2.9 6.4

06-65001-A 06-65001-00-CI 3rd hand held fire extinguisher - JAR OPS 3 compatible 2.2 4.9

06-65009-A 06-65009-00-CI 2 Flashlights - JAR OPS 3 compatible 1.2 2.6

06-66003-A 06-66003-00-CI Helicopter Emergency Egress Lighting (HEEL) 5.3 11.7

06-67013-A 06-67013-00-CI Serpe - IESM Kannad 406 AP - Emergency Locator Transmitter 3

2.1 4.6

06-67020-A 06-67020-00-CI HR Smith serie 503 - ADELT 7.6 16.8

06-68005-A 06-68005-00-CI Dukane DK120 Underwater Acoustic Beacon 0.5 1.1

06-69001-A 06-69001-00-CI Automatic Voice Alarm Device (AVAD) 1.3 2.9

06-81022-A 06-81022-00-CI Fire fighting kit (up to 3000 liters) 450.0 992.0

1 Requires to remove the central auxiliary fuel tank if it has been selected by the user 2 Required for JAR OPS 3. 3 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.

332 L1 08.101.01 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 - 2008

Document reference

Commercial reference

Name kg lb

Interior layout

07-10006-A 07-10006-00-CI Pilot and copilot Airline seats leader type 18.2 40.1

07-25020-A 07-25020-00-CI 19 comfort places with 3-place rear bench seat 1 196.7 433.6

07-25022-A 07-25022-00-CI 19 comfort seats installation without 3-place rear bench seat 209.2 461.2

07-30009-A 07-30009-00-CI VIP upholstery with enhanced sound proofing On Request

07-30011-A 07-30011-00-CI Airline upholstery with improved sound proofing 157.0 346.1

07-50013-A 07-50013-00-CI Special RH double door 7.0 15.4

07-50015-A 07-50015-00-CI Special LH door with built-in steps 15.0 33.1

07-50021-A 07-50021-00-CI Rear built-in step door 2 8.3 18.3

07-60003-A 07-60003-00-CI Enlarged luggage hold with 1 special step door with bench seat integrated in cabin bulkhead

48.6 107.1

07-60004-A 07-60004-00-CI Enlarged luggage hold with 1 special step door without bench seat integrated in cabin bulkhead

40.0 88.2

07-70001-A 07-70001-00-CI Self Contained Medical Unit 210.4 463.9

07-70016-A 07-70016-00-CI Air Ambulance Technology EMS quick conversion kit (2 Units of 3 stretchers each)

On Request

07-71014-A 07-71014-00-CI Casualty-carrying installation (without stretchers and seats) 3 28.9 63.7

07-74010-A 07-74010-00-CI Stretcher (NATO type) (loose equipment delivered separately) 4

8.3 18.3

07-80004-A 07-80004-00-CI VIP 11 seats with galley and toilet On Request

07-80005-A 07-80005-00-CI VIP 10+2 seats with galley and toilet 580.0 1278.7

07-80012-A 07-80012-00-CI VIP 10 seats with galley and toilet 555.0 1223.6

07-82008-A 07-82008-00-CI Retractable armrests On Request

07-82009-A 07-82009-00-CI Lombar adjustment On Request

07-83001-A 07-83001-00-CI Electric curtains On Request

07-84003-A 07-84003-00-CI Customized inlaid wood table On Request

07-85007-A 07-85007-00-CI Transparent central partition with storage compartment On Request

07-91001-A 07-91001-00-CI Gold finishing of cabin visible metallic parts 2.0 4.4

1 Installation including 17 comfort seats and the cushions of the 3 bench seats integrated in the cabin bulkhead. 2 Recommended in VIP configuration. 3 The removable parts of present complete installation are not certified. 4 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.

332 L1 08.101.01 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 - 2008

Various Possibilities of the AS332 L1 Cabin Installation

or

Luggage hold with bench seat

Standard upholstery

Passenger transport Crew change

Corporate VIP

10 seats VIP

VIP upholstery

19 comfort seats

19 comfort places

Airline upholstery

10 + 2 seats VIP

Rear built-in step door

Doo

rs

Rea

r Se

atin

g

Standard sliding doors

Special LH door with built-in steps

Special RH double door

and

or Luggage hold without

bench seat

Standard

11 seats VIPor

or

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.

332 L1 08.101.01 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 - 2008

Document reference

Commercial reference

Name kg lb

Avionics

08-00017-B 08-00017-01-CI Civil Use minimum items of equipment (VFR/IFR dual pilot) including:

65.3 144.0

Collins - VHF22A #1

Collins - VHF22A #2

ICS - Basic set : 3 control panels CP 1976 in cockpit

Thales - AHV16 - Radio altimeter with indicator IND 201

Collins - TDR94D - Transponder Elementary Surveillance (including flight identification)

Collins - ADF 60 - ADF #1

Collins - DME 42 - DME

Collins - VIR 32 - VOR/ILS/MKR #1

Collins - VIR 32 - VOR/ILS/MKR #2

Shadin - 8800T - Altitude encoder

08-00018-C 08-00018-02-CI Search & Rescue minimum items of equipment (VFR/IFR dual pilot) including:

On Request

Collins - VHF22A #1

Collins - VHF22A #2

ICS - Basic set : 3 control panels CP 1976 in cockpit

ICS - Complementary set : 4th control panel CP 1976 in cabin

Thales - AHV16 - Radio altimeter

Thales - AHV16 - 2nd Radio altimeter

Collins - TDR94D - Transponder Elementary Surveillance (including flight identification)

Collins - ADF 462 - ADF #1

Collins - DME 442 - DME

Collins - VIR 432 - VOR/ILS/MKR #1

Collins - VIR 432 - VOR/ILS/MKR #2

Telephonics - 1500B - Search Radar with 9 inches display

Canadian Marconi - CMA 3024 - GPS receiver

Canadian Marconi - CMA 9000 - Flight Management System with SAR mode

Collins - MFD255 - Displays (Qty 4)

Marconi - ANV 353 - Doppler Radar

Sagem Avionics (ex-Sfim) - CDV 155 - Flight director coupler

The radio/com/nav. equipment weight figures included in this chapter are average values. As the installation of those equipment may vary from one a/c to an other, the weight of a complete configuration with multiple items may not be the simple sum of all individual weights.

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.

332 L1 08.101.01 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 - 2008

Document reference

Commercial reference

Name kg lb

Possible add-ons depending on mission needs

08-10002-A 08-10002-00-CI Collins - HF 9X00 - HF/SSB 24.3 53.6

08-12024-A 08-12024-00-CI NAT - NPX138 VHF/FM-H 5.0 11.0

08-15515-A 08-15515-00-CI Satcom / Internet (Thuraya / Iridium / Inmarsat) On Request

08-16032-A 08-16032-00-CI Team ICS - Complementary set : 4th control panel CP 1976

3.1 6.8

08-17002-A 08-17002-00-CI Baker - M1060 - Passenger address 25.0 55.1

08-17012-A 08-17012-00-CI Team - BA1920 - Passenger Interphone 1.6 3.5

08-18030-A 08-18030-00-CI David Clark H10-13H - Headset 0.5 1.1

08-24004-A 08-24004-01-CI Collins - ADF 60 - ADF - #2 6.4 14.1

08-27021-A 08-27021-00-CI Chelton DF931-6 V/UHF DF 8.0 17.6

08-27031-A 08-27031-00-CI Chelton System 7 - (121,5) VHF/FM Marine dual frequency homer

5.4 11.9

08-31001-A 08-31001-00-CI Telephonics 1400 C Weather Radar, with beacon mode 28.0 61.7

08-43004-A 08-43004-00-CI Freeflight - TNL 2101 APPROACH +, GPS Navigation System linked to HSI and AFCS 1

3.5 7.7

08-73001-A 08-73001-00-CI Sagem Avionics - CDV 85 P3 - Flight Director Coupler 15.2 33.5

08-81014-A 08-81014-00-CI Allied Signal CVFDR 2 35.0 77.2

08-83006-A 08-83006-00-CI EUROHUMS 3 4 53.8 118.6 The radio/com/nav. equipment weight figures included in this chapter are average values. As the installation of those equipment may vary from one a/c to an other, the weight of a complete configuration with multiple items may not be the simple sum of all individual weights.

1 Delivered with EUROPE map. Subscription to be made by the customer. 2 Compatible with JAR OPS-3 regulation. 3 The toolings of the installation are not included in the price. 4 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.

332 L1 08.101.01 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 - 2008

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.

332 L1 08.101.01 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 - 2008

6- Main performance

The following performance values and figures refer to an AS332 L1 equipped with new engines. Unless otherwise specified, the values and figures refer to a clean helicopter at Sea Level (SL), in International Standard Atmosphere (ISA) and zero wind condition. Performance on 2 engines

Gross Weight kg lb

6,00013,230

7,000 15,430

8,00017,630

8,60018,960

Max. speed, VNE km/hr 304 303 298 278 kts 164 164 161 150 Maximum cruise speed km/hr 283 281 278 262

kts 153 152 150 141 Recommended cruise speed km/hr 265 262 258 252

kts 143 141 139 136 Fuel consumption at recommended cruise speed kg/hr 481 486 497 502

lb/hr 1,060 1,071 1,096 1,107 Fuel consumption at 70 kts kg/hr 335 353 374 389

lb/hr 739 778 825 858 Rate-of-climb at 70 kts m/sec. 14.7 12.1 9.8 8.2

ft/min. 2,894 2,382 1,920 1,618 Hover ceiling IGE (10ft) at take-off power

ISA m 6,500 5,100 3,950 3,250 ft 21,325 16,732 12,959 10,663

ISA + 20°C m 5,850 4,450 3,200 2,300 ft 19,193 14,560 10,499 7,546 Hover ceiling OGE at take-off power

ISA m 5,750 4,300 3,050 2,300 ft 18,865 14,108 10,007 7,546

ISA + 20°C m 5,200 3,550 2,100 1,400 ft 17,060 11,647 6,890 4,593 Service ceiling Vz = 150 ft/min

ISA m 7,200 5,900 4,650 >2,895

ft 23,622 19,357 15,255 >9,500 ISA + 20°C m 6,500 5,100 3,800 2,895

ft 21,325 16,732 12,467 >9,500 Maximum range

(without fuel reserve, at recommended cruise speed)

with standard fuel tanks km nm

736397

879 474

859464

841454

with external fuel tanks km n.m

664358

1148 620

1127609

1105596

with central auxiliary fuel tank km n.m.

724391

1021 551

1000540

979529

with external and central auxiliary fuel tanks km n.m.

652352

1192 644

1267684

1105597

with external, central and cabin fuel tanks km n.m.

624337

1164 628

1528825

1105597

with external, central and 5 ferrying tanks km n.m.

592319

1132 611

1662897

19761067

Maximum endurance (without fuel reserve, at 130 km/hr (70 kts))

with standard fuel tanks hr : min 4:08 4:49 4:34 4:24 with external fuel tanks hr : min 3:46 6:26 6:06 5:54 with central auxiliary fuel tanks hr : min 4:04 5:38 5:20 5:09 with external and central auxiliary fuel tanks hr : min 3:42 6:41 6:53 6:39 with external, central and cabin fuel tanks hr : min 3:32 6:32 8:23 8:06 with external, central and 5 ferrying tanks hr : min 3:21 6:21 9:09 10:46

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.

332 L1 08.101.01 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 - 2008

Performance in external load (maximum gross-weight of 9,350 kg – 20,615 lb) Rate of climb at 9,350 kg 6.4 m/sec

1,260 ft/min Hover ceiling OGE at take-off power

ISA 650 m 2,133 ft

ISA + 10°C 300 m 984 ft

ISA + 17°C Sea level Performance on 1 engine Gross Weight kg

lb 6,000

13,2307,000

15,430 8,000

17,6308,600

18,960

Rate-of-climb at intermediate emergency power S.L. m 9.0 6.8 4.7 3.4 ft/min 1,772 1,339 925 669

Service ceiling at intermediate emergency power (Vz = 0) ISA

m ft

5,20017,060

3,700 12,139

2,5008,202

1,8005,906

Service ceiling at intermediate emergency power (Vz = 0) ISA +20

m ft

4,50014,764

3,050 10,007

1,7505,741

9503,117

Maximum temperature for take-off in Cat. A from clear heliport at S.L.

°C >50 >50 >50 40

Maximum take-off weight at max. emergency power ISA ISA + 20°C

In hover IGE (10 ft) kg lb

7,500 16,534

6,900 15,211

In hover OGE kg lb

6,910 15,233

6,320 13,933

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 M < 8,350 kg : 7,620 m – 25,000 ft Pressure Altitude

M > 8,350 kg : 2,895 m – 9,500 ft Pressure Altitude Take-off and landing : 4,572 m – 15,000 ft Density Altitude

Maximum temperature ISA + 35°C limited to 50°C

Minimum temperature - 30°C (basic)

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.

332 L1 08.101.01 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 - 2008

- 45°C (with optional installation for flight in extreme cold weather) Abbreviations AEO : All Engines Operative SL : Sea Level AGL : Above Ground Level TAS True Air Speed DA : Density Altitude TOP : Take-Off Power IGE : In Ground Effect VNE : Never Exceed Speed ISA : International Standard Atmosphere VTOL : Vertical Take-Off and Landing MCP : Maximum Continuous Power Vtoss : Take-off safety speed OEI : One Engine Inoperative Vy : Optimum climbing speed OGE : Out of Ground Effect Vz : Rate-of-climb PA : Pressure Altitude Units nm : nautical miles hr:min : hours:minutes kts: knots kg : Kilograms ft/min : feet/minute lb : pounds m/sec : meters per second km : kilometers ° C : degrees Celsius

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.

332 L1 08.101.01 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 - 2008

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.

332 L1 08.101.01 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 - 2008

Performance charts The performance charts presented hereafter apply to an aircraft as per the standard definition.

Take-off weight in hover IGE, (10 ft, on 2 engines, at take-off power or max torque, no wind)

Page 31

Take-off weight in hover OGE, (on 2 engines, at take-off power or max torque, no wind)

Page 32

Maximum cruise speed Pitch : 16.5 for weight ≤ 8,350 kg – 18,410 lb Pitch : 16° for weight > 8,350 kg – 18,410 lb ISA

Page 33

Maximum cruise speed Pitch : 16.5 for weight ≤ 8,350 kg – 18,410 lb Pitch : 16° for weight > 8,350 kg – 18,410 lb ISA + 20°C

Page 34

Recommended cruise speed (pitch 15°5) ISA

Page 35

Recommended cruise speed (pitch 15°5) ISA + 20°C

Page 36

Rate of climb in oblique flight (on 2 engines, at best climb speed) ISA

Page 37

Rate of climb in oblique flight (on 2 engines, at best climb speed) ISA + 20°C

Page 38

Rate of climb in oblique flight (on 1 engine, at intermediate emergency power) ISA

Page 39

Rate of climb in oblique flight (on 1 engine, at intermediate emergency power) ISA + 20°C

Page 40

Hourly fuel consumption at maximum cruise speed (pitch 16°5, M ≤ 8,350 kg) ISA

Page 41

Hourly fuel consumption at maximum cruise speed (pitch 16°, M > 8,350 kg) ISA

Page 42

Hourly fuel consumption at maximum cruise speed (pitch 16°5, M ≤ 8,350 kg) ISA + 20°C

Page 43

Hourly fuel consumption at maximum cruise speed (pitch 16°, M > 8,350 kg) ISA + 20°C

Page 44

Hourly fuel consumption at recommended cruise speed ISA

Page 45

Hourly fuel consumption at recommended cruise speed ISA + 20°C

Page 46

Take off clear heliport CAT A Page 47

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.

332 L1 08.101.01 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 - 2008

TAKE-OFF WEIGHT IN HOVER IGE (HEIGHT = 10 FT)

(10 ft, on 2 engines, at take-off power or maximal torque, no wind)

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.

332 L1 08.101.01 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 - 2008

TAKE-OFF WEIGHT IN HOVER OGE

(on 2 engines, at take-off power or maximal torque, no wind)

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.

332 L1 08.101.01 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 - 2008

MAXIMUM CRUISE SPEED

Pitch: 16°5 for weight ≤ 8,350 kg - 18,410 lb

Pitch: 16° for weight > 8,350 kg - 18,410 lb

ISA

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.

332 L1 08.101.01 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 - 2008

MAXIMUM CRUISE SPEED

Pitch: 16°5 for weight ≤ 8,350 kg - 18,410 lb

Pitch: 16° for weight > 8,350 kg - 18,410 lb

ISA + 20°C

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.

332 L1 08.101.01 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 - 2008

RECOMMENDED CRUISE SPEED

Pitch: 15°5

ISA

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.

332 L1 08.101.01 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 - 2008

RECOMMENDED CRUISE SPEED

Pitch : 15°5

ISA + 20°C

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.

332 L1 08.101.01 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 - 2008

RATE-OF-CLIMB IN OBLIQUE FLIGHT

(on 2 engines, at best climb speed)

ISA

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.

332 L1 08.101.01 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 - 2008

RATE-OF-CLIMB IN OBLIQUE FLIGHT

(on 2 engines, at best climb speed)

ISA + 20°C

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.

332 L1 08.101.01 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 - 2008

RATE-OF-CLIMB IN OBLIQUE FLIGHT

(on 1 engine, at intermediate emergency power)

ISA

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.

332 L1 08.101.01 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 - 2008

RATE-OF-CLIMB IN OBLIQUE FLIGHT

(on 1 engine, at intermediate emergency power)

ISA + 20°C

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.

332 L1 08.101.01 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 - 2008

HOURLY FUEL CONSUMPTION

AT MAXIMUM CRUISE SPEED

(pitch 16°5)

M ≤ 8350 kg

ISA

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.

332 L1 08.101.01 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 - 2008

HOURLY FUEL CONSUMPTION

AT MAXIMUM CRUISE SPEED

(pitch 16°)

M > 8350 kg

ISA

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.

332 L1 08.101.01 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 - 2008

HOURLY FUEL CONSUMPTION

AT MAXIMUM CRUISE SPEED

(pitch 16°5)

M ≤ 8350 kg

ISA + 20°C

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.

332 L1 08.101.01 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 - 2008

HOURLY FUEL CONSUMPTION

AT MAXIMUM CRUISE SPEED

(pitch 16°)

M > 8350 kg

ISA + 20°C

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.

332 L1 08.101.01 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 - 2008

HOURLY FUEL CONSUMPTION

AT RECOMMENDED CRUISE SPEED

ISA

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.

332 L1 08.101.01 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 - 2008

HOURLY FUEL CONSUMPTION

AT RECOMMENDED CRUISE SPEED

ISA + 20°C

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.

332 L1 08.101.01 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 - 2008

TAKE-OFF CLEAR HELIPORT

Cat. A

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.

332 L1 08.101.01 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 - 2008

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 SUPER PUMA and COUGAR in service is around 600 helicopters world-wide. The total flight hours accumulated at this date are about 3,500,000 hours. The “lead the fleet” aircraft has accumulated 35,000 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.

332 L1 08.101.01 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 - 2008

Inspection Program

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

50 flight hrs periodicity tasks

13 MMH

500 flight hrs or 24 months periodicity tasks

220 MMH

Airframe Major Inspection Estimated Man Hour

7500 flight hrs or 15 years periodicity tasks

1200 MMH

Scheduled Engine Inspection

MAKILA 1A1

Estimated Man Hour

30 flight hrs periodicity tasks

50 flight hrs periodicity tasks

300 flight hrs periodicity tasks

600 flight hrs periodicity tasks

0,0836 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.

332 L1 08.101.01 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 - 2008

Main components Time Between Overhaul (TBO) / Service Life Limit (SLL) 1

Main Components TBO (h) SLL (h)

Alternator 40 KVA 5000

Hydraulic Pump 3000

Booster Pump 2000

Main Rotor Blades 20000

Main Rotor Hub 1500

Main Rotor Shaft 11000

Coupling Shaft 4800

Main Reduction Gear Module 3000

Main Oil Pumps 3000

Secondary Reduction Gear 3000

Accessory Drive Housing 3000

MGB Support Flexible Monting Plate 9500

Tail Gear Box 3500

Tail Rotor Hub 3500

Intermediate Gear Box 3400

Main and Tail Servo Control 3000

Main Components

TBO (h)

SLL (h)

MAKILA 1A1 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.

332 L1 08.101.01 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 - 2008

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.

332 L1 08.101.01 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 - 2008

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.

332 L1 08.101.01 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 - 2008

Engine Maintenance program Always looking to maximize your efficiency and reduce your costs, Turbomeca, the engine manufacturer has developed an improved service offering. Turbomeca has 32 Repair Centers across the globe, supplemented by several new factory-authorized service facilities strategically located near to you 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

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.

332 L1 08.101.01 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 - 2008

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 state-of-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. AS332 L1 - Example of basic training course

COURSE TYPE

COURSE REFERENCE THEORETICAL INSTRUCTION

FULL FLIGHT

SIMULATOR

FLIGHT INSTRUCTION

Type Rating (with simulator) 10 days 10 1/2 hours 2 hours Pilots Instructor Pilot Conversion (with simulator) (1) - 6 Hours 2 hours

COURSE TYPE

COURSE REFERENCE THEORETICAL & PRACTICAL INSTRUCTION

Mechanics Type Rating (Airframe + engine) 5 weeks

Avionics Type Rating 4 weeks Blades Maintenance and repair 2 weeks

(1) Pilot already qualified on AS332 L1 (mini 15 hours, within last 12 months, not included in Type Rating. Note: length is given as information and depends on pilot or technician qualification or experience. Complementary courses may be required.

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.

332 L1 08.101.01 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 - 2008

Engine Training Courses Training courses dedicated to Engine Maintenance is also organized by Turbomeca training schools and approved centers the world over Up-to-date course calendars, on-line tests and e-learning modules are also available on the Turbomeca Operator On-Line Support (TOOLS site) 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 OPEN DVD-ROM includes the Maintenance Program (PRE), the Maintenance Manual (MET), the Wiring Diagram Manual (MCS), the Description and Operation Manual (MDF), the Fault and Isolation Manual (MFI), the Storage and Preservation Manual (MST), the Repair Manual (MRR), the Standard Practices Manual (MTC) and the Illustrated Parts Catalogue (IPC). The component maintenance manual (CMM) is available on DVD-ROM or hard copy, depending on the Vendor. Along with the OPEN 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:

Télex 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.

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

E U R O C O P T E R

EC120 B

120 B 07.101.01 E

Technical Data