AS332L1 Technical Data

EUROCOPTER

AS332 L1

Technical Data

332 L1 07.101.02 E

EUROCOPTER

AS332 L1 Tech Te ch nic al Data Data

SUPER PUMA (Civil Version)

AS 332 C1 (MK1)

AS 332 L1 (MK1)

EC 225

COUGAR (Military Version)

Short version utility/armed

Naval version missiles/torpedoes

AS 532 AC (MK1)

AS 532 SC (MK1)

Stretched version utility/armed

Utility/armed version

AS 532 AL (MK1)

EC 725

Technical Data

Contents 1 - General characteristics characteristics ........... ............................... ............................... .........

3

2 - Standard Aircraft Definition ........................... ............................. ..................

6

3 - Optional equipment .......................... ............................. .............................. ..

9

4 - Table of Constraints ............................. .............................. ........................... 17 5 - Main performance ............................. .............................. .............................. . 31 6 - Customer Service Overview ............................ ............................... ............... 53

Manufacturers notice Attention ! EUROCOPTER, EUROCOPTER , its logo, SUPER PUMA, PUMA, AS332 L1 L1 are trade marks of the Eurocopter Group. EUROCOPTER’S policy is one of on-going product enhancement which means that alterations in definition, pictures, weights, dimensions or performance performance may be made at any time without notice notice being included in those documents that have already been issued. This document cannot thus be taken as an offer or serve as an appendix to a contract without a prior check as to its validity and prior written agreement of EUROCOPTER. The operational or certification regulations, as defined by the local authorities, can make compulsory the installation of some of the equipment and recommended solutions, listed in this document. This list does not claim to cover the whole of the worldwide operational requirements nor the equipment not specifically related to the helicopter (for example: life jacket) or necessary for particular missions (for example: supplemental oxygen). The operator is responsible for ascertaining with his local authorities that the planned configuration configuration of the helicopter helicopter complies with regulatory regulatory requirements requirements for the area(s) of operations and the type(s) of mission(s) considered.

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

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER EUROCOPTER - 2007

Technical Data

Blank

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

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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER - 2007

Technical Data

1- 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 % 

   

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

kg

lb

4,510

9,943

4,090 8,600 4,500 9,350

9,017 18,960 9,920 20,615

Power plant 2 Turbomeca Makila 1A1 turboshaft engines

Engine ratings Power per engine, in standard atmosphere, at sea level :    

Maximum emergency power Intermediate emergency power Take-off power Maximum continuous power

kW

ch

shp

1,400 1,330 1,357 1,185

1,902 1,807 1,845 1,610

1,877 1,783 1,819 1,588

US gal. 535

kg 1,595

lb 3,516

254 2 x 257 474 5 x 375

560 2 x 567 1,045 5 x 827

Usable Fuel capacities  

litres 2,020

Standard fuel tanks Auxiliary fuel tanks (option) Central fuel tank  External fuel tanks  Cabin fuel tank  1 to 5 ferrying fuel tanks 

321 2 x 326 600 5 x 475

85 2 x 86 158 5 x 126


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Technical Data

Main dimensions 18.70 m Rotor Rotating 61.35 ft φ 15.60 m

51.18 ft dia

φ 3.05 m

10.00 ft dia 4.60 m

4.92 m

15.09 ft

16.14 ft

5.25 m 17.22 ft

16.29 m 53.44 ft

3.38 m 11.08 ft 2.00 m 6.56 ft 2.12 m 6.95 ft

3.00 m 9.84 ft

Dimensions with blades folded

3.81 m 12.50 ft


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Technical Data

Dimensions of compartments and accesses

Cabin floor characteristics


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Technical Data

2-

Super Puma AS332 Puma AS332 L1 - Standard Aircraft Definition

GENERAL    

 





Crashworthy design fuselage including cockpit and cabin Monocoque tail boom boom with tail rotor protection and stabilizer Polyurethane white paint re-inforced anti-corrosive treatment Front part of the tail boom arranged as a luggage compartment Fuselage upper part used as transmission deck Fuselage lower lower part fittable with the floatation floatation gear and the the crashworthy installation (tanks) Engine cowlings serving as a work platform when in the open position Provisions for external pod fuel tanks





   

High energy absorption, retractable, tricycle landing gear with with trailing-arm main landing gear and castering nose wheel unit Footsteps for climbing to the transmission deck, the cockpit and the cabin Built-in jacking and towing points Provisions for attaching gripping points Interior paint : light beige Exterior paint : the fuselage is painted following customer customer paint scheme (gloss or dull polyurethane finish) ; the landing gears are grey and unless otherwise specified, the optional equipments keep their original colors.

COCKPIT 

         

2 pilot pilot and copilot seats adjustable in height and fore-and-aft, fore-and-aft, complete with safety belts and extensible shoulder harnesses 1 third crew man jump-seat with extensible safety belt. Dual flight control Steadying rods at pilot station Engine controls Master cut-off switches Rotor brake control Landing gear control Differential wheel brakes at pilot and copilot stations 2 map cases on pilot and copilot doors 1 Flight Manual

         

1 ash-tray 1 hand fire extinguisher De-iced pilot and copilot windshield panes with wiper Adjustable front ventilation system Heating and ventilation diffusers Windshield demisting diffusers 2 adjustable heating and ventilation outlets Manual cock for selective pane demisting 2 jettisonable doors with door-stops Access to cabin with partitioning curtain

INSTRUMENTS        

       

2 airspeed indicators 2 rate-of-climb indicators 2 altimeters 2 stop watches 3 gyro-horizons 1 pitch indicator 1 stand-by magnetic compass 2 SFIM CG 130 gyro compasses associated with 2 Astronautics 5" HSI/RMI 1 thermometer 2 torquemeter indicators 2 fuel pressure indicators 2 hydraulic pressure indicators (left and right) 1 auxiliary electropump hydraulic pressure indicator 1 MGB oil pressure indicator 1 MGB oil temperature indicator 1 MGB stand-by circuit oil pressure indicator

                 

1 IGB oil temperature indicator 1 TGB oil temperature indicator 2 T4 temperature indicators 2 gas generator tachometers 2 dual engine oil pressure and temperature indicators 1 self-contained rotor tachometer 1 rotor rotor and free turbines turbines 1 and 2 triple tachometer tachometer 1 warning panel 1 autopilot control box 1 fuel circuit control control and monitoring panel 2 fuel gauges 1 dual DC indicator 1 dual AC indicator 1 engine starting panel 1 landing gear position control and monitoring panel 2 heated pitot heads and 4 static vents 1 ventilation/heating system control panel Instruments units available in English units (Altimeter in feet and Airspeed indicator in kts); other units on request

CABIN 

 

 

Floor fitted with 15 cargo tie-down rings, capable of accommodating various types of seat and cabin additional fuel tanks available on option 2 jettisonable sliding plug doors 12 jettisonable jettisonable windows (including 4 in the sliding doors) for emergency exit 1 removable rear panel with jettisonable window 1 hand fire extinguisher, 1 axe and anti-smoke equipment

 

  

Soundproofing upholstery (light beige padded cloth) Heating and and ventilation (12 upper outlets adjustable for direction and flow, plus 4 lower bottoms adjustable for flow) with evacuation of stale air (2 outlets) Fittings for ambulance equipment, fixed parts 6 stretchers Floor hatch for cargo sling pole Stowage space for airborne kit


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Technical Data POWER PLANT 





2 Turbomeca Turbomeca Makila Makila 1A1 1,902 ch (1,877 shp) turbine engines in two separate groups groups with own starting, feeding, lubricating, cooling and governing systems 1 fuel system of of 2,020 litres (535 US gal.) usable capacity comprising 6 tanks, arranged in 2 groups, 4 booster pumps, 1 transfer pump and a low/high fuel level warning system. The pipes are of the crashworthy type Provisions for ferrying, central auxiliary and external tanks

   

 

2 engine bay fire-detection systems 1 two-cylinder selective fire-extinguishing system 2 engine chip detectors Engine air intakes protected against icing by grids and heating mats on the air intake stub frames 1 engine flushing device without removal of cowlings N.G. limiter for training

TRANSMISSION SYSTEM 



1 main gearbox (MGB) on flexible mountings with chip detector with fuzz burner, oil sight gauge, oil temperature and pressure sensors and torquemeter pick-ups 2 lubrication pumps and independant circuits 1 intermediate intermediate gearbox with magnetic plug, oil sight gauge and temperature sensor



  

1 tail gearbox (TGB) with magnetic plug, oil sight gauge and and temperature sensor 1 MGB oil cooling system 1 rotor brake 2 MGB bay fire detection circuits

ROTORS AND FLYING CONTROLS 

 

1 main rotor with 4 composite-material blades equipped with with gust and droop stops 1 anti-torque rotor with 5 composite-material blades 1 flying control system, fitted with 4 dual-body servo-units (3 on the cyclic and collective pitch channels and 1 on the antitorque rotor pitch control channel) with 2 chambers per body



1 duplex autopilot autopilot associated with two SFIM GV 76-2 vertical gyro units and one baroanemometric module

ELECTRICAL INSTALLATION      

2 alternators (20/30 kVA, 115/200 V, 400 Hz) 1 cadmium-nickel battery (43 amp.-hr) 2 transformer-rectifiers (150 amp.) 1 stand-by battery 2 transformers (26 V, 400 Hz) 1 cockpit lighting system including : white/blue pedestal instrument and overhead panel  lighting (normal/stand-by) red or white general lighting  1 red and white extension light  2 white map lights 



     

1 cabin lighting system made up of two-lighting strips, plus signs : "Emergency Exit", "No Smoking" and "Fasten seat Belts" 6 receptacles for ancillaries (28 V, 15 amp.) 1 receptacle for ancillaries (28 V, 25 amp.) 2 external power receptacles (AC and DC) 1 landing light (600 W) 3 position lights 1 anti-collision light

HYDRAULIC GENERATION 



2 independent hydraulic systems : the LH system feeds one of the servo-unit bodies, the  autopilot, the landing gear control, the rotor brake and wheel brakes  the RH system feeds feeds the other body of the servo-units Hydraulic ground couplings





1 DC auxiliary electropump electropump on stand-by for for the LH system and for supplying sufficient hydraulic pressure for movement of the controls on the ground before starting in high winds 1 stand-by electropump electropump for complete lowering of the landing gear

AIRBORNE KIT (*)       

(*)

4 static vent blanks 3 pitot head covers 1 engine air-intake grid protection cover 2 engine tail-pipe blanks 4 mooring rings 2 rough-weather mooring fittings (included on the aircraft) 1 access ladder

     

1 data case 3 jacking ball-joints Main blade tie-down Tail rotor blade lock Fuel bleed line 1 stowing bag for the airborne kit

(weight not included in standard aircraft empty weight) The data set forth in this document are general in nature and for information purposes only. They may vary with conditions. For performance performance data and operating operating limitations,reference limitations,reference must be made made to the approved flight flight manual and all all appropriate appropriate documents.

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Technical Data

Blank


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Technical Data

3- Optional equipment Symbol

shown beside an item denotes some constraint (see table on page 17)

Note : value of the weight breakdown is given for information and shall no t be considered as contractual. Document reference

Name

Commercial reference

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 p lug-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 in dicator (ex-Rosemount)

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

05-67020-A

05-67020-00-CI

Power socket 12 VDC for electronic devices

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 2

Mounted in production-line instead of the standard air intakes. Instead of the 20/30 kVA standard ones. The data set forth in this document are general in nature and for information purposes only. They may vary with conditions. For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data Document reference

Name


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

05-81026-A

05-81026-00-RP Additional crashworthy pod fuel tanks - Removable parts

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

05-82023-A

05-82023-00-CI

Fuel jettison system

9.0

19.8

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

15.0

33.1

103.0

227.0

45.0

99.2

On Request On Request

Specific mission equipment 06-20002-A

06-20002-00-FP

Double hoist installation - Fixed Parts

06-20002-A

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

06-20002-A

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

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

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Technical Data 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 1

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 2

23.9

52.7

06-31017-A

06-31017-00-FP

Hailer installation (Qty 1) - Fixed Parts

On Request

06-31017-A

06-31017-00-RP

Hailer installation (Qty 1) - Removable Parts

On Request

06-42010-A

06-42010-00-CI

Second landing light 3

5.0

11.0

06-42023-A

06-42023-00-CI

Fixed lights in maritime sponsons 3

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 3

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 f ire 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 4

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

06-70007-A

06-70007-00-CI

NVG compatible cockpit lighting

3.9

8.6

06-81006-A

06-81006-00-CI

Fire Fighting "Bambi Bucket" installation

435.0

959.0

06-81022-A

06-81022-00-CI

Fire fighting kit (up to 3000 liters)

382.0

842.0

1

2 3 4

The 3 metric ton cargo sling fixed parts incl ude : The whole 4.5 metric ton cargo sling fixed parts. One supplement for 3 metric ton cargo sling specific fixed parts. The customer choosing the 3 metric ton cargo sling has then automatically the 4.5 metric ton cargo sling fixed parts. Requires to remove the central auxiliary fuel tank if it has been selected by the user. Required for JAR OPS 3. Acceptance by local airworthiness authorities to be checked. The data set forth in this document are general in nature and for information purposes only. They may vary with conditions. For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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Technical Data Name


Document reference

kg

lb

Interior layout 07-10003-A

07-10003-00-CI

Pilot and copilot Airline seats comfort type

12.4

27.3

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

07-30011-A

07-30011-00-CI

Airline upholstery with improved sound proofing

07-50013-A

07-50013-00-CI

Special RH double door

07-50015-A

07-50015-00-CI

Special LH door with built-in steps

07-50021-A

07-50021-00-CI

Rear built-in step door 2

07-60003-A

07-60003-00-CI

07-60004-A

On Request 157.0

346.1

7.0

15.4

15.0

33.1

8.3

18.3

Enlarged luggage hold with 1 special step door with bench seat integrated in cabin bulkhead

48.6

107.1

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)

28.9

63.7

07-74010-A

07-74010-00-CI

Stretcher (NATO type) (loose equipment delivered separately)

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

On Request

07-80012-A

07-80012-00-CI


On Request

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

1 2

2.0

4.4

Installation including 17 comfort seats and the cushions of the 3 bench seats integrated in the cabin bulkhead. Recommended in VIP configuration. 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 07.101.02 E

12 ®

®


Technical Data

Various Possibilities of the AS332 L1 Cabin Installation

Corporate VIP

Passenger transport Crew change

10 seats VIP or

g n i t a e S

19 comfort seats

19 comfort places

11 seats VIP or

12 seats VIP

Standard r a e R

Luggage hold with bench seat

Standard upholstery

or

or

Luggage hold without bench seat

Rear built-in step door

Airline upholstery

VIP upholstery

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

Standard sliding doors

and Special RH double door


332 L1 07.101.02 E

13 ®

®



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 Team - TB31 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 Team - TB31 ICS - Basic set : 3 control panels CP 1976 in cockpit Team - TB31 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.


332 L1 07.101.02 E

14 ®

®




Name

kg

lb

Possible add-ons depending on mission needs 08-10002-A

08-10002-00-CI Collins - HF 9X00 - HF/SSB

08-12024-A

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

08-15515-A

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

08-16032-A

08-16032-00-CI Team TB31 ICS - Complementary set : 4th control p anel CP 1976

08-17002-A

08-17002-00-CI Baker - M1060 - Passenger address

08-17004-A

24.3

53.6

5.0

11.0

On Request 3.1

6.8

25.0

55.1

08-17004-00-CI Multimedia Player

6.4

14.1

08-17012-A

08-17012-00-CI Team - BA1920 - Passenger Interphone

1.6

3.5

08-18005-A

08-18005-00-CI Optique Scientifique - FPH 600 helmet

1.3

2.9

08-18008-A

08-18008-00-CI Silec 4452 - Headset

0.5

1.1

08-18019-A

08-18019-00-CI Silec 4449-1 - 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 2 3 4

Delivered with EUROPE map. Subscription to be made by the c ustomer. Compatible with JAR OPS-3 regulation. The toolings of the installation are not included in the price. At least one ground station per helicopter base must be purchaded. 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 07.101.02 E

15 ®

®


Technical Data

Blank


332 L1 07.101.02 E

16 ®

®


Technical Data

4- Table of Constraints Note :

This table only indicates the major compatibility restrictions between some usual installations. It is presented for information and as examples only. For a complete formal status of compatibility restrictions, the customized configuration must be built an submitted to Eurocopter for a precise check .

EXL Impossibility of simultaneous fitment of the fixed parts of 2 items of equipment NSF Total or partial incompatibility of simultaneous fitment of the removal parts of two items of equipment NSU Possibility of simultaneous fitment on the same aircraft, but impossible to use simultaneously REQ Requires the fitting of

Document Reference

00-10021-A

Commercial Reference

Installation

Nature of the Constraint L F U Q X S S E E N N R

00-10021-00-CI AS 332 L1 Standard Aircraft

X


08-00017-01-C I

or

05-01010-A

05-01010-00-CI

CAA kit

Wire strike protection system Removable parts

Civil Use minimum items of equipment (VFR/IFR dual pilot)

Document Reference

08-00017-B

or

or

X

08-00018-02-C I

Search & Rescue minimum items of equipment (VFR/IFR dual pilot)

08-00018-C

X

05-51002-00-C I


05-51002-A

X

06-42010-00-C I

Second landing light

06-42010-A

or

05-21012-A 05-21012-00-RP

Installation

or

or

X

06-42023-00-C I

Fixed lights in maritime sponsons

06-42023-A

X

06-66003-00-C I

Helicopter Emergency Egress Lighting (HEEL)

06-66003-A

X

06-69001-00-C I

X

08-83006-00-C I

EUROHUMS

08-83006-A

X

05-21012-00-FP

Wire strike protection system - Fixed parts

05-21012-A

Automatic Voice Alarm Device (AVAD) 06-69001-A

05-25012-A

05-25012-00-CI

Main rotor blades re-inforced sanderosion protection strip (loose equipment, delivered uninstalled)

X

05-50004-00-CI


05-50004-A

05-25013-A

05-25013-00-CI

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

X

05-50004-00-CI


05-50004-A

05-31017-A

05-31017-00-CI


X

05-31018-00-CI


05-31018-A

05-31018-A

05-31018-00-CI


X

05-31017-00-CI


05-31017-A

05-31020-A

05-31020-00-CI


X

05-31022-00-CI


05-31022-A

05-31022-A

05-31022-00-CI


X

05-31020-00-CI


05-31020-A

05-42009-A

05-42009-00-CI Air conditioning system with pod mounted

X

05-42009-01-CI

unit (to be used with Airline-type sound proofing) X

05-62008-00-C I

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

Two 30/40 kVA alternators and 2nd electrical box

05-62008-A


332 L1 07.101.02 E

17 ®

®


Technical Data Document Reference

05-42009-A


Installation

05-42009-01-CI Air conditioning system with pod mounted


X


05-42009-00-CI

unit (to be used with VIP-type sound proofing)

05-50004-A

05-50006-A

05-67020-A

05-50004-00-CI

05-50006-00-CI

05-67020-00-CI


05-62008-A

X

05-22009-00-C I

Multipurpose engine air intakes (stretched version)

05-22009-A

X

05-25012-00-CI

Main rotor blades re-inforced sanderosion protection strip (loose equipment, delivered uninstalled)

05-25012-A

X

05-25013-00-CI

Tail rotor blades re-inforced sanderosion protection strip (loose equipment, delivered uninstalled)

05-25013-A

X

05-51002-00-C I


05-51002-A

X

05-52004-00-C I

Goodrich icing severity indicator

05-52004-A

X

05-62008-00-C I


05-62008-A

X

08-31001-00-C I

Telephonics 1400 C Weather Radar, with beacon mode

08-31001-A

X

05-51002-00-C I


05-51002-A

X

05-52004-00-C I

Goodrich icing severity indicator

05-52004-A

X

08-31001-00-C I

Telephonics 1400 C Weather Radar, with beacon mode

08-31001-A

X

07-25020-00-CI

19 comfort places with 3-place rear bench seat

07-25020-A

X

07-25022-00-CI

19 comfort seats installation without 3place rear bench seat

07-25022-A

07-30009-00-C I


07-30009-A

Kit for flight in limited icing conditions

X

07-30011-00-CI

07-50013-00-C I


07-50013-A

X

07-50015-00-C I


07-50015-A

X

07-60003-00-CI


07-60003-A

X

07-60004-00-CI


07-60004-A

07-80004-00-C I


07-80004-A

or

X

07-80005-00-C I or

X


Airline upholstery with improved sound 07-30011-A proofing

X

X

05-81010-00-CI

05-42009-A

05-62008-00-C I

X

05-81010-A

Air conditioning system with pod mounted unit (to be used with Airlinetype sound proofing)

Document Reference

X


Power socket 12 VDC for electronic devices

Installation

X

X

or

or

VIP 10 + 2 seats with galley and toilet

07-80005-A

or

or

07-80012-00-C I


07-80012-A

05-81022-00-CI


05-81022-A

06-27017-00-RP

Cargo sling with dynamometer (4.5 metric tons) - Removable parts

06-27017-A


332 L1 07.101.02 E

18 ®

®




05-81011-A

05-81011-00-CI

05-81022-A

05-81022-00-CI

Installation

Crashworthy external additional fuel tanks 2x318 l (2x84 US gal)



05-81026-A

05-81024-00-CI

External additional fuel tanks 2x326 l (2x86 US gal)

05-81026-00-FP Additional crashworthy pod fuel tanks -

Installation

Document Reference

X

05-81024-00-CI


05-81024-A

X

05-82013-00-CI

Pressure refuelling on the ground usable with maritime sponsons and floatation

05-82013-A

X

05-82014-00-CI


05-82014-A

X

06-60003-00-CI

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

06-60003-A

X

06-61012-00-CI


06-61012-A

X

05-81010-00-CI


05-81010-A

06-27017-00-RP


06-27017-A

X

05-81011-00-CI


05-81011-A

X

05-82013-00-CI

Pressure refuelling on the ground usable with maritime sponsons and floatation

05-82013-A

X

05-82014-00-CI


05-82014-A

X

06-60003-00-CI


06-60003-A

X

06-61012-00-CI


06-61012-A

X

06-31017-00-FP


06-31017-A

X

06-31017-00-RP


06-31017-A

X

06-45014-00-FP


06-45014-A

X

06-45014-00-RP

Search light Spectrolab SX 16 Removable parts

06-45014-A

X

05-81024-A


Fixed parts

05-81026-A 05-81026-00-RP

Additional crashworthy pod fuel tanks Removable parts

X

05-81026-00-FP

05-82012-A

Pressure refuelling on the ground usable with additional external tanks, and jettisonable plug-in cabin door

X

05-81011-00-C I

05-82012-00-CI

or

X

Additional crashworthy pod fuel tanks - 05-81026-A Fixed parts Crashworthy external additional fuel tanks 2x318 l (2x84 US gal)

05-81011-A

or

or

05-81024-00-C I


05-81024-A

X

05-82013-00-CI


05-82013-A

X

05-82014-00-CI


05-82014-A

X

06-60003-00-CI


06-60003-A


332 L1 07.101.02 E

19 ®

®



05-82013-A


05-82013-00-CI

Installation



05-82014-00-CI

05-84006-A 05-84006-00-RP


05-84007-00-CI

Document Reference

06-61012-00-CI


06-61012-A

X

05-81011-00-CI


05-81011-A

X

05-81024-00-CI


05-81024-A

X

05-82012-00-CI


05-82012-A

X

05-82014-00-CI


05-82014-A

06-61012-00-C I

Emergency floatation gear usable without external fuel tanks

06-61012-A

X

06-61014-00-FP

Emergency floatation gear usable with external fuel tanks - Fixed Parts

06-61014-A

X

05-81011-00-CI


05-81011-A

X

05-81024-00-CI


05-81024-A

X

05-82012-00-CI


05-82012-A

X

05-82013-00-CI


05-82013-A

X

06-60003-00-CI


06-60003-A

X

06-61012-00-CI


06-61012-A

X

06-61014-00-FP


06-61014-A

06-25003-00-CI

Drip tub

06-25003-A

X

07-30009-00-CI


07-30009-A

X

07-30011-00-CI

X


X

05-84007-A

Installation

X

X

05-82014-A



07-71014-00-CI


07-71014-A

X

07-80004-00-CI


07-80004-A

X

07-80005-00-CI


07-80005-A

X

07-80012-00-CI


07-80012-A

06-25003-00-CI

Drip tub

06-25003-A

X

07-30009-00-CI


07-30009-A

X

07-30011-00-CI

X




332 L1 07.101.02 E

20 ®

®




Installation


06-20002-A

06-20002-00-FP

06-20002-A 06-20002-00-RP1

06-20002-A 06-20002-00-RP2

06-21012-A

06-21012-00-FP


07-60003-A

X

07-60004-00-CI


07-60004-A

07-71014-00-CI


07-71014-A

X

07-80004-00-CI


07-80004-A

X

07-80005-00-CI


07-80005-A

X

07-80012-00-CI


07-80012-A

05-92005-00-FP

Main rotor blade folding system - Fixed 05-92005-A Parts

X

06-21012-00-FP

Hydraulic hoist with variable speed 75 meter cable, 272kg (246ft, 600lb) Fixed parts

06-21012-A

X

06-21024-00-FP


06-21024-A

06-20002-00-FP


06-20002-A

X

06-27015-00-RP


06-27015-A

X

06-27017-00-RP


06-27017-A

X

08-16032-00-C I

Team TB31 ICS - Complementary set : 08-16032-A 4th control panel CP 1976

X

06-20002-00-RP1

Double hoist installation - Removable Parts (Main Hoist & Beam)

06-20002-A

X

06-20002-00-FP


06-20002-A

X

06-21024-00-FP


06-21024-A

06-21012-A 06-21012-00-RP

06-21012-00-FP


06-21012-A

X

06-27015-00-RP


06-27015-A

X

06-27017-00-RP


06-27017-A

08-16032-00-C I


X

06-20002-00-FP


06-20002-A

X

06-21012-00-FP


06-21012-A

06-21024-00-FP


06-21024-A

06-27015-00-RP


06-27015-A

X

X


Double hoist installation - Removable Parts (Backup Hoist) Hydraulic hoist with variable speed 75 meter cable, 272kg (246ft, 600lb) - Fixed parts

X

Hydraulic hoist with variable speed 75 meter cable, 272kg (246ft, 600lb) Removable parts

X

06-21024-A

06-21024-00-FP

06-21024-A 06-21024-00-RP


Document Reference

07-60003-00-CI

Main rotor blade folding system Removable Parts Double hoist installation - Fixed Parts

Installation

X

X

05-92005-A 05-92005-00-RP


X

Goodrich 28V electrical hoist (290ft, 600lb) - Removable parts X


332 L1 07.101.02 E

21 ®

®




Installation


X

06-25003-00-CI


X

06-27017-00-RP


06-27017-A

X

07-25020-00-CI


07-25020-A

X

07-25022-00-CI


07-25022-A

07-50015-00-CI


07-50015-A

07-71014-00-CI


07-71014-A

X

07-80004-00-CI


07-80004-A

X

07-80005-00-CI


07-80005-A

X

07-80012-00-CI


07-80012-A

X

06-61012-00-CI


06-61012-A

X

06-61014-00-RP

Emergency floatation gear, usable with external fuel tanks - Removable parts

06-61014-A

X

06-20002-00-RP1


06-20002-A

X

06-21012-00-RP


06-21012-A

X

06-21024-00-RP


06-21024-A

06-27015-00-FP

Cargo sling with dynamometer (3 metric tons) - Fixed parts

06-27015-A

06-27017-00-RP


06-27017-A

08-27021-00-CI

Chelton DF931-6 V/UHF DF

08-27021-A

X

05-81010-00-CI


05-81010-A

X

05-81022-00-CI


05-81022-A

Drip tub



X

X

X 06-27017-A 06-27017-00-RP


06-27017-A

08-16032-00-C I

X

06-27015-A 06-27015-00-RP

Document Reference


X

06-26005-A 06-26005-00-CI

Installation

06-27017-00-RP

X

06-25003-A


X

06-20002-00-RP1


06-20002-A

X

06-21012-00-RP


06-21012-A

X

06-21024-00-RP


06-21024-A

06-27015-00-RP


06-27015-A

06-27017-00-FP

Cargo sling with dynamometer (4.5 metric tons) - Fixed parts

06-27017-A

07-25020-00-CI


07-25020-A

X

X

X


332 L1 07.101.02 E

22 ®

®



06-31017-A


06-31017-00-FP

Installation


06-31017-A 06-31017-00-RP


06-45014-A 06-45014-00-FP


06-45014-A 06-45014-00-RP

06-60003-A

06-60003-00-CI



07-25022-A

X

07-71014-00-CI


07-71014-A

X

07-80004-00-CI


07-80004-A

X

07-80005-00-CI


07-80005-A

X

07-80012-00-CI


07-80012-A

X

08-27021-00-CI

Chelton DF931-6 V/UHF DF

08-27021-A

X

05-81026-00-FP

Additional crashworthy pod fuel tanks - 05-81026-A Fixed parts

X

05-81026-00-RP

Additional crashworthy pod fuel tanks - 05-81026-A Removable parts

X

06-31017-00-FP


06-31017-A

X

05-81026-00-FP

Additional crashworthy pod fuel tanks - 05-81026-A Fixed parts

X

05-81026-00-RP

Additional crashworthy pod fuel tanks - 05-81026-A Removable parts

X

06-45014-00-FP


06-45014-A

X

05-81011-00-CI


05-81011-A

X

05-81024-00-CI


05-81024-A

X

05-82012-00-CI


05-82012-A

X

05-82014-00-CI


05-82014-A

X

06-61014-00-FP


06-61014-A

06-61012-00-C I


06-61012-A

07-50015-00-CI


07-50015-A

05-26005-00-C I


05-26005-A

X

05-81011-00-CI


05-81011-A

X

05-81024-00-CI


05-81024-A

X

05-82012-00-CI


05-82012-A

X

05-82014-00-CI


05-82014-A

06-26005-00-CI


06-26005-A

06-61014-00-FP


06-61014-A

X 06-61012-00-CI

Document Reference

07-25022-00-CI

X

06-61012-A

Installation

X

Search light Spectrolab SX 16 Removable parts 2 AERAZUR SR14 self-righting life rafts (with jettison control in cockpit and survival aid kits) in the sponsons


X


X

X


332 L1 07.101.02 E

23 ®

®




06-61014-A

06-61014-00-FP

Installation


Emergency floatation gear, usable with external fuel tanks - Fixed parts


Document Reference

X

05-26005-00-C I


05-26005-A

X

05-81011-00-C I


05-81011-A

or

X

06-61014-A 06-61014-00-RP

Installation

or

or

05-81024-00-C I


05-81024-A

X

05-82013-00-CI


05-82013-A

X

05-82014-00-CI


05-82014-A

X

06-60003-00-CI


06-60003-A

X

06-61012-00-CI


06-61012-A

06-26005-00-CI


06-26005-A

06-61014-00-FP

Emergency floatation gear, usable with external fuel tanks - Fixed parts

06-61014-A

X

Emergency floatation gear, usable with external fuel tanks - Removable parts

X

07-10003-A

07-10003-00-CI


X

07-10006-00-CI


07-10006-A

07-10006-A

07-10006-00-CI


X

07-10003-00-CI


07-10003-A

07-25020-A

07-25020-00-CI


06-25003-00-CI

Drip tub

06-25003-A

X

07-25022-00-CI


07-25022-A

X

07-30009-00-CI


07-30009-A

07-60003-00-C I


07-60003-A

X

07-60004-00-CI


07-60004-A

X

07-80004-00-CI


07-80004-A

X

07-80005-00-CI


07-80005-A

X

07-80012-00-CI


07-80012-A

06-25003-00-CI

Drip tub

06-25003-A

X

07-25020-00-CI


07-25020-A

X

07-30009-00-CI


07-30009-A

X

07-60003-00-CI


07-60003-A

X

07-80004-00-CI


07-80004-A

X

X

07-25022-A

07-25022-00-CI

X



332 L1 07.101.02 E

24 ®

®



07-30009-A


07-30009-00-CI

Installation




07-80005-00-CI


07-80005-A

X

07-80012-00-CI


07-80012-A

X

05-84006-00-RP


05-84006-A

X

05-84007-00-CI


05-84007-A

X

06-27017-00-RP


06-27017-A

X

07-25020-00-CI


07-25020-A

X

07-25022-00-CI


07-25022-A

X

07-30011-00-CI


X

07-50013-00-C I


07-50013-A

X

07-50015-00-C I


07-50015-A

X

07-60003-00-CI


07-60003-A

X

07-60004-00-CI


07-60004-A

X

07-71014-00-CI


07-71014-A

07-80004-00-C I


07-80004-A

or

X

07-80005-00-C I or

X 07-30011-00-CI Airline upholstery with improved sound

Document Reference

X

X

07-30011-A

Installation

or

or


07-80005-A

or

or

07-80012-00-C I


07-80012-A

X

05-84006-00-RP


05-84006-A

X

05-84007-00-CI


05-84007-A

X

07-30009-00-CI


07-30009-A

X

07-50013-00-CI


07-50013-A

X

07-50015-00-CI


07-50015-A

07-60003-00-C I


07-60003-A

proofing

X

or

X

or

or

07-60004-00-C I


07-60004-A

X

07-71014-00-CI


07-71014-A

X

07-80004-00-CI


07-80004-A

X

07-80005-00-CI


07-80005-A


332 L1 07.101.02 E

25 ®

®




Installation


X 07-50013-A

07-50013-00-CI

X

Special RH double door X

07-50015-A

07-50015-00-CI

X


07-60004-A

07-71014-A

07-80004-A

07-60003-00-CI

07-60004-00-CI

07-71014-00-CI

07-80004-00-CI



Document Reference


07-80012-A

07-30009-00-C I


07-30009-A


06-60003-00-CI


06-60003-A

07-30009-00-C I


07-30009-A

X

07-30011-00-CI

X

07-25022-00-CI


07-25022-A

X

07-30009-00-CI


07-30009-A

X

07-80004-00-CI


07-80004-A

X

07-80005-00-CI


07-80005-A

X

07-80012-00-CI


07-80012-A

X

07-25020-00-CI


07-25020-A

X

07-30009-00-CI


07-30009-A

X

07-80004-00-CI


07-80004-A

X

07-80005-00-CI


07-80005-A

X

07-80012-00-CI


07-80012-A

X

06-25003-00-CI

Drip tub

06-25003-A

X

06-27017-00-RP


06-27017-A

X

07-30009-00-CI


07-30009-A

X

07-30011-00-CI

X

07-25020-00-CI


07-25020-A

X

07-25022-00-CI


07-25022-A

07-30009-00-C I


07-30009-A



Installation

07-80012-00-CI

07-30011-00-CI

X

07-60003-A


X

X

07-30011-00-CI




X

07-50013-00-C I


07-50013-A

X

07-50015-00-C I


07-50015-A

X

07-50021-00-C I


07-50021-A


332 L1 07.101.02 E

26 ®

®



07-80005-A


07-80005-00-CI

Installation




Document Reference

07-60003-00-CI


07-60003-A

X

07-60004-00-CI


07-60004-A

X

07-80005-00-CI


07-80005-A

X

07-80012-00-CI


07-80012-A

X

07-25020-00-CI


07-25020-A

X

07-25022-00-CI


07-25022-A

07-30009-00-C I


07-30009-A

X

07-80012-00-CI

Installation

X

X

07-80012-A


07-30011-00-CI


X

07-50013-00-C I


07-50013-A

X

07-50015-00-C I


07-50015-A

X

07-50021-00-C I


07-50021-A

X

07-60003-00-CI


07-60003-A

X

07-60004-00-CI


07-60004-A

X

07-80004-00-CI


07-80004-A

X

07-80012-00-CI


07-80012-A

X

07-25020-00-CI


07-25020-A

X

07-25022-00-CI


07-25022-A

07-30009-00-C I


07-30009-A

X

X

07-30011-00-CI


X

07-50013-00-C I


07-50013-A

X

07-50015-00-C I


07-50015-A

X

07-50021-00-C I


07-50021-A

X

07-60003-00-CI


07-60003-A

X

07-60004-00-CI


07-60004-A

X

07-80004-00-CI


07-80004-A

X

07-80005-00-CI


07-80005-A


332 L1 07.101.02 E

27 ®

®




07-82008-A

07-82008-00-CI

Installation

Retractable armrests



07-25020-00-CI


07-25020-A

X

07-25022-00-CI


07-25022-A

07-30009-00-C I


07-30009-A

X

07-30011-00-CI

07-50013-00-C I


07-50013-A

X

07-50015-00-C I


07-50015-A

X

07-60003-00-CI


07-60003-A

X

07-60004-00-CI


07-60004-A

07-80004-00-C I


07-80004-A

or

X

07-80005-00-C I or

X

Lombar adjustment


07-80005-A

or

or 07-80012-A

X

07-25020-00-CI


07-25020-A

X

07-25022-00-CI


07-25022-A

07-30009-00-C I


07-30009-A

07-30011-00-CI


X

07-50013-00-C I


07-50013-A

X

07-50015-00-C I


07-50015-A

X

07-60003-00-CI


07-60003-A

X

07-60004-00-CI


07-60004-A

07-80004-00-C I


07-80004-A

X

or

X

07-80005-00-C I or

X

Electric curtains

or


X

07-83001-00-CI

or

07-80012-00-C I

X

07-83001-A


X

X

07-82009-00-CI

Document Reference

X

X

07-82009-A

Installation

or

or


07-80005-A

or

or

07-80012-00-C I


07-80012-A

X

07-25020-00-CI


07-25020-A

X

07-25022-00-CI


07-25022-A

07-30009-00-C I


07-30009-A

X


332 L1 07.101.02 E

28 ®

®




Installation


X


07-30011-00-CI


07-50013-A

X

07-50015-00-C I


07-50015-A

X

07-60003-00-CI


07-60003-A

X

07-60004-00-CI


07-60004-A

07-80004-00-C I


07-80004-A

X

07-80005-00-C I or

X

Customized inlaid wood table


07-80005-A

or

or 07-80012-A

X

07-25020-00-CI


07-25020-A

X

07-25022-00-CI


07-25022-A

07-30009-00-C I


07-30009-A

07-30011-00-CI


X

07-50013-00-C I


07-50013-A

X

07-50015-00-C I


07-50015-A

X

07-60003-00-CI


07-60003-A

X

07-60004-00-CI


07-60004-A

07-80004-00-C I


07-80004-A

X

or

X

07-80005-00-C I or

X

Transparent central partition with storage compartment

or


X

07-85007-00-CI

or

07-80012-00-C I

X

07-85007-A


07-50013-00-C I

or

07-84003-00-CI

Document Reference

X

X

07-84003-A

Installation

or

or


07-80005-A

or

or

07-80012-00-C I


07-80012-A

X

07-25020-00-CI


07-25020-A

X

07-25022-00-CI


07-25022-A

07-30009-00-C I


07-30009-A

X

X

07-30011-00-CI


X

07-50013-00-C I


07-50013-A

X

07-50015-00-C I


07-50015-A


332 L1 07.101.02 E

29 ®

®




Installation



07-60003-00-CI


07-60003-A

X

07-60004-00-CI


07-60004-A

07-80004-00-C I


07-80004-A

or

X

07-80005-00-C I or

X 07-91001-00-CI

Gold finishing of cabin visible metallic parts

07-25020-A

X

07-25022-00-CI


07-25022-A

07-30009-00-C I


07-30009-A

07-30011-00-CI

07-50013-00-C I


07-50013-A

X

07-50015-00-C I


07-50015-A

X

07-60003-00-CI


07-60003-A

X

07-60004-00-CI


07-60004-A

07-80004-00-C I


07-80004-A

07-80005-00-C I

or

or


07-80005-A

or

or

07-80012-00-C I


07-80012-A

06-27015-00-RP


06-27015-A

06-27017-00-FP

Cargo sling with dynamometer (4.5 metric tons) - Fixed parts

06-27017-A

X

08-83006-00-CI

EUROHUMS

08-83006-A

X

08-81014-00-CI

X

Chelton DF931-6 V/UHF DF X

EUROHUMS


X

X

08-83006-00-CI

or


or

08-83006-A

or

07-25020-00-CI

X

Allied Signal CVFDR

07-80005-A

X

or

08-81014-00-CI


07-80012-A

X

08-81014-A

or


X

08-27021-00-CI

or

07-80012-00-C I

X

08-27021-A

Document Reference

X

X

07-91001-A

Installation

Allied Signal CVFDR

08-81014-A


332 L1 07.101.02 E

30 ®

®


Technical Data

5- 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 

Max. speed, VNE



Maximum cruise speed



Recommended cruise speed



Fuel consumption at recommended cruise speed



Fuel consumption at 70 kts



Rate-of-climb at 70 kts





8,000 17,630 298 161 278 150 258 139 497 1,096 374 825 9.8 1,920

8,600 18,960 278 150 262 141 252 136 502 1,107 389 858 8.2 1,618

m ft m ft

6,500 21,325 5,850 19,193

5,100 16,732 4,450 14,560

3,950 12,959 3,200 10,499

3,250 10,663 2,300 7,546

m ft m ft

5,750 18,865 5,200 17,060

4,300 14,108 3,550 11,647

3,050 10,007 2,100 6,890

2,300 7,546 1,400 4,593

m ft m ft

7,200 23,622 6,500 21,325

5,900 19,357 5,100 16,732

4,650 15,255 3,800 12,467

>2,895 >9,500 2,895 >9,500

km nm km n.m km n.m. km n.m. km n.m. km n.m.

736 397 664 358 724 391 652 352 624 337 592 319

879 474 1148 620 1021 551 1192 644 1164 628 1132 611

859 464 1127 609 1000 540 1267 684 1528 825 1662 897

841 454 1105 596 979 529 1105 597 1105 597 1976 1067

ISA + 20°C

ISA + 20°C

Service ceiling Vz = 150 ft/min ISA  



7,000 15,430 303 164 281 152 262 141 486 1,071 353 778 12.1 2,382

Hover ceiling OGE at take-off power ISA  



6,000 13,230 304 164 283 153 265 143 481 1,060 335 739 14.7 2,894

Hover ceiling IGE (10ft) at take-off power  ISA 



kg lb km/hr kts km/hr kts km/hr kts kg/hr lb/hr kg/hr lb/hr m/sec. ft/min.

ISA + 20°C

Maximum range (without fuel reserve, at recommended cruise s peed) with standard fuel tanks  

with external fuel tanks



with central auxiliary fuel tank



with external and central auxiliary fuel tanks



with external, central and cabin fuel tanks



with external, central and 5 ferrying tanks

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


332 L1 07.101.02 E

31 ®

®


Technical Data

Performance in external load (maximum gross-weight of 9,350 kg – 20,615 lb) 

Rate of climb at 9,350 kg



Hover ceiling OGE at take-off power

6.4 m/sec 1,260 ft/min



ISA

650 m 2,133 ft



ISA + 10°C

300 m 984 ft



ISA + 17°C

Sea level

Performance on 1 engine kg lb

Gross Weight 







6,000 13,230

7,000 15,430

8,000 17,630

8,600 18,960

9.0 1,772

6.8 1,339

4.7 925

3.4 669

Rate-of-climb at intermediate emergency power S.L.

m ft/min

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

m ft

5,200 17,060

3,700 12,139

2,500 8,202

1,800 5,906

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

m ft

4,500 14,764

3,050 10,007

1,750 5,741

950 3,117

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


332 L1 07.101.02 E

32 ®

®


Technical Data

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 :  M > 8,350 kg :

7,620 m – 25,000 ft 2,895 m – 9,500 ft

Pressure Altitude Pressure Altitude

Take-off and landing :

4,572 m – 15,000 ft

Density Altitude



Maximum temperature





Minimum temperature

ISA + 35°C limited to 50°C - 30°C (basic) - 45°C (with optional installation for flight in extreme cold weather)

Abbreviations AEO : AGL : DA : IGE : ISA : MCP : OEI : OGE : PA :

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

SL : TAS TOP : VNE : VTOL : Vtoss : Vy : Vz :

Sea Level True Air Speed Take-Off Power Never Exceed Speed Vertical Take-Off and Landing Take-off safety speed Optimum climbing speed Rate-of-climb

Units nm : kts: ft/min : m/sec : °C:

nautical miles knots feet/minute meters per second degrees Celsius

hr:min : kg : lb : km :

hours:minutes Kilograms pounds kilometers


332 L1 07.101.02 E

33 ®

®


Technical Data

Blank


332 L1 07.101.02 E

34 ®

®


Technical Data

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) Take-off weight in hover OGE, (on 2 engines, at take-off power or max torque, no wind) 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 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 Recommended cruise speed (pitch 15°5) ISA Recommended cruise speed (pitch 15°5) ISA + 20°C Rate of climb in oblique flight (on 2 engines, at best climb speed) ISA Rate of climb in oblique flight (on 2 engines, at best climb speed) ISA + 20°C Rate of climb in oblique flight (on 1 engine, at intermediate emergency power) ISA Rate of climb in oblique flight (on 1 engine, at intermediate emergency power) ISA + 20°C Hourly fuel consumption at maximum cruise speed (pitch 16°5, M ≤ 8,350 kg) ISA Hourly fuel consumption at maximum cruise speed (pitch 16°, M > 8,350 kg) ISA Hourly fuel consumption at maximum cruise speed (pitch 16°5, M ≤ 8,350 kg) ISA + 20°C Hourly fuel consumption at maximum cruise speed (pitch 16°, M > 8,350 kg) ISA + 20°C Hourly fuel consumption at recommended cruise speed ISA Hourly fuel consumption at recommended cruise speed ISA + 20°C Take off clear heliport CAT A

Page 36 Page 37 Page 38

Page 39

Page 40

Page 41

Page 42

Page 43

Page 44

Page 45

Page 46

Page 47

Page 48

Page 49

Page 50

Page 51

Page 52


332 L1 07.101.02 E

35 ®

®


Technical Data TAKE-OFF WEIGHT IN HOVER IGE (HEIGHT = 10 FT) (10 ft, on 2 engines, at take-off power or maximal torque, no wind)


332 L1 07.101.02 E

36 ®

®


Technical Data TAKE-OFF WEIGHT IN HOVER OGE (on 2 engines, at take-off power or maximal torque, no wind)


332 L1 07.101.02 E

37 ®

®


Technical Data 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


332 L1 07.101.02 E

38 ®

®


Technical Data 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


332 L1 07.101.02 E

39 ®

®


Technical Data RECOMMENDED CRUISE SPEED Pitch: 15°5 ISA


332 L1 07.101.02 E

40 ®

®


Technical Data RECOMMENDED CRUISE SPEED Pitch : 15°5 ISA + 20°C


332 L1 07.101.02 E

41 ®

®


Technical Data RATE-OF-CLIMB IN OBLIQUE FLIGHT (on 2 engines, at best climb speed) ISA


332 L1 07.101.02 E

42 ®

®


Technical Data RATE-OF-CLIMB IN OBLIQUE FLIGHT (on 2 engines, at best climb speed) ISA + 20°C


332 L1 07.101.02 E

43 ®

®


Technical Data RATE-OF-CLIMB IN OBLIQUE FLIGHT (on 1 engine, at intermediate emergency power) ISA


332 L1 07.101.02 E

44 ®

®


Technical Data RATE-OF-CLIMB IN OBLIQUE FLIGHT (on 1 engine, at intermediate emergency power) ISA + 20°C


332 L1 07.101.02 E

45 ®

®


Technical Data HOURLY FUEL CONSUMPTION AT MAXIMUM CRUISE SPEED (pitch 16°5) M

8350 kg ISA


332 L1 07.101.02 E

46 ®

®


Technical Data HOURLY FUEL CONSUMPTION AT MAXIMUM CRUISE SPEED (pitch 16°) M > 8350 kg ISA


332 L1 07.101.02 E

47 ®

®


Technical Data HOURLY FUEL CONSUMPTION AT MAXIMUM CRUISE SPEED (pitch 16°5) M

8350 kg

ISA + 20°C


332 L1 07.101.02 E

48 ®

®


Technical Data HOURLY FUEL CONSUMPTION AT MAXIMUM CRUISE SPEED (pitch 16°) M > 8350 kg ISA + 20°C


332 L1 07.101.02 E

49 ®

®


Technical Data HOURLY FUEL CONSUMPTION AT RECOMMENDED CRUISE SPEED

ISA


332 L1 07.101.02 E

50 ®

®


Technical Data HOURLY FUEL CONSUMPTION AT RECOMMENDED CRUISE SPEED

ISA + 20°C


332 L1 07.101.02 E

51 ®

®


Technical Data

TAKE-OFF CLEAR HELIPORT Cat. A


332 L1 07.101.02 E

52 ®

®


Technical Data

6 - 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 delivered SUPER PUMA and COUGAR is over to 648 helicopters world-wide. The total flight hours accumulated at this date are about 3,307,000 hours. The “lead the fleet” aircraft has accumulated 34,000 flight hours.


332 L1 07.101.02 E

53 ®

®


Technical Data

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 t hose 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

1200 MMH 7500 flight hrs or 15 years periodicity tasks

Scheduled Engine Inspection Estimated Man Hour MAKILA 1A1 30 flight hrs periodicity tasks 50 flight hrs periodicity tasks 0,0836 MMH per FH 300 flight hrs periodicity tasks 600 flight hrs periodicity tasks MMH: Mean Man Hour Note: All the “hands-on” aircraft values mentioned here above are given on the basis of a 20 000 flight hours life cycle. They refer only to the scheduled inspections for the standard helicopter without optional equipment in accordance with the Master Servicing Manual (MSM). The announced Man Hours are without incoming flight, work preparation, reworking, servicing, Service Bulletin implementation and unscheduled maintenance.


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Technical Data

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

Main Components Alternator 40 KVA

5000

Hydraulic Pump

3000

Booster Pump

2000

SLL (h)

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 Gear Box

3000

MGB Support Flexible Monting Plate

9500

Tail Gear Box

3500

Tail Rotor Hub

3500

Intermediate Gear Box

3400

Main Servo Control

3000

Main Components

TBO (h)

MAKILA 1A1

SLL (h)

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

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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: • • • • • •

Classical Support Standard exchange Repair with guaranteed Turn Around Times (TAT) Guaranteed Direct Maintenance Costs (DMC) Unscheduled Maintenance Insurance Plan Parts by the Hour service


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Classical Support The classical 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.

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.

Repair with Guaranteed TAT EUROCOPTER offers for some components a repair with commitment on guaranteed TAT. When this lead time is exceeded for the repair, EUROCOPTER provides the customer with a standard part exchange delivery at the same price as agreed for the repair.

Guaranteed DMC The Guaranteed DMC services offers guaranteed repair and overhaul TATs as well as guaranteed prices. This addition to the classical 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 basic equipment. The data set forth in this document are general in nature and for information purposes only. They may vary with conditions. For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.

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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 factoryauthorized service facilities strategically located near to you Turbomeca range of services covers: • Classical 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


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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 T YPE

COURSE REFERENCE

THEORETICAL INSTRUCTION

FULL FLIGHT

FLIGHT INSTRUCTION

SIMULATOR Pilots

Type Rating (with simulator)

10 days (1)

Instructor Pilot Conversion (with simulator)

COURSE T YPE

COURSE REFERENCE

10

-

Blades

hours

6 Hours

2 hours 2 hours

THEORETICAL & PRACTICAL INSTRUCTION

Mechanics Type Rating (Airframe + engine) Avionics

1/2

5 weeks

Type Rating

4 weeks

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.


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

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AS332L1 Technical Data

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