Eurocopter reserves the right to make configuration and data changes at any time without notice.The facts and figures contained in this document and expressed in good faith do not constitute any offer or contract with Eurocopter

TechnicalData

355 N 05.101.01 E

EUROCOPTER

AS355 N

C

M

J

CM

MJ

CJ

CMJ

N

Base_Ecureuil.ai 03/02/2005 09:13:24Base_Ecureuil.ai 03/02/2005 09:13:24

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 1This 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

Contents

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

2 - General characteristics ........................................................................... 4

3 - Standard Aircraft Definition ................................................................... 11

4 - Optional equipment ................................................................................ 13

5 - Incompatibility between of optional equipment ..................................... 25

6 - Main performance .................................................................................... 29

7 - Customer Service Overview ................................................................... 49

Manufacturers notice

Attention !

Eurocopter’s policy is one of on-going product enhancement which meansthat alterations in definition, pictures, weights, dimensions or performancemay be made at any time without notice being included in those documentsthat have already been issued.

This document cannot thus be taken as an offer or serve as an appendix to acontract without a prior check as to its validity and prior written agreement ofEUROCOPTER.

The operational or certification regulations, as defined by the localauthorities, can make compulsory the installation of some of the equipmentand recommended solutions, listed in this document. This list does not claimto cover the whole of the worldwide operational requirements nor theequipment 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 theplanned configuration of the helicopter complies with regulatory requirementsfor the area(s) of operations and the type(s) of mission(s) considered.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 2This 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

Blank

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 3This 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

1- Foreword

The AS 355 N twin engine version of the ECUREUIL family is powered with 2

TURBOMECA ARRIUS 1A engines of 520 shp (388 kW) each. It benefits from the

FADEC system (Full Authority Digital Engine Control) which makes piloting easier and

safer. it is the most affordable twin-engine helicopter in the market.

Thanks to its two engines and its redundant systems, the AS 355 N is able to perform

missions such as flights over water, or hostile environments by day and night.

Equipped with options required by the local regulation, it is compliant with the JAR

OPS 3 regulation requirements for operations in performance class 1. More particularly,

it is totally suited for police and MEDEVAC operations over large cities, aerial work and

offshore support operations. It is fully Category A and IFR certified. It can also be

equipped with a 3 axis autopilot.

Thanks to its single engine flight performance, the AS 355 N is able to operate from

building rooftops, to work near power lines or to ensure safe harbour pilot

transportation.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 4This 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

2- General Characteristics

Lay-Out

� Passenger-transport � 1 pilot + 5 passengers in standard version� 1 pilot + 4 or 5 passengers in "comfort" version� 1 pilot + 6 passengers in "high density" version

� Casualty-evacuation� 1 pilot + 1 or 2 stretcher patients + 2 doctors

� Cargo carrying� 1 pilot + 3 m³ (105.9 ft³) load in cabin

Weights

Note : Empty weight accuracy : within � 2 % kg lb� Empty weight, standard aircraft

(including engine oil and unusable fuel) 1,437 3,168

� Useful load 1,163 2,564� Maximum all-up weight 2,600 5,732� Maximum cargo-swing load 1,134 2,500� Maximum all-up weight in external load configuration 2,600 5,732

Power plant

2 TURBOMECA ARRIUS 1A turbine engines

Engine ratingsThermodynamic Power, in standard atmosphere, at sea level : kW ch shp

� Maximum emergency power (OEI 2½min.) 388 528 520� Intermediate emergency power (OEI 30 min.) 358 487 480� Take-off power 340 462 456� Maximum continuous power 296 402 397

Usable Fuel capacitieslitres US gal. kg lb

� Standard fuel tanks 730 193 577 1,272� Auxiliary fuel tank (option) 475 125 375 827

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 5This 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

Main dimensions

Dimensions with blades folded

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 6This 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

Configurations

Standard lay-out

Customizedlay-out

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 7This 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

Dimensions of compartments and accesses

Cabin main dimensions

CABINSurface

A2.60 m²27.98 ft²

Volume 3.000 m³105.94 ft³

LH HOLDSurface 0.43 m²

4.62 ft²Volume 0.235 m³

8.29 ft³

RH HOLDSurface 0.35 m²

3.76 ft²Volume 0.200 m³

7.06 ft³

REAR HOLDSurface 0.55 m²

5.92 ft²Volume 0.496 m³

17.50 ft³

TOTAL HOLDSSurface 1.33 m²

14.3 ft²Volume 0.931 m³

32.85 ft³

Cabin floor

� Pilot's safety belt attachment and freight-tie-down rings

� Passenger safety belt or freight tie-down rings

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 8This 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

Other characteristics

TURBOMECA ARRIUS 1A turbine engines

� 520 shp (388 kW) maximum contingency power

� Optimized engine ratings according to outsideoperations conditions thanks to electronicgoverning system (FADEC)

� Modular design

� Fully proven and reliable engine

IFR cockpit lay-out (on option)

� Standard redundant hydraulic and electricalsystems

� Single-pilot or two-pilot possible configurations

� 3 axis autopilot with flight director coupler

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 9This 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

Criteria for Category A or JAR OPS 3 operations

The twin-engined helicopters that are :

� certified according to FAR Part 27

� compliant with the FAR Part 29 requirements for CAT.A engine insulation

� compliant with the JAR Part 29 requirements, as clarified in IEM OPS 3480

have the Category A equivalence.

The ECUREUIL AS355N complies with the above-mentioned requirements and thus has the Category Aequivalence, which is mandatory for JAR OPS 3 operations in performance class 1 and 2.

All the conditions relating to the helicopter that are required for the JAR OPS 3 Performance Class 1operations are met by the ECUREUIL AS355N as soon as :

1. the aircraft is equipped with the "Engines fire-extinguishing system".This installation is available as an optional item on new helicopter (commercial reference05-22004-00-CI) or it can be installed after delivery according to the Service Bulletin n° 26-01.

2. the weight conditions for the procedure on helipad are respected. These are described in the FlightManuel Supplement n° 2 "Procedures and performance data on clear airfield and helipad with oneengine inoperative - Normal mode and Training mode".

3 All other equipment items, required by the local flight regulations of the country concerned, areinstalled and serviceable.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 10This 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

Blank

ECUREUIL AS 355 NTechnical Data

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

355 N 05.100.01 E 11This 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

3- AS 355 N ECUREUIL - Standard Aircraft DefinitionThe helicopter in the definition, presented hereafter, is approved by the following airworthiness authorities : DGAC, LBA, ENAC, CAA, FAA.This list is not restrictive and the status of approval by other airworthiness authorities must be checked.According to the type of operations considered (day or night VFR, single or two-pilot IFR), this definition must be supplemented in agreementwith the local regulation in force.

GENERAL� Fuselage comprising the cabin and 3 luggage holds with

floor, tie-down nets and access doors� Tail boom with stabilizer, anti-torque rotor and fin� Skid landing gear capable of taking handling wheels� Lifting points

� Upper mooring fixtures� External paint : fuselage according to standard paint

schemes. Unless modified by optional item, the main rotorhead cover and the skid landing gear are painted in grey.

� Internal paint : grey.

CABIN� Cabin floor in light-alloy sheet-metal with tie-down rings� 2 pilot and copilot high-back seats, adjustable in reach,

removable, complete with cushions, safety belts and dual-strap shoulder harnesses

� 2 two-place rear bench-seats, foldable separately, completewith cushions, safety belts and single-strap shoulderharnesses

� 2 pilot and copilot jettisonable doors each fitted with a slidingwindow

� 2 rear door-extensions for passengers and cargo� 2 tinted upper panes� 1 double-wall ceiling housing the ventilation and air

conditioning ducts� Fixed parts for pilot and copilot windshield wipers� 1 pilot map case� Demisting system for pilot and copilot front panes� 1 fire-extinguisher� 1 Flight Manual.

INSTRUMENTS� 1 airspeed indicator� 1 altimeter� 1 rate-of-climb indicator� 1 torquemeter (2 needles)� 1 triple tachometer (N rotor - free turbines 1 & 2)� 1 engine outlet temperature dual indicator� 2 engine oil temperature indicators� 2 engine oil pressure indicators� 2 alpha-numerical Ng indicators� 1 �Ng indicator

� 2 fuel contents gauges� 2 fuel pressure indicators� 1 ammeter� 1 voltmeter� 1 clock� 1 warning panel� 1 OAT indicator on canopy� 1 magnetic compass� 1 heated pitot head.

POWER PLANT� 2 Turboméca ARRIUS 1A turbine engines, developping

388 kW (528 ch – 520 shp) max. emergency power (oneengine inoperative), complete with starting, fuel supply, fuelreheating, digital engine control (DEC) with manual back-upgoverning, overspeed protection, in-flight restart systems andfitted with 2 chip detectors.

� 2 fuel systems including 2 independent tanks of 730 litres(193 US gal.) total capacity

� 2 engine lubrication and oil cooling systems� 4 fire detection systems� 2 air-intake protective grids� 2 torque-measurement pick-ups.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.100.01 E 12This 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

TRANSMISSION SYSTEM� 1 main gearbox, anti-vibration mounted, with oil sight gauge,

chip detector, oil temperature and pressure switches, port forendoscope and self-sealing valve for oil sampling anddraining

� 1 combination box� 1 main gearbox oil cooling system� 2 engine to main gearbox coupling shafts

� 1 rotor brake� 1 main rotor r.p.m. sensor and high and low r.p.m. warning

device� 1 tail drive carried by six ball bearings� 1 tail gearbox with oil sight gauge, chip detector and port for

endoscopic inspection.

ROTORS AND FLYING CONTROLS� 1 main rotor with 3 composite-material blades around a

Starflex head fitted with spherical thrust bearings� 1 anti-torque rotor with 2 composite-material blades� 2 hydraulic generation systems

� 3 dual-body main rotor hydraulic servo units� 1 tail rotor hydraulic servo-unit and a load compensator� Flying controls with provisions for the autopilot.

ELECTRICAL INSTALLATION� 2 4.5 kW, 28 V DC starter-generators, supplying two

independant bus bars� 1 15 amp.hr cadmium-nickel battery� 1 ground power receptacle� 3 position lights

� 1 flashing anti-collision light� 2 fixed landing lights� 2 cabin dome lights� Instrument-panel, ceiling-panel and console lighting� 1 28 V DC cabin power outlet.

AIRBORNE KIT (*)� 2 pitot head covers� 2 static vent blanks� 1 radiator air-intake cover� 2 engine air-intake covers� 2 tail-pipe covers� 2 twin-wheel units c/w hydraulic jacking system

� 1 lifting ring� 2 upper mooring rings� 3 main-blade socks� 1 tail rotor locking device� 1 document holder� 1 airborne kit stowage bag.

(*) (weight not included in standard aircraft empty weight)

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 13This 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

4- Optional equipment4-1 Mission package

Eurocopter proposes one mission package, specially designed for passenger transport, offering anhigh level of finishing.

This package must be regarded as a whole and its contents cannot be modified nor soldseparately.

The cabin layout offers transportation ability for one pilot and one passenger at the front and for 3passengers at the rear. An optional transformation kit allows transporting 4 rear passengers.

All the optional items listed in chapter 4-2 can be installed as equipment complementary to thispackage, in coherence with the table of incompatibility presented in chapter 5.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 14This 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

Documentreference

Commercialreference

Name

00-50022-A 00-50022-00-CI Stylence ® package 163 kg - 418 lbExtra charge for customized external paint - level 2 1Tinted windowsCabin heating installationAir conditioning systemLow skid landing gear with 2 short footstepsLayout Stylence ®, including mainly� Light grey internal paint� Energy absorbing front seats upholstered in leather, with casing made

of carbon fiber and leather storage pouch� 3-place rear bench seats upholstered in leather with fairing of the lower

part� Integrated door case covered with light grey leather on large RH front

door� Left rear sliding door� Cabin carpet with one set of overcarpets� Carpet edge protection� Upholstery panels on cabin ceiling and rear partition with sound-

proofing� Leather insert on rear partition� Carpet baggage bay floor covering� Protection covers for seats� Protection cover for carpetVFR day and night solution� Thales H 321 EHM - Gyro-horizon� Honeywell KCS 55 A - Gyro Compass with Honeywell KI 525 A -

Horizontal Situation Indicator� UI 9560 - Turn and Bank indicator� Honeywell KX165A - VHF/VOR/LOC/GS� Garmin GNS 430 - VHF/VOR/LOC/GS/GPS� Garmin GTX 327 - Transponder (mode A+C)� Shadin 8800 T - Altitude Encoder� Kannad 121 AF-H - Emergency Locator Transmitter� Garmin GMA340H - ICS

The STYLENCE ® layout is available in 6 colour schemes :� Brick � Aubergine � Camel� Graphite � Chocolate � Marine

AS 355 N Stylence ® configuration empty weight : 1 600 kg - 3 586 lb

Specific optional item

00-50022-A 00-50022-01-CI Stylence ® 4 rear places layout transformation kit 10 kg - 22 lb

The aircraft equipped empty weight is correct to ± 2 %. According to aircraft equipment, ballast may berequired to accommodate various mission configurations. 1 Sophisticated paint scheme with finishing of superior quality, possibility of varnished finishing.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 15This 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

4-2 List of optional equipmentNote : value of the weight breakdown is given for information and shall not be considered as contractual.

General equipment

Documentreference

Commercialreference

Name kg lb

05-01016-A 05-01016-01-CI C.A.A. V.F.R. certification kit 1 14.5 32.0

05-01017-A 05-01017-00-CI C.A.A. I.F.R. (single pilot or two pilot) certification kit 2 33.5 73.9

05-02004-A 05-02004-00-CI Extra-charge for customized external paint - level 1 3 4.0 8.8

05-02005-A 05-02005-00-CI Extra-charge for customized external paint - level 2 4 4.0 8.8

05-02006-A 05-02006-00-CI Extra-charge for customized external paint, apart from levels 1and 2 5

On request

05-21004-A 05-21004-00-CI Wire strike protection system 6 9.9 21.8

05-22004-A 05-22004-00-CI Engine fire-extinguishing system 7 6.2 13.7

05-23002-A 05-23002-00-CI Engine flushing device without removal of cowlings 0.7 1.5

05-24003-A 05-24003-00-CI High visibility main rotor blades 0.1 0.2

05-24004-A 05-24004-00-CI Tail rotor arch 1.5 3.3

05-25004-A 05-25004-00-CI Sand-prevention filters, dynamic type 26.4 58.2

05-25006-A 05-25006-00-CI Re-inforced sand-erosion protection strip on main rotor blades 0.2 0.4

05-25007-A 05-25007-00-CI Re-inforced sand-erosion protection strip on tail rotor blades 0.1 0.2

05-28001-A 05-28001-00-CI Protective lower cowlings On request

05-31003-A 05-31003-00-CI Tinted window for standard and optional configuration 0.0 0.0

05-31004-A 05-31004-01-CI Bulged window on copilot front door (LH side) -0.5 -1.1

05-31004-A 05-31004-02-CI Bulged window on right rear door 0.1 0.2

05-31004-A 05-31004-03-CI Bulged window on left rear door 0.1 0.2

05-32001-A 05-32001-00-CI Pilot's windshield wiper 8 2.6 5.7

05-32003-A 05-32003-00-CI Copilot's windshield wiper 8 2.6 5.7

1 These extras cover in particular the following items of optional equipment : Engine fire-extinguishing system,

RH landing-light (swivelling in elevation) and LH landing-light (swivelling in elevation and azimuth).2 These extras cover in particular the following items of optional equipment : Engine fire-extinguishing system,

RH landing-light (swivelling in elevation), LH landing-light (swivelling in elevation and azimuth),2nd battery / 2nd altimeter.

3 Paint scheme comprising a basic shade and 2 or 3 additional shades, with straight separation lines, apart fromstandard paint schemes.

4 Paint scheme comprising a basic shade and up to 3 additional shades, with separation lines not straight or tangledup, with graduated shades or complicated emblem or logo to be hand-painted.

5 Sophisticated paint scheme with numerous shades, complex graduated shades, or complicated emblem or logo.6 This optional item has to be fitted in production line.7 Mandatory for JAR OPS 3 operations in performance classes 1 and 2.8 Optional equipment already included in the copilot IFR kit when this configuration is purchased.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 16This 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

General equipment (continued)

Documentreference

Commercialreference

Name kg lb

05-37008-A 05-37008-00-CI Dual controls 1 4.7 10.4

05-41003-A 05-41003-00-CI Cabin heating installation 2 2.1 4.6

05-42004-A 05-42004-00-CI Air conditioning system 3 55.0 121.3

05-61007-A 05-61007-00-CI 2nd battery kit 4 18.0 39.7

05-62002-A 05-62002-00-CI 250 VA AC 1st generation system 5 4.8 10.6

05-70001-A 05-70001-00-CI Hydraulic ground power receptacle 1.7 3.7

05-82017-A 05-82017-00-CI Fuel tanks self-sealing protection 21.0 46.3

05-84002-A 05-84002-00-FP Ferrying tank - Fixed Parts 0.3 0.705-84002-00-RP Ferrying tank - Removable Parts 27.6 60.8

05-85003-A 05-85003-00-CI Remaining fuel flowmeter 2.0 4.4

05-92002-A 05-92002-00-FP Folding of main rotor blades - Fixed Parts 6 1.8 4.005-92002-00-RP Folding of main rotor blades - Removable Parts 7 not applicable

05-93001-A 05-93001-00-CI Mooring kit (ground or ships) 8 0.8 1.8

05-93002-A 05-93002-00-CI Marine gripping system 1.0 2.2

Specific mission equipment

06-11008-A 06-11008-00-CI SURFAIR Skis 9 27.0 59.5

06-11012-A 06-11012-00-CI Settling protectors 4.1 9.0

06-11017-A 06-11017-00-CI Skid wearing plates 1.3 2.9

06-12012-A 06-12012-00-CI Low skid landing gear with 2 short footsteps 10 7.9 17.4

06-12013-A 06-12013-02-CI High skid landing gear with 2 double footsteps 10 10.7 23.6

06-12014-A 06-12014-02-CI High skid landing gear with 2 short footsteps 10 16.0 35.3

06-12015-A 06-12015-01-CI High skid landing gear with 2 long footsteps 10 16.9 37.3

1 Optional item of equipment already included in the copilot IFR kit when this configuration is purchased.2 Optional item of equipment already included in the single-pilot IFR kit when this configuration is purchased.3 Available : cycle + 2 months. Requires the fitting of one of the optional items 07-00009-00-CI “Comfort layout”

or 07-00011-00-CI “Comfort lay-out with sound-proofing” or 07-00012-00-CI “Executive lay-out”.4 Recommended for start-up in cold weather.5 Mandatory for autopilot.6 Capable of rough weather conditions.7 The removable parts are delivered as Ground Support Equipment. Tool weight = 32.2 kg - 71 lb.8 Recommended for transport by land, air and sea (when not in a container).9 Incompatible with the optional item 06-12015-01-CI "High skid landing gear with 2 long footsteps".10 Replaces the standard type of landing gear.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 17This 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

Specific mission equipment (continued)

Documentreference

Commercialreference

Name kg lb

06-21002-A 06-21002-00-FP AIR EQUIPEMENT electrical hoist(136 kg - 300 lb, 40 m - 131 ft cable) - Fixed Parts 1

2.6 5.7

06-21002-00-RP AIR EQUIPEMENT electrical hoist(136 kg - 300 lb, 40 m - 131 ft cable) - Removable Parts

37.5 82.7

06-21006-A 06-21006-00-FP BREEZE electrical hoist (204 kg - 450 lb, 50 m - 164 ft cable) -Fixed Parts 1

3.3 7.3

06-21006-00-RP BREEZE electrical hoist (204 kg - 450 lb, 50 m - 164 ft cable) -Removable Parts

51.8 114.2

06-21018-A 06-21018-00-CI Support for Breeze electrical hoist 2 5.4 11.9

06-24001-A 06-24001-00-CI Rappelling installation (without rope) 3 3.2 7.1

06-25001-A 06-25001-00-CI Drip tub (sea rescue) 4 -0.8 -1.8

06-26003-A 06-26003-00-CI RH side external mirror 5 - 6 2.9 6.4

06-27006-A 06-27006-00-FP Cargo swing with dynamometer (1,134 kg - 2,500 lb) - FixedParts 7

4.5 9.9

06-27006-00-RP Cargo swing with dynamometer (1,134 kg - 2,500 lb) -Removable Parts

13.2 29.1

06-31006-A 06-31006-00-CI Integrated hailers 8 7.4 16.3

06-42006-A 06-42006-00-CI RH landing light (swivelling in elevation) 9 3.1 6.8

06-42007-A 06-42007-00-CI LH Landing-light (swivelling in elevation and azimuth) 3.4 7.5

06-47002-A 06-47002-00-FP Spectrolab SX 16 search-light - Fixed Parts 5.5 12.106-47002-00-RP Spectrolab SX 16 search-light - Removable Parts 29.5 65.0

06-47003-A 06-47003-00-CI Infra Red filter for SPECTROLAB SX-16 search-light 10 2.0 4.4

06-61004-A 06-61004-00-FP Emergency floatation gear - Fixed Parts 5.7 12.606-61004-00-RP Emergency floatation gear - Removable Parts 67.6 149.0

06-74006-A 06-74006-00-CI Adaptation for night-time missions with NVG On request

1 Implies the fitting of the optional item 07-50003-00-CI "Left rear sliding door".2 Requires the selection of the optional item 06-21006-00-FP "BREEZE electrical hoist - Fixed Parts".3 Implies the fitting of rear sliding door on both sides.4 The weight figure includes the removal of the cushions of the two standard two-place rear bench-seats

and seat belts (bench seats folded).5 Recommended for sling/swing work.6 The optional item 06-42006-00-CI "RH swivellable landing light" is recommended for simultaneous use.7 Implies the fitting one type of high skid landing gear : 06-12013-02-CI or 06-12014-02-CI or 06-12015-01-CI.8 Compatible with coupler SFIM CDV 85 T 3.

Incompatible with the optional item 06-61004-00-FP "Emergency floatation gear - Fixed Parts".9 Optional items of equipment already included in the single-pilot IFR instrument kit when this configuration is

purchased.10 The filter is not remotely controlled retractable.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 18This 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

Interior cabin layout

Documentreference

Commercialreference

Name kg lb

07-00009-A 07-00009-00-CI Comfort layout 30.7 67.7

07-00011-A 07-00011-00-CI Comfort lay-out with sound-proofing 43.7 96.3

07-00019-A 07-00019-00-CI Alternate fabrics for seats On request

07-00020-A 07-00020-00-CI Leather upholstery for seats 1 On request

07-15010-A 07-15010-00-CI Energy-absorbing front seats 3.0 6.6

07-15010-A 07-15010-01-CI Lengthened rails for energy-absorbing front seats 2 2.0 4.0

07-24004-A 07-24004-00-FP Left side two-place front bench seat (pilot on right side) - FixedParts 3

2.3 5.1

07-24004-00-RP Left side two-place front bench seat (pilot on right side) -Removable Parts

3.2 7.1

07-25001-A 07-25001-00-CI 3 places instead of 4 places transformation kit 4 4.4 9.7

07-40003-A 07-40003-00-CI Velvet carpeting 1 On request

07-40004-A 07-40004-00-CI Washable floor covering On request

07-50002-A 07-50002-01-CI Improved side-visibility in RH large front door 3.0 6.6

07-50002-A 07-50002-02-CI Improved side-visibility in LH large front door 3.0 6.6

07-50003-A 07-50003-00-CI Left rear sliding door 5 3.4 7.5

07-50005-A 07-50005-00-CI Right rear sliding door 5 3.4 7.5

07-50006-A 07-50006-00-CI Sliding window, on rear LH sliding door 1.1 2.4

07-50007-A 07-50007-00-CI Sliding window, on rear RH sliding door 1.1 2.4

07-70013-A 07-70013-00-CI EMS kit (AAT) 6 Refer to AAT

07-71001-A 07-71001-00-FP Lower casualty carrying installation with stretcher - Fixed Parts 0.3 0.707-71001-00-RP Lower casualty carrying installation with stretcher - Removable

Parts 7-4.5 -9.9

07-71006-A 07-71006-00-FP Upper casualty carrying installation with stretcher- Fixed Parts 8

0.2 0.4

07-71006-00-RP Upper casualty carrying installation with stretcher - RemovableParts 7

-2.9 -6.4

1 Option available for the optional items 07-00009-00-CI "Comfort lay-out" and

07-00011-00-CI "Comfort lay-out with sound-proofing".2 Requires the selection of the optional item 07-15010-00-CI "Energy-absorbing front seats".3 The two-place front bench seat is incompatible with the I.F.R version.4 Including mainly 4 arm-rests and a fifth harness.5 Improved side visibility in the corresponding front door included in the optional equipment.6 Air Ambulance Technology (AAT) is responsible for the conformity, performance and certification

of the ambulance installation on the helicopter.7 Each weight figure includes the complete removal of one two-place rear bench seat and copilot seat. When the

removable parts of lower and upper casualty carrying installations are installed simultaneously, the total weightsupplement for both removable parts is 12.8 kg – 28.2 lb.

8 Incompatible with I.F.R. instrument panel. Compatibility with the VFR instrument panel to be checked accordingto the radio communication / navigation configuration.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 19This 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

Avionics

VFR day and night recommended package

Documentreference

Commercialreference

Name kg lb

08-00014-A 08-00014-01-CI VFR day and night solution 28.0 61.7

IncludingThales H 321 EHM - Gyro-horizon 1Honeywell KCS 55 A - Gyro Compasswith Honeywell KI 525 A - Horizontal Situation Indicator 2UI 9560 - Turn and Bank indicatorHoneywell KX165 - VHF/VOR/LOC/GSGarmin GNS 430 - VHF/VOR/LOC/GS/GPS 3Garmin GTX 327 - Transponder (mode A+C)Shadin 8800 T - Altitude EncoderKannad 121 AF-H - Emergency Locator Transmitter 4Team TB 27 - ICS 5Team BA1816 - Passenger Interphone

Equipment that can replace an equipment in recommended package

Documentreference

Commercialreference

Name kg lb

06-67031-A 06-67031-02-CI KANNAD 406 AF-H - Emergency Locator Transmitter 6 - 7instead of KANNAD 121 AF-H - Emergency LocatorTransmitter

0.1 0.2

08-11006-A 08-11006-00-CI Honeywell KX165A - VHF/VOR/LOC/GS 8instead of Honeywell KX 165 - VHF/VOR/LOC/GS

On request

08-16040-A 08-16040-02-CI Garmin GMA 340 H 8 - 9 - 10 instead of Team TB 27 - ICS +Team BA 1816 - Passenger Interphone

On request

08-22025-A 08-22025-00-CI Garmin GTX 330 - Transponder (mode S) 7 - 11instead of Honeywell KT 76 A - Transponder (mode A+C)

0.6 1.3

08-51018-A 08-51018-01-CI Thales H 140 - Gyro-horizoninstead of Thales H 321 EHM - Gyro-horizon

0.4 0.9

08-51019-A 08-51019-02-CI Thales H 321 EHM - Stand-by gyro-horizoninstead of UI 9560 - Turn and Bank indicator

3.0 6.6

1 With slip indicator included when the Turn and Bank indicator is replaced by the stand-by gyro-horizon.2 With a selector switch for NAV1/NAV2 selection.3 Delivered with EUROPE map. Subscription to be made by the customer.4 2 frequencies : 121.5 MHz, 243 MHz. Compliant with ED 62 and TSO C91A.5 I.C.S. compatible only with Low level / High impedance headsets.6 3 frequencies : 121.5 MHz, 243 MHz, 406 MHz. Compliant with ED 62 and TSO C91A.

The Programming Data Sheet must be filled and communicated by the customer two monthsat the latest before the helicopter's delivery.

7 May be a mandatory equipment, required by local airworthiness authorities.8 Availability to be checked.9 I.C.S. compatible only with High level / High impedance headsets.10 Includes the passenger interphone function.11 The mode S identification must be communicated by the customer two months at the latest before the delivery.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 20This 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

Additional equipment that can be added depending on operational needs or therequirements of the authorities in certain countries if not included in therecommended package

Applicable for day and night VFR Certification

Documentreference

Commercialreference

Name kg lb

08-10007-A 08-10007-00-CI Honeywell - KHF 950 - HF/SSB 18.2 40.1

08-12012-A 08-12012-00-CI NAT NPX 138 A - VHF/FM marine 2.5 5.5

08-18011-A 08-18011-00-CI David Clark - H 10-36 - Headset 1 0.5 1.1

08-18013-A 08-18013-00-CI Silec - 4449-1 - Headset 2 0.5 1.1

08-18024-A 08-18024-00-CI Electrical extension 0.2 0.4

08-18025-A 08-18025-00-CI Elno FPH600 - Helmet 1.0 2.2

08-21008-A 08-21008-00-CI Thales AHV 16 - Radio altimeter 5.0 11.0

08-24011-A 08-24011-01-CI Honeywell KR 87 - ADF 3 3.5 7.7

08-25003-A 08-25003-00-CI Honeywell KN 63 - DME 4.3 9.5

08-25017-A 08-25017-00-CI 2nd indicator for Honeywell KN 63 - DME 0.4 0.9

08-26009-A 08-26009-00-CI Honeywell KR 21 - Marker beacon receiver 1.0 2.2

08-46001-A 08-46001-00-CI GPS moving map 4 On request

08-61004-A 08-61004-02-CI Honeywell KI 229 - Radio Magnetic Indicator 2.7 6.0

08-70005-A 08-70005-00-CI SFIM 85 T 31 - 3-axis autopilot 5with failure passivation unit

33.6 74.1

08-91005-A 08-91005-00-CI Hourmeter 0.3 0.7

1 High level / High impedance headset.2 Low level / High impedance headset.3 Implies the fitting of 08-61004-02-CI "HONEYWELL KI 229 - Radio Magnetic Indicator".4 The model currently certified is AVALEX AMS 7000. Other models can be proposed according

to customer's operational needs.5 Implies the mandatory fitting of the 250 VA AC generation system, Thales H140 gyro-horizon.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 21This 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

IFR solutions

Minimum items of equipment - single pilot IFR

Documentreference

Commercialreference

Name kg lb

08-01020-A 08-01020-00-CI Single-pilot IFR installation 110.0 242.5

IncludingSpecial IFR instrument panel in place of the standard oneSecond anemo-barometric circuitThales H 140 - Flight director gyro-horizonHoneywell KCS 55 A - Gyro Compass withHoneywell KI 525 A - Horizontal Situation IndicatorThales H 140 - Stand-by gyro-horizonRate-of-climb indicator with setter in place of the standard oneHoneywell KNI 582 Radio Magnetic Indicatorwith two needles and twin switchingPilot's windshield wiperCopilot's windshield wiperRH landing light (swivelling in elevation) instead of the standardfixed oneCabin heating installationHoneywell KX165 - VHF/VOR/LOC/GSGarmin GNS 430 - VHF/VOR/LOC/GS/GPS 1Honeywell KR 87 - ADFHoneywell KR 21 - Marker beacon receiverHoneywell KT 76 A - Transponder (mode A+C)Shadin 8800 T - Altitude EncoderThales AHV 16 - Radio altimeterSFIM 85 T 31 + SFIM CDV 85 T 3 - 3-Axis AP + FDC, VFR &IFR, with failure passivation unit250 VA AC 1st generation system250 VA AC 2nd generation systemKannad 121 AF-H - Emergency Locator Transmitter 2Team TB 39 (2 control boxes) - ICS 3Team BA1816 - Passenger Interphone

1 Delivered with EUROPE map. Subscription to be made by the customer.2 2 frequencies : 121.5 MHz, 243 MHz. Compliant with ED 62 and TSO C91A.3 I.C.S. compatible only with Low level / High impedance headsets.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 22This 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

Additional equipment for two pilot IFR

Documentreference

Commercialreference

Name kg lb

08-01021-A 08-01021-00-CI IFR copilot kit (for two pilot IFR flight) 18.9 41.7

Including2nd set of instruments for two-pilot IFR :- Altimeter,- Airspeed indicator,- Rate-of-climb indicator,- Rotor tachometer,- Autopilot indicating panel.Honeywell KCS 55 A - Gyro Compass withHoneywell KI 525 A - Horizontal Situation IndicatorThales H 140 - Gyro-horizonDual controls

Equipment that can replace an equipment in IFR solution

Documentreference

Commercialreference

Name kg lb

06-67031-A 06-67031-02-CI KANNAD 406 AF-H - Emergency Locator Transmitter 1 - 2instead of KANNAD 121 AF-H - Emergency LocatorTransmitter

0.0 0.0

08-11006-A 08-11006-00-CI Honeywell KX165A - VHF/VOR/LOC/GS 3instead of Honeywell KX 165 - VHF/VOR/LOC/GS

On request

08-22024-A 08-22024-00-CI Garmin GTX 327 - Transponder (mode A+C) 3instead of Honeywell KT 76 A - Transponder (mode A+C)

On request

08-22025-A 08-22025-00-CI Garmin GTX 330 - Transponder (mode S) 2 - 4instead of Honeywell KT 76 A - Transponder (mode A+C)

0.6 1.3

1 3 frequencies : 121.5 MHz, 243 MHz, 406 MHz. Compliant with ED 62 and TSO C91A.

The Programming Data Sheet must be filled and communicated by the customer two months at the latest beforethe helicopter's delivery.

2 May be a mandatory equipment, required by local airworthiness authorities.3 Availability to be checked.4 The mode S identification must be communicated by the customer two months at the latest before the delivery.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 23This 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

Additional equipment that can be added depending on operational needs or therequirements of the authorities in certain countries if not included in minimumitems package

Documentreference

Commercialreference

Name kg lb

08-10007-A 08-10007-00-CI Honeywell - KHF 950 - HF/SSB 18.2 40.1

08-12012-A 08-12012-00-CI NAT NPX 138 - VHF/FM marine 2.5 5.5

08-18013-A 08-18013-00-CI Silec - 4449-1 - Headset 1 0.5 1.1

08-18024-A 08-18024-00-CI Electrical extension 0.2 0.4

08-18025-A 08-18025-00-CI Elno FPH600 - Helmet 1.0 2.2

08-21017-A 08-21017-00-CI 2nd indicator IND201 for Thales AHV 16 - Radio altimeter 0.9 2.0

08-25003-A 08-25003-00-CI Honeywell KN 63 - DME 3.3 7.3

08-25017-A 08-25017-00-CI 2nd indicator for Honeywell KN 63 - DME 0.4 0.9

08-31023-A 08-31023-00-CI Telephonics RDR 1400 C - Colour Weather Radar 18.5 40.8

08-31024-A 08-31024-00-CI Honeywell RDR 2000 - Colour Weather Radar 2 On request

08-38003-A 08-38003-00-CI BFGoodrich WX1000 - Stormscope 2 6.1 13.5

08-91005-A 08-91005-00-CI Hourmeter 0.3 0.7

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

1 Low level / High impedance headset.2 Availability to be checked.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 24This 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

Blank

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 25This 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

5- Incompatibility between of optional equipment� Impossibility of simultaneous fitment of the fixed parts of 2 items of equipment

� Total or partial incompatibility of simultaneous fitment of the removal parts of two items of equipment

� Possibility of simultaneous fitment on the same aircraft, but impossible to use simultaneously

Note: This table indicates the compatibility restrictions existing between the installations. The consultation of EUROCOPTER is necessary for the definitive EquipmentCompatibility clearance of a configuration.

Nature of the incompatibilityReferenceOptional

Installation� � �

General equipment

05-24004-00-CI Tail rotor arch 08-10007-00-CI

05-32003-00-CI Copilot's windshield wiper 05-42004-00-CI

05-37008-00-CI Dual controls 07-24004-00-RP07-70013-00-CI07-71001-00-RP07-71006-00-RP

05-42004-00-CI Air conditioning system 05-32003-00-CI 07-70013-00-CI07-71001-00-RP07-71006-00-RP

05-84002-00-RP Ferrying tank - Removable parts 07-00009-00-CI07-00011-00-CI07-00012-00-CI07-24004-00-RP07-25001-00-CI07-70013-00-CI07-71001-00-RP07-71006-00-RP

06-21002-00-RP06-21006-00-RP06-27006-00-RP

06-11008-00-CI SURFAIR skis 06-12015-01-CI 06-61004-00-RP

06-12012-00-CI Low skid landing gear with 2 short footsteps 06-61004-00-FP

06-12015-01-CI High skid landing gear with 2 long footsteps 06-11008-00-CI

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 26This 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

Nature of the incompatibilityReferenceOptional

Installation� � �

Specific mission equipment

06-21002-00-FP AIR EQUIPEMENT electrical hoist(136 kg - 300 lb, 40 m - 131 ft cable)- Fixed parts

06-21006-00-FP 1

06-21002-00-RP AIR EQUIPEMENT electrical hoist(136 kg - 300 lb, 40 m - 131 ft cable)- Removable parts

05-84002-00-RP

06-61004-00-RP 206-27006-00-CI06-24001-00-CI07-24004-00-RP07-25001-00-CI07-70013-00-CI07-71001-00-RP07-71006-00-RP

06-21006-00-FP BREEZE electrical hoist(204 kg - 450 lb, 50 m - 164 ft cable)- Fixed parts

06-21002-00-CI 1

06-21006-00-RP BREEZE electrical hoist(204 kg - 450 lb, 50 m - 164 ft cable)- Removable parts

05-84002-00-RP06-24001-00-CI06-27006-00-RP

06-61004-00-RP 207-24004-00-RP07-25001-00-CI07-70013-00-CI07-71001-00-RP07-71006-00-RP

06-24001-00-CI Rappelling installation 3 06-21002-00-RP06-21006-00-RP06-27006-00-RP06-61004-00-RP

06-25001-00-CI Drip tub (sea rescue) 07-00009-00-CI07-00011-00-CI07-25001-00-CI07-70013-00-CI07-71001-00-RP07-71006-00-RP

1 Only the structural supplies included in 06-21006-00-FP "BREEZE electrical hoist – Fixed parts"

are compatible with 06-21002-00-FP "AIR EQUIPEMENT electrical hoist – Fixed parts".2 Hoisting remains possible when the floats are folded.3 Implies the fitting of rear sliding door on both sides.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 27This 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

Nature of the incompatibilityReferenceOptional

Installation� � �

Specific mission equipment(continued)

06-27006-00-FP Cargo swing with dynamometer(1134 kg - 2,500 lb) - Fixed parts

07-00012-00-CI

06-27006-00-RP Cargo swing with dynamometer(1134 kg - 2,500 lb) - Removable parts

06-47002-00-RP 05-84002-00-RP06-21002-00-RP06-21006-00-RP06-24001-00-CI07-24004-00-RP07-70013-00-CI07-71001-00-RP07-71006-00-RP

06-31006-00-CI Integrated hailers 06-61004-00-FP Being studied Being studied

06-47002-00-RP SPECTROLAB SX 16 searchlight- Removable parts

06-27006-00-RP

06-61004-00-FP Emergency floatation gear - Fixed parts 06-12012-00-CI06-31006-00-CI

06-61004-00-RP Emergency floatation gear - Removableparts

06-11008-00-CI 06-21002-00-RP 1

06-21006-00-RP 106-24001-00-CI

06-74006-00-CI Adaptation for night time missions with NVG Being studied Being studied Being studied

Interior arrangement

07-00009-00-CI Comfort lay-out 07-00011-00-CI07-00012-00-CI

05-84002-00-RP06-25001-00-CI07-70013-00-CI

07-00011-00-CI Comfort lay-out with sound-proofing 07-00009-00-CI07-00012-00-CI

05-84002-00-RP06-25001-00-CI07-70013-00-CI

07-00012-00-CI "Executive" lay-out 06-27006-00-FP07-00009-00-CI07-00011-00-CI

05-84002-00-RP06-25001-00-CI07-70013-00-CI

07-15010-00-CI Energy-absorbing front seats Being studied Being studied Being studied

07-24004-00-RP Left side two-place front bench seat(pilot on RH side) - Removable parts

05-37008-00-CI05-84002-00-RP07-70013-00-CI07-71001-00-RP07-71006-00-RP

06-21002-00-RP06-21006-00-RP06-27006-00-RP

1 Hoisting remains possible when the floats are folded.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 28This 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

Nature of the incompatibilityReferenceOptional

Installation� � �

Interior arrangement (continued)

07-25001-00-CI 3 places instead of 4 places transformationkit

05-84002-00-RP06-25001-00-CI07-70013-00-CI07-71001-00-RP07-71006-00-RP

06-21002-00-RP06-21006-00-RP

07-50002-01-CI Improved side-visibility in RH large frontdoor

07-50003-00-CI07-50005-00-CI

07-50002-02-CI Improved side-visibility in LH large frontdoor

07-50003-00-CI07-50005-00-CI

07-50003-00-CI Left rear sliding door 07-50002-02-CI

07-50005-00-CI Right rear sliding door 07-50002-01-CI

07-70013-00-CI EMS kit AAT 05-37008-00-CI05-42004-00-CI05-84002-00-RP07-25001-00-CI07-00009-00-CI07-00011-00-CI07-00012-00-CI07-24004-00-RP06-25001-00-CI07-71001-00-RP07-71006-00-RP

06-21002-00-RP06-21006-00-RP06-27006-00-RP

07-71001-00-RP Lower casualty-carrying installationwith stretcher - Removable parts

05-37008-00-CI05-42004-00-CI05-84002-00-RP06-25001-00-CI07-24004-00-RP07-25001-00-CI07-70013-00-CI

06-21002-00-RP06-21006-00-RP06-27006-00-CI

07-71006-00-RP Upper casualty-carrying installation 1with stretcher - Removable parts

05-37008-00-CI05-42004-00-CI05-84002-00-RP07-25001-00-CI07-24004-00-RP06-25001-00-CI07-70013-00-CI

06-21002-00-RP06-21006-00-RP06-27006-00-CI

Avionics

08-10007-00-CI Honeywell - KHF 950 - HF/SSB 05-24004-00-CI

1 Incompatible with I.F.R. instrument panel. Compatibility with the VFR instrument panel to be checked according to

the radio communication / navigation configuration.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 29This 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

6- Main performanceThe following performance values and figures refer to an AS 355 N, equipped with new engines.Unless otherwise specified, the values and figures refer to a clean helicopter at Sea Level (SL), inInternational Standard Atmosphere (ISA) and zero wind condition.

Performance on 2 engines

Gross Weight kglb

1,8003,968

2,0004,409

2,2004,850

2,4005,291

2,6005,732

� Maximum speed, VNE km/hrkts

278150

278150

278150

278150

278150

� Fast cruise speed (at MCP) km/hrkts

250135

244132

237128

230124

222120

� Recommended cruise speed km/hrkts

244132

237128

231124

223120

215116

� Fuel consumption at recommended cruisespeed

kg/hrIb/h

183403

183403

183403

183403

183403

� Rate-of-climb at MCP m/secft/min

10.92,146

9.91,949

8.91,752

7.71,516

6.41,260

� Hover ceiling IGE (at TOP, height 6 ft)� ISA m

ft 6,00019,685

5,10016,732

4,25013,944

3,40011,155

2,0006,560

� ISA + 20°C mft

5,30017,388

4,30014,108

3,40011,155

2,5508,366

1,4004,590

� Hover ceiling OGE (at TOP)� ISA m

ft5,700

18,7014,700

15,4203,850

12,6312,8509,350

7502,460

� ISA + 20°C mft

4,85015,912

3,90012,795

2,9509,378

2,1006,890

150490

� Service ceiling (1 m/s, 200 ft/min) mft

>6,096>20,000

>6,096>20,000

5,33517,500

4,52514,846

3,80012,470

� Range(without reserve, at recommended cruisespeed)

kmnm

428231

693374

760410

740400

713385

� Endurance(without reserve, at 100 km/hr – 54kts)

hr : min 2h53 4h38 5h05 4h55 4h45

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 30This 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

Performance on 1 engine

Gross Weight kglb

1,8003,968

2,0004,409

2,2004,850

2,4005,291

2,6005,732

� Rate of climb at intermediate contingencypower

m/secft/min

7.01,378

6.11,201

4.9965

3.8748

2.6500

� Service ceiling (1 m/sec., 200 ft/min.)

� ISA mft

4,85015,912

3,90012,795

3,05010,007

2,2507,382

1,4504,757

� ISA + 20°C mft

4,05013,287

3,05010,007

2,1006,890

1,2003,937

250820

� Maximum Temperature for CAT A take-offfrom clear heliport, at SL

°C >50 >50 >50 47.5 36

� Maximum Temperature for CAT A take-offfrom helipad, at SL

°C >50 >50 49 38 -(1)

(1) Maximum weight on helipad CAT. A : 2,540 kg (+ 29°C).

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 : 6,096 m - 20,000 ft (PA)

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

� Minimum temperature – 40°C

For CAT A operations, the density-altitude must be equal to or less than 2,255 m - 7,400 ft.

Abbreviations

AEO : All Engines Operative PA : Pressure AltitudeIGE : In Ground Effect SL : Sea LevelISA : International Standard Atmosphere TAS True Air SpeedMCP : Maximum Continuous Power TOP : Take-Off PowerOEI : One Engine Inoperative VNE : Never Exceed SpeedOGE : Out of Ground Effect Vz : Rate-of-climb

Units

nm : nautical miles hr:min : hours:minuteskts: knots kg : kilogrammsft/min : feet per minute lb : poundsm/sec : meters per second km : kilometers° C : degrees Celsius

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 31This 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

Performance charts

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

� Take-off weight in hover IGE, AEO (height 6 ft, Maximum TOP, no wind)

Page 32

� Take-off weight in hover OGE, AEO(Maximum TOP, no wind)

Page 33

� Take-off weight in hover IGE, OEI(Maximum contingency power, no wind)

Page 34

� Take-off weight in hover OGE, OEI(Maximum contingency power, no wind)

Page 35

� Take-off weight CAT A, clear heliport (Intermediate contingency power)

Page 36

� Take-off weight CAT A, helipad (Maximum contingency power)

Page 37

� Fast cruise speed (ISA)

Page 38

� Fast cruise speed (ISA+ 20°C)

Page 39

� Recommended cruise speed (ISA)

Page 40

� Recommended cruise speed (ISA + 20°C)

Page 41

� Rate of climb in oblique flight(AEO, ISA, MCP)

Page 42

� Rate of climb in oblique flight(AEO, ISA +20°C, MCP)

Page 43

� Rate of climb in oblique flight(OEI, ISA, Intermediate contingency power)

Page 44

� Rate of climb in oblique flight(OEI, ISA +20°C, Intermediate contingency power)

Page 45

� Hourly fuel consumption at fast cruise speed(ISA, ISA + 20°C, ISA +35°C)

Page 46

� Hourly fuel consumption at recommended cruise speed (ISA, ISA + 20°C, ISA +35°C)

Page 47

� Payload/Range (ISA, SL, recommended cruise speed, without reserve)

Page 48

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 32This 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

TAKE-OFF WEIGHTS IN HOVER IGE

on two engines at maximum TOP

(Height 6 ft)

Note : Approved performances (as long as the engines meet the power check criteria), as defined in the Flight Manual.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 33This 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

TAKE-OFF WEIGHTS IN HOVER OGE

on two engines

at maximum TOP

Note : Approved performances (as long as the engines meet the power check criteria), as defined in the Flight Manual.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 34This 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

TAKE-OFF WEIGHTS IN HOVER IGE

on 1 engine

at maximum contingency power

(O.E.I. 2½ min)

Note : Approved performances (as long as the engines meet the power check criteria), as defined in the Flight Manual.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 35This 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

TAKE-OFF WEIGHTS IN HOVER OGE

on 1 engine

at maximum contingency power

(O.E.I. 2½ min)

Note : Approved performances (as long as the engines meet the power check criteria), as defined in the Flight Manual.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 36This 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

TAKE-OFF WEIGHTS FROM A CLEAR HELIPORT (CAT. A)

at intermediate contingency power

(O.E.I. 30 min)

0

2000

4000

6000

8000

0

500

1000

1500

2000

2500

-20 -10 0 10 20 30 40 50

T (°C)

Pressure Altitude (m)(ft) ISO-Weight (kg)

2000

21002200

23002400

2500

2600

2540Std

Std +20

Std +35

7400 ft density altitude limit

Note : Approved performances (as long as the engines meet the power check criteria), as defined in the Flight Manual.

ECUREUIL AS 355 NTechnical Data

F355 N 05

This d

TAKE-OFF WEIGHTS FROM A HELIPAD (CAT. A)

at maximum contingency power

(O.E.I. 2½ min)

0

2000

4000

6000

8000

0

500

1000

1500

2000

2500

0 10 20 30 40 50

T (°C)

Pressure Altitude (m)(ft) ISO-Weight (kg)1800

2000

2200

2400

2600

2540

19002100

2500

2300

7400 ft density altitude limitStd

Std +20

Std +35

Not

Height / speed limitSubstantiated height / speed envelope

The data set forth in this document are general in nature and for information purposes only.or performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents..101.01 E 37ocument 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

e : Approved performances (as long as the engines meet the power check criteria), as defined in the Flight Manual.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 38This 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

FAST CRUISE SPEED

ISA

Note : Typical performance with clean standard aircraft.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 39This 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

FAST CRUISE SPEED

ISA + 20°C

Note : Typical performance with clean standard aircraft.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 40This 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

RECOMMENDED CRUISE SPEED

ISA

Note : Typical performance with clean standard aircraft.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 41This 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

RECOMMENDED CRUISE SPEED

ISA + 20°C

Note : Typical performance with clean standard aircraft.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 42This 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

RATE OF CLIMB IN OBLIQUE FLIGHT

on 2 engines at MCP

ISA

Note : Approved performances (as long as the engines meet the power check criteria), as defined in the Flight Manual.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 43This 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

RATE OF CLIMB IN OBLIQUE FLIGHT

on 2 engines at MCP

ISA + 20°C

Note : Approved performances (as long as the engines meet the power check criteria), as defined in the Flight Manual.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 44This 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

RATE OF CLIMB IN OBLIQUE FLIGHT

on 1 engine

at intermediate contingency power (O.E.I. 30 min)

ISA

Note : Approved performances (as long as the engines meet the power check criteria), as defined in the Flight Manual.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 45This 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

RATE OF CLIMB IN OBLIQUE FLIGHT

on 1 engine

at intermediate contingency power (O.E.I. 30 min)

ISA + 20°C

Note : Approved performances (as long as the engines meet the power check criteria), as defined in the Flight Manual.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 46This 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

HOURLY FUEL CONSUMPTION

at fast cruise speed

ISA, ISA + 20°C, ISA + 35°C

Note : Typical consumption with clean standard aircraft and new engines.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 47This 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

HOURLY FUEL CONSUMPTION

at recommended cruise speed

ISA, ISA + 20°C, ISA + 35°C

Note : Typical consumption with clean standard aircraft and new engines.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 48This 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

PAYLOAD / RANGE

ISA

Recommended cruise speed

Empty weight equipped a/c + 1 pilot : 1,545 kg - 3,406 lb 1

Note : Typical mission without reserve, with clean aircraft and new engines.

1 Aircraft equipped and approved for VFR day and night operations (avionics included in empty weight).

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 49This 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

7- Customer Service Overview

Assets

� Possibility to perform maximum of maintenance tasks by operators through modular exchange,

� Low required manhour on the scheduled maintenance,

� Maintenance simple and easy to perform thanks to optimized accessibility to dynamic components andequipment that is confirmed by Ecureuil large experience (more than 13 millions flight hours),

� Limited number of tools,

� No test bench,

� Among technical publications, Master Servicing Recommendation has been written in such a manner thatit can be directly used as a maintenance tasks repertory in the workshop,

� Customer Services network through numerous and experienced service stations thanks to large Ecureuilfleet (nearly 4000 A/C) flying all over the world.

Maintenance and maintainability data

"Scheduled" and "unscheduled" maintenance are considered in manhour figures given hereafter.

Scheduled maintenance

� Possibility to perform maintenance tasks according to each operator needs :

� blocked whole inspection (helicopter unavailable during all the inspection duration),

or

� “splitted” inspection (helicopter available for flight since the inspection is performed in severalbatches of maintenance operations, in respect with the limitations and periodicities defined in theMaster Servicing Recommendation).

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 50This 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

Estimated Mean Man Hour per Flying Hour (MMH/FH)(standard aircraft - 300 Flying hour/year – 2 flights per day)

0.80 MMH/FH 1 (Scheduled + unscheduled + SB implementation)

Detail

� Basic

� Daily checks : Pilot’s task

� 100 flight hrs periodicity tasksIncluding average “corrective” works 4.3 MMH 2

� 500 flight hrs or 24 months periodicity tasksIncluding average “corrective” works 148 MMH

� Unscheduled (reliability cause) 0.32 MMH/FH

� SB implementation 0.05 MMH/FH

� 12 years inspections requiring 335 MMH

1 MMH/FH : Mean Man Hour per Flight Hour.2 MMH : Mean Man Hour.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 51This 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

Time Between Overhaul (TBO)/Service Life Limit (SLL)

Major assemblies TBO (h) SLL (h)

Main Blade 20 000Rear Blade 4 000MGB Epicyclic reduction gear box 3000

Reduction gear tapered 3000Oil pump 3500

Complete engine 2500TGB 2700Main servo-unit (TRW type) 3000Tail servo-unit (TRW type) 3000

Documentation

Eurocopter AS 355 N technical documentation, pleasant and easy to consult, is basically supplied :

� On an Interactive Electronic Support (CD-ROM OPEN 355), provided free of charge, with a twice ayear update, that includes the whole documentation : Operating (except Flight Manual), Maintenance,Identification and Specific documents.

The CD-ROM product presents great advantages such as :

� More efficiency in maintenance thanks to :

� Direct and instantaneous access to manuals and data by "hypertext" navigation� Easy search by keywords and multiple criteria� Highly portable technical publications in an extremely compact format

� Quick updating without insertion mistake risk.

and

� On paper- Flight Manual- Other documents : Master Servicing Recommendation, Service Bulletins.

Note : 1. As an option , the whole documentation is available on paper.

2. Turbomeca Arrius 1A engine documentation is available both under CD-ROM and paper format.

ECUREUIL AS 355 NTechnical Data

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

355 N 05.101.01 E 52This 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

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