technical data - heli asset

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

AS365 N3

TechnicalData

365 N3 08.101.01 E

DAUPHIN(Civil Version)

PANTHER(Military version)

Utility/armed versionAS 565 UB

AS 365 N3

Technical Data

Naval versionAS 565 MB

AS365 N3

PageTD365N3.pdf 05/05/2008 16:54:45

Technical 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.

365 N3 08.101.01 E 1 This document is the property of EUROCOPTER® ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER® and its contents shall not be disclosed. © EUROCOPTER-2008

Contents

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

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

3 - Baseline Aircraft Definition ..................................................................... 12

4 – Recommended mission configurations ................................................. 15

5 – Optional equipment .................................................................................. 40

6 - Main performance .................................................................................... 44

7 - Customer Service Overview ..................................................................... 63

Manufacturer notice

Attention !

EUROCOPTER, its logo, AS365 N3, DAUPHIN, FENESTRON, STARFLEX, are trade marks of the Eurocopter group. EUROCOPTER’S policy is one of on-going product enhancement which means that alterations in definition, pictures, weights, dimensions or performance may be made at any time without notice being included in those documents that have already been issued. This document cannot thus be taken as an offer or serve as an appendix to a contract without a prior check as to its validity and prior written agreement of EUROCOPTER. The operational or certification regulations, as defined by the local authorities, can make compulsory the installation of some of the equipment or recommended solutions, listed in this document. This list does not claim to cover the whole of the worldwide operational requirements nor the equipment not specifically related to the helicopter (for example: life jacket) or necessary for particular missions (for example: supplemental oxygen). The operator is responsible for ascertaining with his local authorities that the planned configuration of the helicopter complies with regulatory requirements for the area(s) of operations and the type(s) of mission(s) considered.

Technical Data



Blank

Technical Data



1 - Foreword

The AS365 N3 is a medium twin engine helicopter of 4,300 kg Maximum Take-Off Weight that belongs to the famous AS365 family. Over 900 units delivered to date have cumulated more than 4 334 000 flight hours.

The AS365 N3 is a multirole powerful and fast helicopter with outstanding performance and long range capabilities particularly well adapted for operations in high altitude and hot countries thanks to its two Turbomeca ARRIEL 2C turbine engines fitted with Full Authority Digital Engine Control System (FADEC). It has a very large useful volume and will accommodate various seating arrangements up to 12 passengers and 2 crew members in a spacious cabin.

Technical advancements developed by EUROCOPTER on the AS365 N3 include modular design of the mechanical assemblies, use of composite materials (STARFLEX rotor head, blades, airframe, ...) which has led to significant maintenance reduction.

The AS365 N3 also incorporates the new generation, all composite FENESTRON tail rotor that provides high manoeuvrability, exceptional efficiency at all speeds, low noise level and unparallel ground crew safety.

EUROCOPTER improves continuously each helicopter of its range, taking benefit from the field experience of several hundred Customers operating daily worldwide. Since 2006 some significant improvement are implemented in the basic AS365 N3, such as PFD & ND Multifunction Displays replacing the electromechanical instruments, a fuzz burner on engines lubrication system and additional anti corrosion protection. EUROCOPTER knows only too well that the majority of the cost of ownership is incurred over the operational life of the helicopter. Indeed, as much as 60 % of the life cycle costs occur during the in-service phase. For this reason, reliability, maintainability and supportability are the cornerstones of the design of all EUROCOPTER products.

The basic AS365 N3 vehicle design is based on the concept of Reliability Centered Maintenance and, as such, embodies a modern concept of dynamic assemblies and systems, use of composite materials, redundant systems and unlimited service life of main components.

The AS365 N3 possesses “designed-in maintainability” with numerous interchangeable parts that can be replaced quickly to ease maintenance and reduce down time. The main components (engines, main rotor head, main gearbox) have a modular design and are directly accessible, with minimum requirements to remove other components of the aircraft.

Technical Data



Blank

Technical Data



2 - General Characteristics

Layout

Crew

single / dual-pilot VFR single / dual-pilot IFR

Passenger transport up to 12 passengers with comfort seats

VIP up to 7 passengers with VIP layout

Corporate up to 8 passengers with Executive layout

Casualty transport

up to 2 stretcher-patients and 4 seats up to 4 NATO stretcher-patients and 1 attendant

seat

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

Empty weight, baseline aircraft definition (including engine oil and unusable fuel) 2,411 5,315

Maximum all-up weight 4,300 9,480 Maximum cargo-sling load 1,600 3,527 Maximum all-up weight in external load configuration 4,300 9,480

Power plant: 2 Turbomeca ARRIEL 2C free turbine engines Note: Thermal power, ISA, Sea Level kW ch shp

O.E.I. 30 seconds rating 717 974 961 OE.I. 2 minutes rating 645 876 865 Continuous O.E.I. rating 622 845 834 Take-Off Power 625 849 838 Maximum Continuous Power 580 788 778

Usable Fuel capacities litres US gal. kg lb

Standard fuel tanks (2 groups) 1,135 300 897 1,977 Additional fuel tanks

Auxiliary fuel tank 180 47 142 313 6th fuel tank 112 29.5 89 195 Ferrying fuel tank 475 125 375 827

Technical Data



Main dimensions

Dimensions with blades folded

Technical Data



Dimensions of compartments and doors

Cabin main dimensions

HOLD

Surface 2.25 m2

24.21 sq.ft

Volume 1.10 m3

38.84 cu.ft

CABIN

Surface 4.20 m2

45.20 sq.ft

Volume 5.10 m3

180.10 cu.ft

The cockpit is accessible through

two jettisonable hinged doors. The luggage hold is accessible from the RH side

of the helicopter.

Technical Data



High performance Arriel 2C Power Plant...

1 axial compressor (1) 1 one-stage centrifugal compressor (2) 1 through-flow annular combustion (3)

chamber with centrifugal fuel injection system 1 single-stage monocristal blade (4)

generator turbine 1 rear bearing (5) 1 single-stage free turbine (6) 1 outlet diffuser (7) 1 reduction gearbox (8) 1 shielding rings for the turbines (9) 1 coupling shaft (10) 1 accessory gearbox (11)

... with modular design, for easier maintenance, blade shedding and FADEC, for increased safety

The ARRIEL 2C is controlled by a Full Authority Digital Engine Control (FADEC), which controls the power turbine constant speed, whatever the power drawn from the engine by continuous accurate adjustment of the gas generator speed. In addition, the FADEC controls some automatic functions (Automatic engine starts / shut-down sequences, acceleration / deceleration control of the engine preventing surge / flame out, in-flight automatic restart and engine maintenance aid), offering the latest safety standards in engine technology.

Technical Data



STARFLEX Main Rotor: reliability and simplicity

With a diameter of 11.94 m (39.17 ft), the main rotor includes a STARFLEX type rotor head and four fibreglass blades rotating clockwise (as viewed from above) at a nominal speed of 349.7 r.p.m. for an engine output speed of 5,990.4 r.p.m. This speed varies between 347 and 365 r.p.m. in flight (except in autorotation flight).

The STARFLEX rotor head combines simplicity and reliability:

very few parts among which the main elements are fibreglass / carbon fiber composite (fail safe design)

no bearing

no lubrication

Main Rotor Blades:

The main rotor blades take benefit of 30 years experience in composite material blades. Immune to scratches and notches, corrosion free and impact resistant they are individually interchangeable and manually foldable.

1 - Blade tip cap 2 - Balancing weights 3 - Stainless steel strip 4 - Glass carbon fibre cloth 5 - Bushings 6 - Tab

7 - Fibreglass-roving spar 8 - Moltoprene filler 9 - Integrated weight 10 - Balancing weight support 11 - Bonding strip

Technical Data



FENESTRON Tail Rotor: safety and discretion The FENESTRON tail rotor provides outstanding characteristics compared to classical tail rotors: safety on ground: with nearly 30 years in operation,

no injury to ground personnel was reported; discretion: the 10 blades are unevenly distributed

around the rotor hub to reduce noise safety in flight: tail fin asymmetrical profile design

provides anti-torque thrust.

Tail Rotor Blades: The 10 rotor carbon fibre composite blades take advantage from Resin Transfer Molding advanced technology. Individually-interchangeable, they have the following characteristics:

Length 0.505 m (1.656 ft) Chord length 0.094 m (0.308 ft) Profile O.A.F. Built-in twist - 10°

Technical Data



Instruments:

(*) optional equipment, to be ordered separately Note: depending on the optional equipment to be installed the instrument panel here above may be organized differently.

Instrument-panel equipment: 2 Collins MFD-255 Primary Flight Displays (PFD) 2 Collins MFD-255 Navigation Displays (ND) 1 stand-by gyro-horizon 1 stand-by altimeter 1 stand-by airspeed indicator 1 dual torquemeter 2 engine T4 indicators 2 engine oil temperature indicators 2 engine oil pressure indicators 2 fuel pressure indicators 2 hydraulic circuit 1 and 2 pressure indicators 1 MGB oil pressure indicator 1 MGB oil temperature indicator 1 voltmeter 1 ammeter 1 dual fuel gauge 2 stopwatches 1 triple tachometer (rotor and engine 1 and 2 free

wheel r.p.m) 1 rotor r.p.m tachometer 2 engine 1 and 2 ΔNg indicators 1 electric and hydraulic power generation control

panel 1 landing gear monitoring and control panel 1 warning panel 3 autopilot galvanometers 2 master alarm warning lights 2 manoeuvring limit (or torque limit, or gas

generator r.p.m deviation limit) warning lights 1 "landing gear not extended" warning light 1 stand-by magnetic compass 1 outside air temperature indicator

Console equipment: 1 AFCS SFIM AP 155 control box 1 fuel circuit control and monitoring panel 1 gyro-magnetic compass control box 1 landing gear brake control handle 1 breaker panel Main overhead panel standard equipment: 1 engine control panel with 2 fire warning lights and 2 dual

fire extinguisher controls for engine bays lighting controls ventilation / heating system controls

Technical Data



3 - AS365 N3 - Baseline Aircraft Definition

Technical Data



Technical Data



Blank

Technical Data



4 - Recommended mission configurations EUROCOPTER proposes the following mission configurations for the AS365 N3. These proposed packages should be regarded as recommended configurations and can be complemented by additional items from the optional equipment list given in chapter 5. Please take note that there may be incompatibilities between optional items of equipment. Any modification and/or complement of the proposed mission configuration must be done with the assistance of a EUROCOPTER sales representative. The AS365 N3 recommended mission configurations are:

Passenger transport Oil & Gas Offshore: this configuration is adapted to Oil and Gas operations and is intended for flight

over water in "hostile environment". Passenger Transport Onshore: this configuration is intended for general passenger transport over

land. VIP

The cabin is fitted with two hinged doors instead of the sliding doors and enhanced sound proofing. 5-seat VIP configuration (2+3)

Two armchairs and a galley are installed in the front part of the cabin and a 3-place divan is installed in the rear part. The cabin is separated from the cockpit by a partition.

6-seat VIP configuration (2+4) Two armchairs and a galley are installed in the front part of the cabin and two 2-place bench-seats are installed in the rear part. The cabin is separated from the cockpit by a partition.

6-seat VIP configuration (4+2) Two 2-place bench-seats are installed in the front part of the cabin and 2 armchairs and a galley are installed in the rear part. The cabin is not separated from the cockpit by a partition.

6-seat VIP Configuration (3+3) Two 3-place divans are installed face-to-face in the cabin. The cabin is not separated from the cockpit by a partition.

4/7-seat VIP Configuration Two 2-place bench-seats are installed in the front part of the cabin and a 3-place divan is installed in the rear part. The cabin is not separated from the cockpit by a partition.

Corporate 7-seat Corporate Configuration (4+3) – hinged doors

The cabin is fitted with two hinged doors instead of the sliding doors and specific sound proofing. Two 2-place bench-seats are installed in the front part of the cabin and one 3-place divan is installed in the rear part.

7-seat Corporate Configuration (4+3) – sliding doors The cabin is fitted with the standard sliding doors and specific sound proofing. Two 2-place bench-seats are installed in the front part of the cabin and one 3-place divan is installed in the rear part.

8-seat Corporate Configuration (4+4) – hinged doors The cabin is fitted with two hinged doors instead of the sliding doors and specific sound proofing. Two 2-place bench-seats are installed in the front part of the cabin and two 2-place bench-seats are installed in the rear part.

8-seat Corporate Configuration (4+4) – sliding doors The cabin is fitted with the standard sliding doors and specific sound proofing. Two 2-place bench-seats are installed in the front part of the cabin and two 2-place bench-seats are installed in the rear part.

Public Services The AS365 N3 being designed for Multipurpose Roles in the most severe environmental conditions, it can be reconfigured easily, without any special tools for any mission such as Search and Rescue, Police, EMS, Fire Fighting, Utility, etc… It is why the AS365 N3 recommended Public Services mission configuration is fitted with Fixed Parts only for optional items of equipment such as hoist, searchlight, sling, hailers and rappelling. Depending on the mission, the aircraft can be fitted with any of the corresponding Removable Parts (see Chapter 5). Very specific equipment such as flir, mission console, EMS equipment, etc… can be provided on request. Please contact a EUROCOPTER sales representative.

Technical Data



4.1 – Oil & Gas Offshore Configuration

Document reference

Commercial reference

Name kg lb

00-10013-A 00-10013-00-CI Baseline Aircraft Definition as per 365 N3 08.100.02 E 2,411 5,315 05-02037-A 05-02037-00-CI Customized external paint – Level 2 1.5 3.3 05-03010-A 05-03010-00-CI First aid kit - JAR OPS 3 compatible 5.0 1.1 05-27005-A 05-27005-00-CI Second fire extinguisher 2.4 5.3 05-31036-A 05-31036-00-CI Front panes in glass instead of plexiglass 10.9 24.0 05-32009-A 05-32009-00-CI Windshield washer 2.8 6.2 05-85009-A 05-85009-00-CI Fuel flowmeter, displayed on GPS Freeflight 2101 I/O Approach + 2.5 5.5 06-21022-A 06-21022-00-FP Goodrich Class 1 electrical Hoist (272 kg - 90 m) - Fixed Parts 3.6 8.0 06-61020-A 06-61020-00-FP Emergency floatation gear with automatic percussion - Fixed parts 14.5 32.0

06-61020-00-RP Emergency floatation gear with automatic percussion - Removable parts 43.1 95.0 06-62026-A 06-62026-00-FP Aerazur life rafts inst. (2 x 10 pax) dual handles, ELT compart, cabin footsteps – Fixed

Parts 4.6 10.1

06-62026-00-RP Aerazur life rafts inst. (2 x 10 pax) dual handles, ELT compart, cabin footsteps – Removable Parts

77.6 171.1

06-66012-A 06-66012-00-CI Helicopter Emergency Egress Lighting (HEEL) 4.0 8.8 06-67012-A 06-67012-00-CI Emergency Locator Transmitter Kannad 406-AP 1 2.4 5.3

06-67041-A 06-67041-00-CI HR Smith series 503 Automatic Deployable Emergency Locator Transmitter (ADELT) 1 7.1 15.7 06-67052-A 06-67052-00-CI Personal Locator Beacon HR Smith PLB 500-12 YF (Qty 2) 1.2 2.6 07-25009-A 07-25009-01-CI 11-seat lay-out with 3 points harnesses instead of standard 8-seat lay-out 10.0 22.0 07-25034-A 07-25034-01-CI 4 points harnesses for 11 standard seat lay-out. 4.3 9.5 00-50021-A 00-50021-00-CI AS365 N3 minimum equipment package 72.4 159.6

Including: VHF-AM Honeywell KTR 908 (n°1) VHF-AM Honeywell KTR 908 (n°2) Inter Communication System TEAM TB 31 with 2 control boxes 1976 Passengers address with 4 loudspeakers NAT AA 20-431 David Clark H 10-13H headset (Qty 2) Thales AHV 16 radio altimeter (displayed on MFD-255) Transponder Honeywell MST-67A with flight ident function (including S mode) 2 ADF Honeywell KDF 806 (displayed on MFD-255) DME Honeywell KDM 706 A - displayed on MFD-255 VOR/ILS/MKR - Honeywell - KNR 634A n°1 (displayed on MFD-255) VOR/ILS/MKR - Honeywell - KNR 634A n°2 (displayed on MFD-255) GPS navigation system FREEFLIGHT 2101 I/O Approach+ Air Data Computer Shadin ADC 2000 Sfim CDV 85 D3 Flight Director Coupler (3 -axis)

08-16015-A 08-16015-00-CI Third control box 1976 in cabin for TEAM TB 31 ICS 3.0 6.6 08-31040-A 08-31040-00-CI Telephonics RDR-1600C weather/search radar (displayed on MFD 255). 14.6 32.2 08-35016-A 08-35016-02-CI EGPWS Honeywell MK XXII displayed on KMD850 (not included). 3.6 7.9 08-35019-A 08-35019-00-CI TCAS Goodrich SKYWATCH HP 899 (displayed on KMD-850 - not included) 10.5 23.1 08-46029-A 08-46029-00-CI Honeywell KMD 850 Jeppesen map 3 3.0 6.6 08-81023-A 08-81023-00-CI Solid State Cockpit Voice & Flight Data Recorder Honeywell AR COMBI (2 hrs CVR

and 10 hrs FDR rec) 4 14.0 30.8

08-83010-A 08-83010-00-CI UMS - complement of SSCVFDR (Usage functions) 1.5 3.3 08-83012-A 08-83012-00-CI HUMS (complement of UMS) (Health functions) 10.5 23.1

1 The Programming Data Sheet must be filled and communicated by the Customer two months at the latest before the helicopter's delivery. 2 The mode S identification must be communicated by the Customer two months at the latest before the delivery. 3 The operational geographic zone of the helicopter must be communicated by the customer two months at the latest before the delivery. 4 Includes an underwater beacon.

Technical Data



Weights / Radius of Action kg lb

Empty weight, Oil & Gas Offshore Configuration (including engine oil, unusable fuel and 2% margin) 2,796 6,164

Pilots (2 x 85 kg, JAR OPS 3) 170 375 Maximum all-up weight 4,300 9,480 Useful load 1,334 2,941 Fuel tanks capacity

Standard fuel tanks 897 1.977 Standard fuel tanks + auxiliary fuel tank 1039 2,291

0

2

4

6

8

10

12

14

0 50 100 150 200Radius of Action (nm)

NB

of P

AX

@ 8

5 kg

Mission profile (Standard Day):- takeoff at Maximum Take Off Weight (Cat. A Clear Area)- outbound flight: climb + cruise at 5000 ft at Best Range Speed- fuel allowance for operation on platform- inbound flight: climb + cruise at 5000 ft at Best Range Speed- reserve: 10 % of the mission fuel + 30 min at Best Endurance Speed, 1500 ft (JAR OPS 3)

(1) (2)Fuel:- (1) Standard fuel tanks- (2) Standard fuel tanks + auxiliary fuel tank

Technical Data



4. 2 – Passenger Transport Onshore Configuration

Document reference


Name kg lb

00-10013-A 00-10013-00-CI Baseline Aircraft Definition as per 365 N3 08.100.02 E 2,411 5,315

05-02037-A 05-02037-00-CI Customized external paint – Level 2 1.5 3.3

05-03010-A 05-03010-00-CI First aid kit - JAR OPS 3 compatible 5.0 1.1

05-27005-A 05-27005-00-CI Second fire extinguisher 2.4 5.3

05-85009-A 05-85009-00-CI Fuel flowmeter, displayed on GPS Freeflight 2101 I/O Approach + 2.5 5.5

06-67012-A 06-67012-00-CI Emergency Locator Transmitter Kannad 406-AP 1 2.4 5.3

07-25009-A 07-25009-01-CI 11-seat lay-out with 3 points harnesses instead of standard 8-seat lay-out 10.0 22.0

00-50021-A 00-50021-00-CI AS365 N3 minimum equipment package 72.4 159.6

Including:

VHF-AM Honeywell KTR 908 (n°1)

VHF-AM Honeywell KTR 908 (n°2)

Inter Communication System TEAM TB 31 with 2 control boxes 1976

Passengers address with 4 loudspeakers NAT AA 20-431

David Clark H 10-13H headset (Qty 2)

Thales AHV 16 radio altimeter (displayed on MFD-255)

Transponder Honeywell MST-67A with flight ident function (including S mode) 2

ADF Honeywell KDF 806 (displayed on MFD-255)

DME Honeywell KDM 706 A - displayed on MFD-255

VOR/ILS/MKR - Honeywell - KNR 634A n°1 (displayed on MFD-255)

VOR/ILS/MKR - Honeywell - KNR 634A n°2 (displayed on MFD-255)

GPS navigation system FREEFLIGHT 2101 I/O Approach+

Air Data Computer Shadin ADC 2000

Sfim CDV 85 D3 Flight Director Coupler (3 -axis)

08-31038-A 08-31038-00-CI Honeywell RDR 2000 weather radar (displayed on KMD-850 - not included) 9.6 21.2

08-35016-A 08-35016-02-CI EGPWS Honeywell MK XXII displayed on KMD850 (not included) 3.6 7.9

08-35019-A 08-35019-00-CI TCAS Goodrich SKYWATCH HP 899 (displayed on KMD-850 - not included) 10.5 23.1

08-46029-A 08-46029-00-CI Honeywell KMD 850 Jeppesen map 3 3.0 6.6

1 The Programming Data Sheet must be filled and communicated by the Customer two months at the latest before the helicopter's delivery. 2 The mode S identification must be communicated by the Customer two months at the latest before the delivery. 3 The operational geographic zone of the helicopter must be communicated by the customer two months at the latest before the delivery.

Technical Data



Weights / Range kg lb

Empty weight, Passenger Transport Onshore Configuration (including engine oil, unusable fuel and 2% margin) 2,585 5,699

Pilots (2 x 85 kg, JAR OPS 3) 170 375 Maximum all-up weight 4,300 9,480 Useful load 1,545 3,406 Fuel tanks capacity

Standard fuel tanks 897 1,977 Standard fuel tanks + auxiliary fuel tank 1,039 2,291

0

200

400

600

800

1000

1200

1400

0 50 100 150 200 250 300 350 400

Range (nm)

Payl

oad

(kg)

Mission profile (Standard Day):- takeoff at Maximum Take Off Weight (Cat. A Clear Area)- climb + cruise at 5000 ft at Best Range Speed- reserve: 30 min at Best Endurance Speed, 1500 ft Fuel:- (1) Standard fuel tanks- (2) Standard fuel tanks + auxiliary fuel tank

(1) (2)

Technical Data



4.3 – 5-seat VIP Configuration with galley and partition (2+3) Document reference


Name kg lb

00-10013-A 00-10013-00-CI Baseline Aircraft Definition as per 365 N3 08.100.02 E 2,411 5,315 05-02037-A 05-02037-00-CI Customized external paint – Level 2 1.5 3.3 05-31038-A 05-31038-00-CI Green tinted plexiglass panes (cabin only) 0.0 0.0 05-42026-A 05-42026-00-CI Air conditioning system (split) 45.4 100.1 05-85009-A 05-85009-00-CI Fuel flowmeter, displayed on GPS Freeflight 2101 I/O Approach + 2.5 5.5 06-41002-A 06-41002-00-CI Under fuselage anti-collision strobe light 1.5 3.3 06-67012-A 06-67012-02-CI Emergency Locator Transmitter Kannad 406-AP 1 with GPS connection 3.1 6.8

07-50010-A 07-50010-00-CI 2 hinged passengers doors with 2 rear doors extensions (instead of the standard sliding doors)

12.0 26.5

07-81001-A 07-81001-00-CI 5-seat VIP installation with galley and partition (2+3) 240.5 530.2 00-50021-A 00-50021-00-CI AS365 N3 minimum equipment package 72.8 160.5

Including:

VHF-AM Honeywell KTR 908 (n°1) VHF-AM Honeywell KTR 908 (n°2) Inter Communication System TEAM TB 31 with 2 control boxes 1976 Passengers address with 4 loudspeakers NAT AA 20-431 David Clark H 10-13H headset (Qty 2) Thales AHV 16 radio altimeter (displayed on MFD-255) Transponder Honeywell MST-67A with flight ident function (including S

mode) 2

ADF Honeywell KDF 806 (displayed on MFD-255) DME Honeywell KDM 706 A - displayed on MFD-255 VOR/ILS/MKR - Honeywell - KNR 634A n°1 (displayed on MFD-255) VOR/ILS/MKR - Honeywell - KNR 634A n°2 (displayed on MFD-255) GPS navigation system FREEFLIGHT 2101 I/O Approach+ Air Data Computer Shadin ADC 2000 Sfim CDV 85 D3 Flight Director Coupler (3 -axis)

08-17015-A 08-17015-01-CI Passenger interphone TEAM BA 1920 (for VIP installation) 1.6 3.5 08-17016-A 08-17016-00-CI Passenger interphone for active noise cancelling headsets 1 x NAT AA-36 + 2

x NAT AA-82 1.8 4.0

08-18029-A 08-18029-00-CI Bose Aviation X active noise cancelling headset (qty 5) 2.5 5.5 08-18041-A 08-18041-00-CI Two additional ICS jacks in cockpit for Bose Aviation X headsets (headsets

excluded) 0.1 0.2

08-31038-A 08-31038-00-CI Honeywell RDR 2000 weather radar (displayed on KMD-850 - not included) 9.6 21.2 08-35016-A 08-35016-02-CI EGPWS Honeywell MK XXII displayed on KMD850 (not included). 3.6 7.9 08-35019-A 08-35019-00-CI TCAS Goodrich SKYWATCH HP 899 (displayed on KMD-850 - not included) 10.5 23.1 08-46029-A 08-46029-00-CI Honeywell KMD 850 Jeppesen map 3 3.0 6.6 08-81023-A 08-81023-00-CI Solid State Cockpit Voice & Flight Data Recorder Honeywell AR COMBI (2 hrs

CVR and 10 hrs FDR rec 4) 14.0 30.8

08-83010-A 08-83010-00-CI UMS - complement of SSCVFDR (Usage functions) 1.5 3.3


Technical Data



The AS365 N3 5-seat VIP Configuration (2+3) accommodates up to 5 passengers in great comfort conditions.

The cabin is fitted with two hinged doors instead of the sliding doors and specific enhanced sound proofing. A partition fitted with a sliding window isolates the cabin from the cockpit.

Two pivoting armchairs and a galley are installed in the front part of the cabin and one divan, installed in the rear part of the cabin, accommodates comfortably 3 persons.


Empty weight, 5-seat VIP Configuration (2+3) (including engine oil, unusable fuel and 2% margin) 2,895 6,382

Pilots (2 x 85 kg) 170 375 Maximum all-up weight 4,300 9,480 Useful load 1,235 2,723 Fuel tanks capacity

Standard fuel tanks 897 1.977 Standard fuel tanks + auxiliary fuel tank 1,039 2,291

0

2

4

6

8

10

12

14

0 100 200 300 400

Range (nm)

NB

of P

AX

@ 8

0 kg

Mission profile (Standard Day):- takeoff at Maximum Take Off Weight (Cat. A Clear Area)- climb + cruise at 5000 ft at Best Range Speed- reserve: 30 min at Best Endurance Speed, 1500 ftFuel:- (1) Standard fuel tanks- (2) Standard fuel tanks + auxiliary fuel tank

(1) (2)

Technical Data



4.4 – 6-seat VIP Configuration with galley and partition (2+4) Document reference


Name kg lb



12.0 26.5

07-81002-A 07-81002-00-CI 6-seat VIP installation with galley and partition (2+4) 230.5 508.2 00-50021-A 00-50021-00-CI AS365 N3 minimum equipment package 72.8 160.5

Including:


mode) 2



x NAT AA-82 1.8 4.0


excluded) 0.1 0.2





Technical Data




The cabin is fitted with two hinged doors instead of the sliding doors and specific enhanced sound proofing. A partition fitted with a sliding window isolates the cabin from the cockpit.

Two pivoting armchairs and a galley are installed in the front part of the cabin. One divan, installed in the rear part of the cabin, accommodates comfortably 4 persons.


Empty weight, 6 seat VIP (2+4) Configuration (including engine oil, unusable fuel and 2% margin) 2,886 6,362



0

2

4

6

8

10

12

14

0 100 200 300 400

Range (nm)

NB

of P

AX

@ 8

0 kg


(1) (2)

Technical Data



4.5 – 6-seat VIP Configuration with galley and without partition (4+2) Document reference


Name kg lb



12.0 26.5

07-81046-A 07-81046-00-CI 6-seat VIP installation with galley and without partition (4+2) 225.6 497.4 00-50021-A 00-50021-00-CI AS365 N3 minimum equipment package 72.8 160.5

Including:


mode) 2



x NAT AA-82 1.8 4.0


excluded) 0.1 0.2





Technical Data




The cabin is fitted with two hinged doors instead of the sliding doors and specific enhanced sound proofing. There is no partition between the cabin and the cockpit.

Two 2-place bench-seats are installed in the front part of the cabin and two armchairs and a galley are installed in the rear part.

As an option, the galley can be equipped with an in-flight entertainment system.





0

2

4

6

8

10

12

14

0 100 200 300 400

Range (nm)

NB

of P

AX

@ 8

0 kg


(1) (2)

Technical Data



4.6 – 6-seat VIP Configuration (3+3) Document reference


Name kg lb



12.0 26.5

07-81019-A 07-81019-00-CI 6-seat VIP installation (3+3) 224.0 493.8 00-50021-A 00-50021-00-CI AS365 N3 minimum equipment package 72.8 160.5

Including:


mode) 2


08-17016-A 08-17016-00-CI Passenger interphone for active noise cancelling headsets 1 x NAT AA-36 + 2 x NAT AA-82

1.8 4.0


excluded) 0.1 0.2





Technical Data




The cabin is fitted with two hinged doors instead of the sliding doors and specific enhanced sound proofing. There is no partition between the cabin and the cockpit.

Two 3-place divans are installed face-to-face in the cabin.





0

2

4

6

8

10

12

14

0 100 200 300 400

Range (nm)

NB

of P

AX

@ 8

0 kg


(1) (2)

Technical Data



4.7 – 7-seat VIP Configuration (4+3) Document reference


Name kg lb



12.0 26.5

07-81003-A 07-81003-00-CI 7-seat VIP installation (4+3) 186.6 411.4 00-50021-A 00-50021-00-CI AS365 N3 minimum equipment package 72.8 160.5

Including:


mode) 2



1.8 4.0


excluded) 0.1 0.2





Technical Data




The cabin is fitted with two hinged doors instead of the sliding doors and specific enhanced sound proofing. There is no partition between the cabin and the cockpit. Two 2-place bench-seats are installed in the front part of the cabin and one 3-place divan is installed in the rear part.





0

2

4

6

8

10

12

14

16

0 100 200 300 400Range (nm)

NB

of P

AX

@ 8

0 kg


(1) (2)

Technical Data



4.8 – 7-seat Corporate Configuration (4+3) – for hinged doors Document reference


Name kg lb

00-10013-A 00-10013-00-CI Baseline Aircraft Definition as per 365 N3 08.100.02 E 2,411 5,315 05-02037-A 05-02037-00-CI Customized external paint – Level 2 1.5 3.3 05-31038-A 05-31038-00-CI Green tinted plexiglass panes (cabin only) 0.0 0.0 05-42026-A 05-42026-00-CI Air conditioning system (split) 45.4 100.1 05-85009-A 05-85009-00-CI Fuel flowmeter, displayed on GPS Freeflight 2101 I/O Approach + 2.5 5.5 06-41002-A 06-41002-00-CI Under fuselage anti-collision strobe light 1.5 3.3 06-67012-A 06-67012-00-CI Emergency locator Transmitter Kannad 406-AP 1 2.4 5.3

07-25060-A 07-25060-00-CI 7-seat Corporate installation (4+3) – for hinged doors 96.5 212.7 07-50010-A 07-50010-00-CI 2 hinged passengers doors with 2 rear doors extensions (instead of the

standard sliding doors) 12.0 26.5


Including:


mode) 2



1.8 4.0


excluded) 0.1 0.2





Technical Data



The AS365 N3 7-seat Corporate configuration (4+3) accommodates up to 7 passengers in excellent comfort conditions.

The cabin is fitted with two hinged doors instead of the sliding doors and improved sound proofing. There is no partition between the cabin and the cockpit. Two 2-place bench-seats are installed in the front part of the cabin and one 3-place divan is installed in the rear part.


Empty weight, 7 seat Corporate (4+3) Configuration (including engine oil, unusable fuel and 2% margin) 2,748 6,058



0

2

4

6

8

10

12

14

16

0 100 200 300 400Range (nm)

NB

of P

AX

@ 8

0 kg


(1) (2)

Technical Data



4.9 – 7-seat Corporate Configuration (4+3) – for sliding doors Document reference


Name kg lb


07-25061-A 07-25061-00-CI 7-seat Corporate installation (4+3) – for sliding doors 96.5 212.7 00-50021-A 00-50021-00-CI AS365 N3 minimum equipment package 72.8 160.5

Including:


mode) 2



1.8 4.0


excluded) 0.1 0.2





Technical Data



The AS365 N3 7-seat Corporate configuration (4+3) accommodates up to 7 passengers in excellent comfort conditions.

The cabin is fitted with the standard sliding doors and improved sound proofing. There is no partition between the cabin and the cockpit. Two 2-place bench-seats are installed in the front part of the cabin and one 3-place divan is installed in the rear part.





0

2

4

6

8

10

12

14

16

0 100 200 300 400Range (nm)

NB

of P

AX

@ 8

0 kg


(1) (2)

Technical Data



4.10 – 8-seat Corporate Configuration (4+4) – for hinged doors Document reference


Name kg lb


07-25011-A 07-25011-00-CI 8-seat Corporate installation (4+4) – for hinged doors 84.5 186.3 07-50010-A 07-50010-00-CI 2 hinged passengers doors with 2 rear doors extensions (instead of the



Including:


mode) 2



1.8 4.0


excluded) 0.1 0.2





Technical Data



The AS365 N3 8-seat Corporate Configuration (4+4) accommodates up to 8 passengers in excellent comfort conditions.

The cabin is fitted with two hinged doors instead of the sliding doors and specific sound proofing.

Two 2-place bench-seats are installed in the front part of the cabin and two 2-place bench-seats are installed in the rear part.





0

2

4

6

8

10

12

14

16

0 100 200 300 400Range (nm)

NB

of P

AX

@ 8

0 kg


(1) (2)

Technical Data



4.11 – 8-seat Corporate Configuration (4+4) – for sliding doors Document reference


Name kg lb


07-25052-A 07-25052-00-CI 8-seat Corporate installation (4+4) – for sliding doors 84.5 186.3 00-50021-A 00-50021-00-CI AS365 N3 minimum equipment package 72.8 160.5

Including:


mode) 2



1.8 4.0


excluded) 0.1 0.2





Technical Data



The AS365 N3 8-seat Corporate Configuration (4+4) accommodates up to 8 passengers in excellent comfort conditions.

The cabin is fitted with the standard sliding doors and specific sound proofing.

Two 2-place bench-seats are installed in the front part of the cabin and two 2-place bench-seats are installed in the rear part.





0

2

4

6

8

10

12

14

16

0 100 200 300 400Range (nm)

NB

of P

AX

@ 8

0 kg


(1) (2)

Technical Data



4.12 - Public services mission Configuration

Document reference


Name kg lb

00-10013-A 00-10013-00-CI Baseline Aircraft Definition as per 365 N3 08.100.02 E 2,411 5,315 05-02037-A 05-02037-00-CI Customized external paint – Level 2 1.5 3.3 05-31008-A 05-31009-A

05-31008-00-CI 05-31009-00-CI

Sliding window on the enlarged and bubble sliding door - RH Side Sliding window on the enlarged and bubble sliding door- LH Side

1.0 1.0

2.2 2.2

05-85009-A 05-85009-00-CI Fuel flowmeter, displayed on GPS Freeflight 2101 I/O Approach + 2.5 5.5 06-21022-A 06-21022-00-FP Goodrich Class 1 electrical Hoist (272 kg - 90 m) - Fixed Parts 3.6 8.0 06-24002-A 06-24002-00-FP Rappelling (ropes are not included) - Fixed Parts 3.3 7.3 06-27010-A 06-27010-00-FP Cargo sling with dynamometer and external mirrors

(1,600 kg - 3,527 lb) - Fixed Parts 8.6 19.0

06-31009-A 06-31009-00-FP Electrical hailer with siren system - Fixed Parts 7.0 15.4 06-45009-A 06-45009-00-FP SPECTROLAB SX-16 search light - Fixed parts 4.8 10.6

06-67012-A 06-67012-00-CI Emergency locator Transmitter Kannad 406-AP 1 2.4 5.3

07-71015-A 07-71015-00-FP Casualty-carrying installation for 4 stretchers (excluding stretchers) - Fixed Parts 1.8 4.0 00-50021-A 00-50021-00-CI AS365 N3 minimum equipment package 72.8 160.5

Including: VHF-AM Honeywell KTR 908 (n°1) VHF-AM Honeywell KTR 908 (n°2) Inter Communication System TEAM TB 31 with 2 control boxes 1976 Passengers address with 4 loudspeakers NAT AA 20-431 David Clark H 10-13H headset (Qty 2) Thales AHV 16 radio altimeter (displayed on MFD-255) Transponder Honeywell MST-67A with flight ident function (including S mode) 2


08-16015-A 08-16015-00-CI Third control box 1976 in cabin for TEAM TB 31 ICS 3.0 6.6 08-31038-A 08-31038-00-CI Honeywell RDR 2000 weather radar (displayed on KMD-850 - not included) 9.6 21.2 08-35016-A 08-35016-02-CI EGPWS Honeywell MK XXII displayed on KMD850 (not included). 3.6 7.9 08-35019-A 08-35019-00-CI TCAS Goodrich SKYWATCH HP 899 (displayed on KMD-850 - not included) 10.5 23.1 08-46029-A 08-46029-00-CI Honeywell KMD 850 Jeppesen map 3 3.0 6.6

1 The Programming Data Sheet must be filled and communicated by the Customer two months at the latest before the helicopter's delivery. 2 The mode S identification must be communicated by the Customer two months at the latest before the delivery. 3 The operational geographic zone of the helicopter must be communicated by the customer two months at the latest before the delivery.

Technical Data



The AS365 N3 recommended Public Services mission configuration is fitted with Fixed Parts only for optional items of equipment such as hoist, searchlight, sling, hailers and rappelling. Depending on the mission, the aircraft can be fitted with any of the corresponding Removable Parts (see Chapter 5). Very specific equipment such as flir, mission console, EMS equipment, etc… can be provided on request. Please contact a EUROCOPTER sales representative.

Weights kg lb

Empty weight, public Service Configuration (including engine oil, unusable fuel and 2% margin) 2,602 5,736


Standard fuel tanks 897 1.977 Standard fuel tanks + auxiliary fuel tank 1039 2,291

0

200

400

600

800

1000

1200

1400

0 100 200 300 400Range (nm)

Payl

oad

(kg)


(1) (2)

Technical Data



5 - Optional equipment The following list presents the main optional items of equipment which may be added to customize the recommended configurations or to build specific configurations. For peculiar applications, specific items of equipment are also available upon request. Please take note that there may be incompatibilities between optional items of equipment. Any modification and/or complement of the proposed mission configuration must be done with the assistance of a EUROCOPTER sales representative.

Document reference


Name kg lb

Minimum Equipment Package 00-50021-A 00-50021-00-CI AS365 N3 Minimum Equipment Package 1 72.8 160.5 VHF-AM Honeywell KTR 908 (No.1) VHF-AM Honeywell KTR 908 (No.2) Inter Communication System Team TB 31 with 2 control boxes 1976 Passengers address with 4 loudspeakers NAT AA 20-431 David Clark H 10-13H headset (Qty 2) Radio altimeter Thales AHV 16 (displayed on MFD-255) Transponder Honeywell MST-67A with flight ident function (including S mode) 2 ADF Honeywell KDF 806 (displayed on MFD-255) DME Honeywell KDM 706 A (displayed on MFD-255) VOR/ILS/MKR - Honeywell - KNR 634A n°1 (displayed on MFD-255) VOR/ILS/MKR - Honeywell - KNR 634A n°2 (displayed on MFD-255) GPS navigation system 3 Freeflight 2101 I/O Approach+ Air Data Computer Shadin ADC 2000 Flight Director Coupler (3-axis) Sfim CDV 85 D3 General Equipment 05-01004-A 05-01004-00-CI FAA certification kit 0 0 05-02011-A 05-02011-00-CI Customized external paint (level 1) 1.5 3.3 05-02037-A 05-02037-00-CI Customized external paint (level 2) 1.5 3.3 05-03010-A 05-03010-00-CI First aid kit – JAR OPS 3 compatible 5.0 11.0 05-21008-A 05-21008-00-CI Wire strike protection system (upper cutter) 7.5 16.5 05-24006-A 05-24006-00-CI High visibility markings of main rotor blades 0.3 0.7 05-24007-A 05-24007-00-CI High visibility markings of main rotor blades tip caps 0.15 0.3 05-25009-A 05-25009-00-FP Sand prevention filters, dynamic type - Fixed Parts 4 2.8 6.2 05-25009-00-RP Sand prevention filters, dynamic type - Removable Parts 4 11.0 24.3 05-25011-A 05-25011-00-CI Re-inforced sand erosion protection strip on main rotor blades 0.4 0.9 05-25020-A 05-25020-00-CI Re-inforced sand erosion protection strip on tail rotor blades 0.1 0.2 05-26014-A 05-26014-00-CI Enhanced anti-corrosion protection 3.5 7.7 05-26017-A 05-26017-00-CI Dynol protection tbd tbd 05-27005-A 05-27005-00-CI Second fire extinguisher 2.4 5.3 05-31008-A 05-31008-00-CI Sliding window on the enlarged bubble sliding door - RH side 1.0 2.2 05-31009-A 05-31009-00-CI Sliding window on the enlarged bubble sliding door - LH side 1.0 2.2

1 In addition to this package a beacon must be selected in the possible optional equipment (ELT or/and ADELT). 2 The mode S identification must be communicated by the customer two months at the latest before the delivery. 3 The customer must take out a subscription to the data base in order to use the GPS after having taken delivery of the helicopter. 4 Includes the supply of the standard cowlings.

Technical Data



Document reference


Name kg lb

05-31036-A 05-31036-00-CI Front panes in glass instead of plexiglass 10.9 24.0 05-31038-A 05-31038-00-CI Green tinted plexiglass panes (cabin only) 0 0 05-31090-A 05-31090-00-CI Limousine panes in the cabin (for hinged cabin door configuration) 0 0 05-32009-A 05-32009-00-CI Windshield washer 2.8 6.2 05-42023-A 05-42023-00-CI Air conditioning system (compact) 56.0 123.5 05-42026-A 05-42026-00-CI Air conditioning system (split) 45.4 100.1 05-51004-A 05-51004-00-CI Heated windshield 1.3 2.9 05-52009-A 05-52009-00-CI Icing detector (Rosemount) 1.1 2.4 05-62013-A 05-62013-00-CI 10-kVA A.C. alternator 27.8 61.3 05-81018-A 05-81018-00-FP Auxiliary fuel tank in the hold (180 litres - 47 US gal.) -

Fixed Parts 3.9 8.6

05-81018-00-RP Auxiliary fuel tank in the hold (180 litres - 47 US gal.) - Removable Parts 23.7 52.2 05-81036-A 05-81036-00-CI 6th fuel tank 9.0 19.9 05-81039-A 05-81039-00-CI Reinforced skin fuel tanks 21.8 48.1 05-82021-A 05-82021-00-FP Fuel jettison system - Fixed Parts 1.9 4.2 05-82021-00-RP Fuel jettison system - Removable Parts 4.7 10.4 05-84003-A 05-84003-00-CI Ferrying tank (475 litres - 125 US gal.) 1 26.5 58.4 05-85009-A 05-85009-00-CI Fuel flowmeter displayed on GPS Freeflight 2101 I/O Approach + 2.5 5.5 Specific Mission Equipment 06-21022-A 06-21022-00-FP Goodrich Class 1 electrical hoist (272 kg - 90 m) -

Fixed Parts 3.6 8.0

06-21022-00-RP Goodrich Class 1 electrical hoist (272 kg - 90 m) - Removable Parts

67.6 149.0

06-24002-A 06-24002-00-FP Rappelling (ropes are not included) - Fixed Parts 3.3 7.3 06-24002-00-RP Rappelling (ropes are not included) - Removable Parts 2.6 5.7 06-27010-A 06-27010-00-FP Cargo sling with dynamometer and external mirrors

(1,600 kg - 3,527 lb) - Fixed Parts 8.6 19.0

06-27010-00-RP Cargo sling with dynamometer and external mirrors (1,600 kg - 3,527 lb) - Removable Parts

19.0 41.9

06-27010-01-FP Cargo sling with dynamometer & ext. mirrors (1,600 kg), ext liferaft compatible - Fixed Parts

4.6 10.1

06-27010-01-RP Cargo sling with dynamometer & ext. mirrors (1,600 kg), ext liferaft compatible - Removable Parts

19 41.9

06-31009-A 06-31009-00-FP Electrical hailer with siren system - Fixed Parts 7.0 15.4 06-31009-00-RP Electrical hailer with siren system - Removable Parts 11.0 24.3 06-41002-A 06-41002-00-CI Under fuselage anti-collision strobe light 1.5 3.3 06-41009-A 06-41009-00-CI Tail fin anti-collision strobe light 0.2 0.4 06-45009-A 06-45009-00-FP Spectrolab SX-16 searchlight - Fixed Parts 4.8 10.6 06-45009-00-RP Spectrolab SX-16 searchlight - Removable Parts 31.5 69.5 06-45034-A 06-45034-00-FP Spectrolab SX-5 searchlight - Fixed Parts 4.8 10.6 06-45034-00-RP Spectrolab SX-5 searchlight - Removable Parts 25.0 55.1 06-61020-A 06-61020-00-FP Emergency floatation gear with automatic percussion -

Fixed Parts 14.5 32.0

06-61020-00-RP Emergency floatation gear with automatic percussion - Removable Parts 43.1 95.0 06-62002-A 06-62002-00-FP Aerazur life-raft installation (2 x 10 pax) in cabin ceiling - Fixed Parts 2 -1.7 -3.7 06-62002-00-RP Aerazur life-raft installation (2 x 10 pax) in cabin ceiling - Removable Parts 2 63.6 140.2 06-62017-A 06-62017-00-FP Aerazur external life raft installation (2 x 10 pax), with dual handle, including

cabin footsteps - Fixed Parts 4.6 10.1

06-62017-00-RP Aerazur external life raft installation (2 x 10 pax), with dual handle, including cabin footsteps - Removable Parts

77.6 171.1

1 It is forbidden to transport pax in cabin when ferrying tank is installed. 2 Deliverable with standard upholstery.

Technical Data



Document reference


Name kg lb

06-62026-A 06-62026-00-FP Aerazur life rafts inst. (2 x 10 pax) dual handles, ELT compart, cabin footsteps - Fixed Parts

4.6 10.1

06-62026-00-RP Aerazur life rafts inst. (2 x 10 pax) dual handles, ELT compart, cabin footsteps - Removable Parts

77.6 171.1

06-66012-A 06-66012-00-CI Helicopter Emergency Egress Lighting (HEEL) 4.0 8.8 06-67012-A 06-67012-00-CI Emergency Locator Transmitter Kannad 406-AP 1 2.4 5.3 06-67012-02-CI Emergency Locator Transmitter Kannad 406-AP with GPS connection 1 3.1 6.8 06-67041-A 06-67041-00-CI HR Smith series 503 Automatic Deployable Emergency Locator Transmitter

(ADELT) 1 7.1 15.7

06-67052-A 06-67052-00-CI Personal Locator Beacon HR Smith PLB 500-12 YF 0.6 1.3 06-68009-A 06-68009-00-CI Under Water Acoustic Beacon Dukane DK 120 0.4 0.9 06-69004-A 06-69004-00-CI Automatic Voice Alarm Device Thales Avionics V 694 2.3 5.1 06-81008-A 06-81008-00-FP Fire-fighting "Bambi Bucket" (910 litres) - Fixed Parts 4.0 7.1 06-81008-00-RP Fire-fighting "Bambi Bucket" (910 litres)- Removable Parts 61.0 113.8 Interior Layout 07-15001-A 07-15001-00-CI Pilot and co-pilot "energy absorber" seats Fisher H110 instead of pilot and co-

pilot standard seats 16.0 35.3

07-25002-A 07-25002-00-CI 12-seat layout complement with 4-point harnesses 16.0 35.3 07-25002-01-CI 12-seat layout with 4-point harnesses instead of standard 8-seat layout 16.0 35.3 07-25009-A 07-25009-00-CI 11-seat layout complement with 3-point harnesses 10.0 22.0 07-25009-01-CI 11-seat layout with 3-point harnesses instead of standard 8-seat layout 10.0 22.0 07-25011-A 07-25011-00-CI 8-seat Corporate installation (4+4) – for hinged doors 185.7 409.4 07-25033-A 07-25033-00-CI 4 points harnesses for 8 standard seats layout 3.1 6.8 07-25034-A 07-25034-00-CI 4 points harnesses for 11 standard seat layout complement 2.7 6.0 07-25034-01-CI 4 points harnesses for 11 standard seat layout 4.3 9.5 07-25052-A 07-25052-00-CI 8-seat Corporate installation (4+4) – for sliding doors 185.7 409.4 07-25060-A 07-25060-00-CI 7-seat Corporate installation (4+3) – for hinged doors 201.6 444.4 07-25061-A 07-25061-00-CI 7-seat Corporate installation (4+3) – for sliding doors 201.6 444.4 07-30003-A 07-30003-00-CI Comfort upholstery with improved sound-proofing and carpeting 57.0 125.7 07-50010-A 07-50010-00-CI 2 hinged passengers doors with 2 rear doors extensions (instead of the


07-50038-A 07-50038-00-CI LH sliding door opening extension (on ground) 2 1.7 3.8

07-71015-A 07-71015-00-FP Casualty-carrying installation for 4 stretchers (excluding stretchers) - Fixed

Parts 3 1.8 4.0

07-71015-00-RP Casualty-carrying installation for 4 stretchers (excluding stretchers) - Removable Parts 3

9.5 20.9

07-74004-A 07-74004-00-CI Stretchers for "Casualty-carrying installation for 4 stretchers" (Qty 4) 4 9.3 20.5 07-81001-A 07-81001-00-CI 5-seat VIP installation with galley and partition (2+3) 240.5 530.2 07-81002-A 07-81002-00-CI 6-seat VIP installation with galley and partition (2+4) 230.5 508.2 07-81003-A 07-81003-00-CI 7-seat VIP installation (4+3) 186.6 411.4 07-81019-A 07-81019-00-CI 6-seat VIP installation (3+3) 224.0 493.8 07-81046-A 07-81046-00-CI 6-seat VIP installation with galley and without partition (4+2) 225.6 497.4 07-82005-A 07-82005-00-CI Headrest (Qty 8) 5 & floor inserts for 8-seat face-to-face installation 4.0 8.8 07-82005-A 07-82005-01-CI Headrest (Qty 8) 2.8 6.2 07-82005-02-CI Headrest (Qty 7) 2.5 5.4 07-91003-A 07-91003-00-CI Gold finishing of cabin visible metallic parts 0 0

1 The Programming Data Sheet must be filled and communicated by the customer two months at the latest before the helicopter's

delivery. 2 Ground Support equipment. The maximum extension of the LH sliding door can be performed on ground only. 3 The corresponding stretchers are not certified. 4 Not certified equipment. 5 Mandatory for seats facing backwards.

Technical Data



Avionics 08-10001-A 08-10001-00-CI HF/SSB Collins HF 9000 23.0 50.7 08-12011-A 08-12011-00-CI VHF/FM Maritime NAT NPX 138 n°1 2.5 5.5 08-14010-A 08-14010-00-CI V/UHF/AM/FM Chelton-Wulfsberg - RT-5000 14.0 30.9 08-15516-A 08-15516-00-CI IRIDIUM satellite phone Aerodata (voice only) tbd tbd 08-16015-A 08-16015-00-CI Third control box 1976 in cabin for Team TB 31 ICS 3.0 6.6 08-16019-A 08-16019-00-CI Fourth control box 1976 for Team TB 31 ICS 3.0 6.6 08-17015-A 08-17015-00-CI Passenger interphone Team BA 1920 (for 8 passengers) 1.3 2.9 08-17015-A 08-17015-01-CI Passenger interphone Team BA 1920 (for VIP installation) 1.6 3.5 08-17016-A 08-17016-00-CI Passenger interphone for active noise cancelling headsets 1 x NAT AA-36 + 2 x

NAT AA-82 1.8 4.0

08-18022-A 08-18022-00-CI Elno FPH 600 helmet (Qty 1)1 1.1 2.4 08-18029-A 08-18029-00-CI Bose Aviation X active noise cancelling headset (Qty 1)1 0.5 1.1 08-18040-A 08-18040-00-CI David Clark H 10-13 H headset (Qty 1)1 0.3 0.6 08-18041-A 08-18041-00-CI Two additional ICS jacks in cockpit for Bose Aviation X headsets (headsets

excluded) 0.1 0.2

08-27017-A 08-27017-00-CI SAR Homer Chelton System 7 4.5 9.9 08-31014-A 08-31014-00-CI Search radar Telephonics RDR 1500 B 44.0 97.0 08-31038-A 08-31038-00-CI Honeywell RDR 2000 weather radar (displayed on KMD-850 - not included) 9.6 21.2 08-31040-A 08-31040-00-CI Telephonics RDR-1600C weather/search radar (displayed on MFD 255) 15.2 33.5 08-35016-A 08-35016-00-CI EGPWS Honeywell MK XXII with dedicated TRA45A indicator 9.0 19.8 08-35016-02-CI EGPWS Honeywell MK XXII displayed on KMD850 (not included) 3.6 7.9 08-35019-A 08-35019-00-CI TCAS Goodrich SKYWATCH HP 899 (displayed on KMD-850 - not included) 10.5 23.1 08-38004-A 08-38004-00-CI Goodrich WX1000E Stormscope (displayed on KMD850 - not included) 15.0 33.1 08-46029-A 08-46029-00-CI Honeywell KMD 850 Jeppesen map 2 3.0 6.6 08-65010-A 08-65010-00-CI Skyquest 10,4" display 2.6 5.7 08-81023-A 08-81023-00-CI Solid State Cockpit Voice & Flight Data Recorder Honeywell AR COMBI (2 hrs

CVR and 10 hrs FDR rec) 3 14 30.9

08-83010-A 08-83010-00-CI UMS - complement of SSCVFDR (usage functions) 1.5 3.3 08-83012-A 08-83012-00-CI HUMS - complement of UMS (health functions) 10.5 23.1

1 Quantity to be defined. 2 Includes Digital Jeppesen Map. The operational geographic zone of the helicopter must be communicated by the customer two

months at the latest before the delivery. 3 Includes an underwater beacon.

Technical Data



6 - Main performance The following performance figures and charts are probable average values obtained with new engines. Unless otherwise specified, they are for the aircraft in "clean" configuration in zero wind, sea level, standard atmosphere conditions.

Performance on 2 engine

Gross Weight kg lb

3,750 8,267

4,000 8,818

4,300 9,480

Max. speed, VNE km/hr 306 296 287 kts 165 160 155

Fast cruise speed km/hr 279 274 269 kts 151 148 145

Recommended cruise speed km/hr 276 274 269 kts 149 148 145

Fuel consumption at recommended cruise speed kg/hr 309 313 314 lb/h 681 690 692

Rate-of-climb m/sec. 8.9 7.9 6.7 ft/min. 1,759 1,554 1,321

Hover ceiling I.G.E. at Take-Off Power (6 ft) ISA m 3,900 3,300 2,620

ft 12,795 10,827 8,596 ISA + 20°C m 3,150 2,530 1,810

ft 10,335 8,300 5,938

Hover ceiling O.G.E. at Take-Off Power ISA m 3,110 2,500 1,150

ft 10,203 8,202 3,773 ISA + 20°C m 2,320 1,685 310

ft 7,610 5,527 1,017

Service ceiling (Vz = 0,5 m/sec. – 100 ft/min.) ISA m 5,865 5,290 4,640

ft 19,242 17,355 15,223

Maximum range (without fuel reserve, at recommended cruise speed)

with standard tanks km 827 811 792 n.m 446 438 427

with optional auxiliary tank km 963 945 923 n.m 520 510 498

Maximum endurance [without reserve at 140 km/hr (75 kts)]

with standard tanks hr 4.3 4.2 4.1 with optional auxiliary tank hr 5.0 4.9 4.75

Technical Data



Performance with external load (drag: 1 m2) In external load carrying mission at maximum gross-weight of 4,300 kg - 9,480 lb

Rate of climb 6.1 m/sec. 1,200 ft/min. Performance on 1 engine

Gross Weight kg lb

3,750 8,267

4,000 8,818

4,300 9,480

Rate-of-climb at continuous OEI power m/sec. ft/min.

4.6 905

3.8 748

2.9 570

Service ceiling (0.5 m/sec. - 100 ft/min.) continuous OEI power

m ft

3,125 10,252

2,515 8,259

1,820 5,971

Operating limitations The aircraft is cleared to operate within the following altitude and temperature limitations: (Refer to Flight Manual for complementary information)

Maximum altitude (Standard Atmosphere conditions)

Take-off and landing 4,575 m - 15,000 ft (density-altitude)

Flight 6,096 m - 20,000 ft (pressure-altitude)

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

Minimum temperature - 40° C

Abbreviations IGE: In Ground Effect TOP: Take-Off Power ISA: International Standard Atmosphere VNE: Never Exceed Speed MCP: Maximum Continuous Power VTOL: Vertical Take-Off and Landing OEI: One Engine Inoperative Vtoss: Take-off Safety Speed OGE: Out of Ground Effect Vy: Optimum Climbing Speed SL: Sea Level Vz: Rate-of-Climb TAS: True Airspeed Units nm: nautical miles hr:min: hours:minutes kts: knots Kg: kilograms ft/min: feet/minute lb: pounds m/sec: meters per seconds km: kilometers ° C: degrees Celsius

Technical Data



Blank

Technical Data



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

Take-off weight in hover IGE (6 ft) on 2 engines at Maximum take-off power................................................................................. page 48

Take-off weight in hover OGE

on 2 engines at Maximum take-off power................................................................................. page 49

Maximum Permissible Gross Weight on take-off from clear heliport Category A Vtoss : 65/75 kts – Vy : 75 kts................................................................................................... page 50

Maximum Permissible Gross Weight on take-off from helipad Category A ................................................................................................................................ page 51

Rate of climb in oblique flight on 2 engines at maximum continuous power ISA; T.A.S. = 75 kts ................................................................................................................. page 52

Rate of climb in oblique flight

on 2 engines at maximum continuous power ISA+ 20°C; T.A.S. = 75 kts ..................................................................................................... page 53


on 1 engine OEI unlimited ISA; T.A.S. = 75 kts ................................................................................................................. page 54


on 1 engine OEI unlimited ISA + 20°C; T.A.S. = 75 kts .................................................................................................... page 55

Hourly fuel consumption in level flight

Pressure-altitude = 0 ft, ISA (temperature = 15°C) ................................................................. page 56

Hourly fuel consumption in level flight Pressure-altitude = 5000 ft, ISA (temperature = 5.1°C) .......................................................... page 57

Hourly fuel consumption in level flight Pressure-altitude = 10000 ft, ISA (temperature = -4.8°C) ....................................................... page 58

Hourly fuel consumption in level flight Pressure-altitude = 0 ft, ISA + 20°C (temperature = 35°C) ..................................................... page 59

Hourly fuel consumption in level flight Pressure-altitude = 5000 ft, ISA + 20°C (temperature = 25°C) ............................................... page 60

Hourly fuel consumption in level flight Pressure-altitude = 10000 ft, ISA + 20°C (temperature = 15.2°C) ......................................... page 61

Technical Data



TAKE-OFF WEIGHT IN HOVER I.G.E. (6 ft)

on 2 engines at Maximum Take-Off Power

Technical Data



TAKE-OFF WEIGHT IN HOVER O.G.E.

on 2 engines at Maximum Take-Off Power

Technical Data



MAXIMUM PERMISSIBLE GROSS WEIGHT ON TAKE-OFF FROM CLEAR HELIPORT

Category A

Vtoss: 65/75 kts - Vy: 75 kts

Technical Data



MAXIMUM PERMISSIBLE GROSS WEIGHT ON TAKE-OFF FROM HELIPAD

Category A

Technical Data



RATE OF CLIMB IN OBLIQUE FLIGHT

on 2 engines at Maximum Continuous Power ISA; T.A.S. = 75 kts

Technical Data




on 2 engines at Maximum Continuous Power ISA+20 °C; T.A.S. = 75 kts

Technical Data




on 1 engine OEI unlimited ISA; T.A.S. = 75 kts

Technical Data




on 1 engine OEI unlimited ISA+20°C; T.A.S. = 75 kts

Technical Data



HOURLY FUEL CONSUMPTION IN LEVEL FLIGHT

Pressure-altitude = 0 ft ; ISA (Temperature = 15 °C)

Technical Data




Pressure-altitude = 5000 ft ; ISA (Temperature = 5.1 °C)

Technical Data




Pressure-altitude = 10000 ft ; ISA (Temperature = -4.8 °C)

Technical Data




Pressure-altitude = 0 ft ; ISA + 20 °C (Temperature = 35 °C)

Technical Data




Pressure-altitude = 5000 ft ; ISA+20 °C (Temperature = 25 °C)

Technical Data




Pressure-altitude = 10000 ft ;ISA + 20 °C (Temperature = 15.2 °C)

Technical Data



Blank

Technical Data



7 - Customer Service Overview

Assets

Proven reliability and availability based on experience

EUROCOPTER’s helicopter production programs have developed a strong reputation world-wide for being fully committed to providing customers with operational, capable aircraft that achieve high availability combined with cost-effective support systems. To achieve this record of performance, EUROCOPTER has stressed the importance of working together with its customers to ensure constant feedback on their demonstrated in-service Reliability, Availability and Maintainability/Testability (RAM) data. The main objective is to reach the most optimized operational cost ensuring the highest flight safety. EUROCOPTER has built and delivered DAUPHIN and PANTHER variants for more than twenty years. The combined population of the DAUPHIN & PANTHER family is 775 helicopters in service world-wide. The total flight hours accumulated at the end of 2007 are about 4,334,000 hours. The “lead the fleet” aircraft has accumulated more than 25,000 flight hours.

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 those with longer time intervals.

Scheduled Airframe Inspection Estimated Man Hour

Daily checks: Pilot’s task

50 Flight hrs periodicity tasks

3,45 MMH

600 Flight hrs or 24 months periodicity tasks

150 MMH

Airframe Major Inspection Estimated Man Hour

5,400 Flight hrs or 10 years periodicity tasks

250 MMH

Scheduled Engine Inspection

ARRIEL 2C

Estimated Man Hour

30 flight hrs periodicity tasks



0,0696 MMH per FH

MMH: Mean Man Hour

FH : Flight 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 Maintenance Program (PRE). The announced Man Hours are without incoming flight, work preparation, reworking, servicing, Service Bulletin implementation and unscheduled maintenance.

Technical Data



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

Main Components TBO (hours) SLL (hours)

MAIN ROTOR BLADE 20000

MAIN ROTOR SHAFT ASSEMBLY 3000

MAIN ROTOR HUB (STARFLEX) 1700

MAIN GEARBOX 3000

TAIL ROTOR BLADE 5000

TAIL ROTOR HUB 14500

TAIL GEARBOX 3000

MAIN SERVO UNIT 3000 20000

TAIL SERVO UNIT 3000 20000

ARRIEL 2C 3500

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 Service Life Limited (SLL): The service life limit is an airworthiness limit. The component in question must be removed from service when it reaches the limit indicated.

1 Main component values are given for information purposes only. The reference document is the aircraft Maintenance

Program Manual

Technical Data



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 various user profiles, such as customers:

with a high number of flight hours,

with a low number of flight hours,

looking for immediate component availability,

wishing budget control. To respond to the different customers’ demands EUROCOPTER offers the following flexible and modular services:

Classic Support

Maintenance, Repair and Overhaul

Standard exchange

Guaranteed Direct Maintenance Costs (DMC)

Unscheduled Maintenance Insurance Plan

Parts By the Hour service In addition Eurocopter proposes a specific maintenance support program called Oil & Gas Availability Program (OGAP) to better stick to Oil & Gas Operators needs and constraints. On request, EUROCOPTER is able to propose extensive services adapted to specific mission and customer expectations, as stock and maintenance management. Classic Support The classic support consists of a comprehensive Initial Provisioning package to sustain aircraft operation. This package includes Spare Parts, Tools, Test Equipment, etc... The required level of operational availability determines the quantity and therefore the investment required. With this support package the Customer bears the responsibility to monitor their repair; manage obsolescence and to procure the right mix and quantity of components and spare parts. Maintenance, Repair and Overhaul EUROCOPTER offers a complete range of industry-leading inspection, repair and overhaul capabilities for the full range of EUROCOPTER helicopters, with guaranteed turn-around times and cost-efficiency. Approved by the most stringent airworthiness authorities in the world, our industrial facilities ensure the highest quality for the maintenance, repair and upgrading works. EUROCOPTER Maintenance Repair and Overhaul covers the four major following areas:

Blades Equipment Dynamic component Maintenance & upgrades

Technical Data



Standard Exchange The Standard Exchange consists in replacing a defective part with a serviceable and interchangeable part within 48 hours subject to availability. This service is available for equipment, blades and dynamic components. Guaranteed DMC (Repair By the Hour) The Guaranteed DMC services offers guaranteed repair and overhaul Turn Around Times as well as guaranteed prices. This addition to the classic repair and overhaul enables the customer to best size its inventory. Price for this service is calculated per flight hour, thus enabling the customer to spread and predict both his scheduled as unscheduled maintenance expenses. The guaranteed DMC service is available for dynamic components, blades and basic equipment Unscheduled Maintenance Insurance Plan (UMIP) With the UMIP, EUROCOPTER gives the customer the option to secure unscheduled maintenance costs while remaining responsible for the scheduled events (overhaul, life limited part replacement). Price for this service is calculated per flight hour. The UMIP service includes component unscheduled repairs and guaranteed parts replacement within 24H through Standard Exchange based on a dedicated inventory. This service is available for dynamic components, blades and basic equipment Parts By the Hour (PBH) The Parts by the Hour (PBH) service is a comprehensive program that offers and balances at the same time guaranteed maintenance costs, reduced inventory and minimized helicopter downtime. This service is intended for Customers looking for total cost control and high level of aircraft readiness. Price for this service is calculated per flight hour. The PBH service includes component unscheduled repairs component overhauls as well as Life Limited part replacement. Parts replacement is guaranteed within 24H through Standard Exchange based on a dedicated inventory. This service is available for dynamic components, blades and equipment. Oil & Gas Availability Program (OGAP) One of the strong points of this offer is undoubtedly the Availability Program. This comprehensive program is based on a genuine partnership between the Operator and Eurocopter.

To best adapt to your specific needs, we size dedicated inventories at your premises or locally, and set up dedicated logistic means.

In order to allow you to optimise your fleet management we are committed to operational part availability. To better stick to your expectations and operationnal context, Eurocopter is involved to customize OGAP package.

Technical Data



Engine Maintenance program Always looking to maximize your efficiency and reduce your costs, Turbomeca, the engine manufacturer has developed an improved service offering. Whatever the mission, wherever it may be, for business or pleasure, Turbomeca offers a range of services tailored to various needs. Turbomeca has 32 Repair Centers across the globe, supplemented by several new factory-authorized service facilities strategically located near to you. Turbomeca range of services covers:

• 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 described 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

http://www.turbomeca-support.com/

Technical Data



Training With more than 50 years of experience, the EUROCOPTER training centers provide the most comprehensive, coherent and highest standard helicopter training in the world for pilots and technicians, whether civilian or military. Qualification training, allowing operators to comply with regulatory requirements, and services training, more mission oriented and tailored to the customers’ operational needs, are addressed. All training courses are established according to the relevant civil aviation authorities’ requirements. The centers are approved by the relevant airworthiness authorities (EASA, FAA, DGAC, LBA, CAA…). We are certified ISO 9001: V2000 and regularly audited by independent organisms such as Véritas, AFAQ… EUROCOPTER training centers provide a wide range of courses and services, from basic training up to preparation for the most sophisticated civil and military missions. As part of the full range of services on offer, EUROCOPTER also plays an active role in helicopter pilot development through its Ab Initio programs. Centers are equipped with multimedia classrooms. This includes computers overhead projectors and 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.

AS365 N3 - Example of basic training course

COURSE TYPE COURSE REFERENCE THEORETICAL

INSTRUCTION FLIGHT INSTRUCTION

AS365 N3 Type Rating 8 days 9 1/2 hours Pilots Instructor Pilot Conversion (1) - 5 hours

COURSE TYPE COURSE REFERENCE THEORETICAL & PRACTICAL INSTRUCTION

Mechanics Type Rating (Airframe + engine) 5 weeks

Avionics Type Rating 4 weeks

Blades Maintenance and repair Up to 2 weeks

(1) Pilot already qualified on AS365 (15 hours mini, within last 12 months, not included in type

rating)

TR1: For pilot non already qualified on single engine turbine TR2: For pilot already qualified on single engine turbine.

Note: Length is given as information and depends on pilot or technician qualification or experience. Complementary courses may be required.

Technical Data



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.

http://www.eurocopter.com/services/technical publications/T.I.P.I

http://www.eurocopter.com/services/technical publications/T.I.P.I

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

EC135

135 08.101.01 E

Technical Data

technical data - heli asset

Documents