AS365N3 - Airbus Helicopters

Transcription

AS365 N3
Technical
Data
365 N3 09.101.01 E
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
PageTD365N3.pdf
05/05/2008
16:54:45
AS365 N3
Technical Data
DAUPHIN
(Civil Version)
AS 365 N3
PANTHER
(Military version)
Utility/armed version
Naval version
AS 565 UB
AS 565 MB
Technical Data
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 ...................................................................................... 46
7 - Customer Service Overview....................................................................... 65
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.
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 09.101.01 E
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This document is the property of EUROCOPTER ; no part of it shall be reproduced or transmitted without the express prior written authorization of EUROCOPTER and its contents shall not be disclosed. © EUROCOPTER-2009
Technical Data
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365 N3 09.101.01 E
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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 4,610,000 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 inservice 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.
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Technical Data
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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 %
Empty weight, baseline aircraft definition
(including engine oil and unusable fuel)
Maximum all-up weight
Maximum cargo-sling load
Maximum all-up weight in external load configuration
kg
lb
2,411
5,315
4,300
1,600
4,300
9,480
3,527
9,480
Power plant: 2 Turbomeca ARRIEL 2C free turbine engines
kW
Note: Thermal power, ISA, Sea Level
ch
717
645
622
625
580
O.E.I. 30 seconds rating
OE.I. 2 minutes rating
Continuous O.E.I. rating
Take-Off Power
Maximum Continuous Power
shp
974
876
845
849
788
961
865
834
838
778
Usable Fuel capacities
Standard fuel tanks (2 groups)
Additional fuel tanks
Auxiliary fuel tank
6th fuel tank
Ferrying fuel tank
litres
US gal.
kg
lb
1,135
300
897
1,977
180
112
475
47
29.5
125
142
89
375
313
195
827
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Technical Data
Main dimensions
Dimensions with blades folded
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Technical Data
Dimensions of compartments and doors
Cabin main dimensions
CABIN
4.20 m2
45.20 sq.ft
5.10 m3
180.10 cu.ft
Surface
Volume
HOLD
The cockpit is accessible through
two jettisonable hinged doors.
Surface
2.25 m2
24.21 sq.ft
Volume
1.10 m3
38.84 cu.ft
The luggage hold is accessible from the RH side
of the helicopter.
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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.
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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
notches, corrosion free
impact resistant they
individually interchangeable
manually foldable.
1
2
3
4
5
6
-
Blade tip cap
Balancing weights
Stainless steel strip
Glass carbon fibre cloth
Bushings
Tab
7 8 9 10 11 -
and
and
are
and
Fibreglass-roving spar
Moltoprene filler
Integrated weight
Balancing weight support
Bonding strip
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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
Chord length
Profile
Built-in twist
0.505 m (1.656 ft)
0.094 m (0.308 ft)
O.A.F.
- 10°
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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:
Console 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
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
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Technical Data
3 - AS365 N3 - Baseline Aircraft Definition
365 N3 08.100.02 E
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Technical Data
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Technical Data
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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 an 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.
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.
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.
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 2place 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 2place 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 an EUROCOPTER sales representative.
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Technical Data
4.1 – Oil & Gas Offshore Configuration
Document
reference
Commercial
reference
00-10013-A
05-02037-A
05-03010-A
05-27005-A
05-31036-A
05-32009-A
05-85009-A
06-21022-A
06-61020-A
00-10013-00-CI
05-02037-00-CI
05-03010-00-CI
05-27005-00-CI
05-31036-00-CI
05-32009-00-CI
05-85009-00-CI
06-21022-00-FP
06-61020-00-FP
06-61020-00-RP
06-62026-00-FP
06-62026-00-RP
06-62026-A
06-66012-A
06-67012-A
06-67041-A
06-67052-A
07-25009-A
07-25034-A
00-50021-A
06-66012-00-CI
06-67012-00-CI
06-67041-00-CI
06-67052-00-CI
07-25009-01-CI
07-25034-01-CI
00-50021-01-CI
Name
kg
lb
Baseline Aircraft Definition as per 365 N3 08.100.02 E
Customized external paint – Level 2
First aid kit - JAR OPS 3 compatible
Second fire extinguisher
Front panes in glass instead of plexiglass
Windshield washer
Fuel flowmeter, displayed on GPS Freeflight 2101 I/O Approach +
Goodrich Class 1 electrical Hoist (272 kg - 90 m) - Fixed Parts
Emergency floatation gear with automatic percussion - Fixed parts
Emergency floatation gear with automatic percussion - Removable parts
External Aerazur life rafts inst. (2 x 10 pax) with ELT compart (ELT not included) 1
Fixed Parts
2,411
3.0
5,315
6.7
5.0
2.4
10.9
2.8
3.5
3.6
14.5
43.1
4.6
1.1
5.3
24.0
6.2
7.7
8.0
32.0
95.0
10.1
Removable Parts
Helicopter Emergency Egress Lighting (HEEL)
77.6
171.1
4.0
8.8
2.4
7.1
1.2
10.0
4.3
71.4
5.3
15.7
2.6
22.0
9.5
157.4
3.0
14.6
3.6
10.5
3.0
14.0
6.6
32.2
7.9
23.1
6.6
30.8
1.5
10.5
3.3
23.1
2
Emergency Locator Transmitter Kannad 406-AP
2
HR Smith series 503 Automatic Deployable Emergency Locator Transmitter (ADELT)
Personal Locator Beacon HR Smith PLB 500-12 YF (Qty 2)
11-seat lay-out with 3 points harnesses instead of standard 8-seat lay-out
4 points harnesses for 11 standard seat lay-out.
AS365 N3 minimum equipment package
Including:
VHF-AM Honeywell KTR 908 (n°1)
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)
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)
3
4
08-16015-A
08-31040-A
08-35016-A
08-35019-A
08-46029-A
08-81023-A
08-16015-00-CI
08-31040-00-CI
08-35016-02-CI
08-35019-00-CI
08-46029-00-CI
08-81023-00-CI
08-83010-A
08-83012-A
08-83010-00-CI
08-83012-00-CI
1
2
3
4
5
6
GPS navigation system FREEFLIGHT 2101 I/O Approach+
Sfim CDV 85 D3 Flight Director Coupler (3 -axis)
Inter Communication System third control box TEAM TB 31
Telephonics RDR-1600C weather/search radar (displayed on MFD 255).
4
EGPWS Honeywell MK XXII displayed on KMD850 (not included)
TCAS Goodrich SKYWATCH HP 899 (displayed on KMD-850 - not included)
4-5
Jeppesen map Honeywell KMD 850, linked to GPS
Solid State Cockpit Voice & Flight Data Recorder Honeywell AR COMBI (2 hrs CVR
6
and 10 hrs FDR rec )
UMS - complement of SSCVFDR (usage functions) - Ground station excluded
HUMS (complement of UMS) (Health functions)
ELT to be ordered separately (could be PLB 500-12 YF)
The Programming Data Sheet must be filled and communicated by the Customer two months at the latest before the helicopter's
delivery.
The mode S identification must be communicated by the Customer two months at the latest before the delivery.
The Customer must take out a subscription to the data base in order to use these optionals after having taken delivery of the
helicopter.
The operational geographic zone of the helicopter must be communicated by the customer two months at the latest before the
delivery.
Includes an underwater beacon.
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Technical Data
Weights / Radius of Action
Empty weight, Oil & Gas Offshore Configuration
(including engine oil, unusable fuel and 2% margin)
Pilots (2 x 85 kg, JAR OPS 3)
Useful load
Fuel tanks capacity
Standard fuel tanks
Standard fuel tanks + auxiliary fuel tank
kg
lb
2,798
6,169
170
4,300
1,332
375
9,480
2,936
897
1039
1,977
2,291
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)
14
12
NB of PAX @ 85 kg
10
8
6
4
2
Fuel:
- (1) Standard fuel tanks
- (2) Standard fuel tanks + auxiliary fuel tank
(1)
(2)
0
0
50
100
150
200
Radius of Action (nm)
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Technical Data
4.2 – Passenger Transport Onshore Configuration
Document
reference
Commercial
reference
00-10013-A
00-10013-00-CI
05-02037-A
05-02037-00-CI
05-03010-A
05-27005-A
05-85009-A
Name
kg
lb
2,411
5,315
3.0
6.7
05-03010-00-CI
First aid kit - JAR OPS 3 compatible
5.0
1.1
05-27005-00-CI
2.4
5.3
05-85009-00-CI
3.5
7.7
2.4
5.3
1
06-67012-A
06-67012-00-CI
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
00-50021-01-CI
71.4
157.4
9.6
21.2
3.6
7.9
10.5
23.1
3.0
6.6
Including:
2
3
08-31038-A
08-31038-00-CI
Honeywell RDR 2000 weather radar (displayed on KMD-850 - not included)
3
08-35016-A
08-35016-02-CI
08-35019-A
08-35019-00-CI
08-46029-A
1
2
3
4
08-46029-00-CI
3-4
delivery.
helicopter.
delivery.
365 N3 09.101.01 E
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Technical Data
Weights / Range
Empty weight, Passenger Transport Onshore Configuration
Pilots (2 x 85 kg, JAR OPS 3)
Useful load
Fuel tanks capacity
Standard fuel tanks
kg
lb
2,586
5,701
170
4,300
1,544
375
9,480
3,404
897
1,039
1,977
2,291
- climb + cruise at 5000 ft at Best Range Speed
- reserve: 30 min at Best Endurance Speed, 1500 ft
Fuel:
1400
1200
Payload (kg)
1000
800
600
400
200
(1)
(2)
0
0
50
100
150
200
250
300
350
400
Range (nm)
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Technical Data
4.3 – 5-seat VIP Configuration with galley and partition (2+3)
Document
reference
Commercial
reference
00-10013-A
00-10013-00-CI
05-02037-A
05-02037-00-CI
05-31095-A
05-31095-00-CI
05-42026-A
05-85009-A
Name
kg
lb
2,411
5,315
3.0
6.7
Limousine panes in the cabin (for hinged cabin door configuration)
0.0
0.0
05-42026-00-CI
Air conditioning system (split)
45.4
100.1
05-85009-00-CI
3.5
7.7
06-41002-A
06-41002-00-CI
Under fuselage anti-collision strobe light
06-67012-A
06-67012-02-CI
Emergency Locator Transmitter Kannad 406-AP with GPS connection
1.5
3.1
3.3
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
00-50021-01-CI
71.4
157.4
1
Including:
2
3
08-17015-A
08-17015-01-CI
Passenger interphone Team BA 1920 (for VIP handset)
1.6
3.5
08-17016-A
08-17016-00-CI
1.8
4.0
08-18029-A
08-18029-00-CI
Passenger interphone for active noise cancelling headsets 1 x NAT AA-36 + 2 x NAT
AA-82
Active noise cancelling headsets Bose X (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
08-35016-A
08-35016-02-CI
08-35019-A
08-35019-00-CI
08-46029-A
08-46029-00-CI
08-81023-A
08-81023-00-CI
08-83010-A
08-83010-00-CI
1
2
3
4
5
9.6
21.2
3.6
7.9
10.5
23.1
3.0
6.6
5
14.0
30.8
1.5
3.3
3
3-4
delivery.
helicopter.
delivery.
365 N3 09.101.01 E
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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.
Weights / Range
Empty weight, 5-seat VIP Configuration (2+3)
Pilots (2 x 85 kg)
Useful load
Fuel tanks capacity
Standard fuel tanks
14
lb
2,896
6,385
170
4,300
1,234
375
9,480
2,720
897
1,039
1,977
2,291
Fuel:
12
10
NB of PAX @ 80 kg
kg
8
6
4
2
(1)
(2)
0
0
100
200
300
400
Range (nm)
365 N3 09.101.01 E
21
®
®
Technical Data
4.4 – 6-seat VIP Configuration with galley and partition (2+4)
Document
reference
Commercial
reference
00-10013-A
00-10013-00-CI
05-02037-A
05-02037-00-CI
05-31095-A
05-31095-00-CI
05-42026-A
05-85009-A
Name
kg
lb
2,411
5,315
3.0
6.7
0.0
0.0
05-42026-00-CI
45.4
100.1
05-85009-00-CI
3.5
7.7
06-41002-A
06-41002-00-CI
06-67012-A
06-67012-02-CI
1.5
3.1
3.3
6.8
07-50010-A
07-50010-00-CI
sliding doors)
12.0
26.5
07-81002-A
07-81002-00-CI
230.5
508.2
00-50021-A
00-50021-01-CI
71.4
157.4
1
Including:
2
3
08-17015-A
08-17015-01-CI
1.6
3.5
08-17016-A
08-17016-00-CI
1.8
4.0
08-18029-A
08-18029-00-CI
AA-82
3.0
6.6
08-18041-A
08-18041-00-CI
excluded)
0.1
0.2
08-31038-A
08-31038-00-CI
08-35016-A
08-35016-02-CI
08-35019-A
08-35019-00-CI
08-46029-A
08-46029-00-CI
08-81023-A
08-81023-00-CI
08-83010-A
08-83010-00-CI
1
2
3
4
5
9.6
21.2
3.6
7.9
10.5
23.1
3.0
6.6
5
14.0
30.8
1.5
3.3
3
3-4
delivery.
helicopter.
delivery.
365 N3 09.101.01 E
22
®
®
Technical Data
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. One divan, installed
in the rear part of the cabin,
accommodates comfortably 4
persons.
Weights / Range
Empty weight, 6 seat VIP (2+4) Configuration
Pilots (2 x 85 kg)
Useful load
Fuel tanks capacity
Standard fuel tanks
14
lb
2,887
6,365
170
4,300
1,243
375
9,480
2,740
897
1,039
1,977
2,291
Fuel:
12
10
NB of PAX @ 80 kg
kg
8
6
4
2
(2)
(1)
0
0
100
200
300
400
Range (nm)
365 N3 09.101.01 E
23
®
®
Technical Data
4.5 – 6-seat VIP Configuration with galley and without partition (4+2)
Document
reference
Commercial
reference
00-10013-A
00-10013-00-CI
05-02037-A
05-02037-00-CI
05-31095-A
05-31095-00-CI
05-42026-A
05-85009-A
Name
kg
lb
2,411
5,315
3.0
6.7
0.0
0.0
05-42026-00-CI
45.4
100.1
05-85009-00-CI
3.5
7.7
06-41002-A
06-41002-00-CI
06-67012-A
06-67012-02-CI
1.5
3.1
3.3
6.8
07-50010-A
07-50010-00-CI
sliding doors)
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
00-50021-01-CI
71.4
157.4
1
Including:
2
3
08-17015-A
08-17015-01-CI
1.6
3.5
08-17016-A
08-17016-00-CI
1.8
4.0
08-18029-A
08-18029-00-CI
AA-82
3.0
6.6
08-18041-A
08-18041-00-CI
excluded)
0.1
0.2
08-31038-A
08-31038-00-CI
08-35016-A
08-35016-02-CI
08-35019-A
08-35019-00-CI
08-46029-A
08-46029-00-CI
08-81023-A
08-81023-00-CI
08-83010-A
08-83010-00-CI
1
2
3
4
5
9.6
21.2
3.6
7.9
10.5
23.1
3.0
6.6
5
14.0
30.8
1.5
3.3
3
3-4
delivery.
helicopter.
delivery.
365 N3 09.101.01 E
24
®
®
Technical Data
conditions.
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.
Weights / Range
Pilots (2 x 85 kg)
Useful load
Fuel tanks capacity
Standard fuel tanks
14
lb
2,882
6,354
170
4,300
1,248
375
9,480
2,751
897
1,039
1,977
2,291
Fuel:
12
10
NB of PAX @ 80 kg
kg
8
6
4
2
(2)
(1)
0
0
100
200
300
400
Range (nm)
365 N3 09.101.01 E
25
®
®
Technical Data
4.6 – 6-seat VIP Configuration (3+3)
Document
reference
Commercial
reference
00-10013-A
00-10013-00-CI
05-02037-A
05-02037-00-CI
05-31095-A
05-31095-00-CI
05-42026-A
05-85009-A
Name
kg
lb
2,411
5,315
3.0
6.7
0.0
0.0
05-42026-00-CI
45.4
100.1
05-85009-00-CI
3.5
7.7
06-41002-A
06-41002-00-CI
06-67012-A
06-67012-02-CI
1.5
3.1
3.3
6.8
07-50010-A
07-50010-00-CI
sliding doors)
12.0
26.5
07-81019-A
07-81019-00-CI
224.0
493.8
00-50021-A
00-50021-01-CI
71.4
157.4
1
Including:
2
3
08-17015-A
08-17015-01-CI
1.6
3.5
08-17016-A
08-17016-00-CI
1.8
4.0
08-18029-A
08-18029-00-CI
AA-82
3.0
6.6
08-18041-A
08-18041-00-CI
excluded)
0.1
0.2
08-31038-A
08-31038-00-CI
08-35016-A
08-35016-02-CI
08-35019-A
08-35019-00-CI
08-46029-A
08-46029-00-CI
08-81023-A
08-81023-00-CI
08-83010-A
08-83010-00-CI
1
2
3
4
5
9.6
21.2
3.6
7.9
10.5
23.1
3.0
6.6
5
14.0
30.8
1.5
3.3
3
3-4
delivery.
helicopter.
delivery.
365 N3 09.101.01 E
26
®
®
Technical Data
conditions.
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.
Weights / Range
Pilots (2 x 85 kg)
Useful load
Fuel tanks capacity
Standard fuel tanks
14
lb
2,878
6,345
170
4,300
1,252
375
9,480
2,760
897
1,039
1,977
2,291
Fuel:
12
10
NB of PAX @ 80 kg
kg
8
6
4
2
(2)
(1)
0
0
100
200
300
400
Range (nm)
365 N3 09.101.01 E
27
®
®
Technical Data
4.7 – 7-seat VIP Configuration (4+3)
Document
reference
Commercial
reference
00-10013-A
00-10013-00-CI
05-02037-A
05-02037-00-CI
05-31095-A
05-31095-00-CI
05-42026-A
05-85009-A
Name
kg
lb
2,411
5,315
3.0
6.7
0.0
0.0
05-42026-00-CI
45.4
100.1
05-85009-00-CI
3.5
7.7
06-41002-A
06-41002-00-CI
06-67012-A
06-67012-02-CI
1.5
3.1
3.3
6.8
07-50010-A
07-50010-00-CI
sliding doors)
12.0
26.5
07-81003-A
07-81003-00-CI
7-seat VIP installation (4+3)
186.6
411.4
00-50021-A
00-50021-01-CI
71.4
157.4
AA-82
1.8
4.0
3.5
7.7
0.1
0.2
1
Including:
2
3
08-17016-A
08-17016-00-CI
08-18029-A
08-18029-00-CI
08-18041-A
08-18041-00-CI
excluded)
08-31038-A
08-31038-00-CI
08-35016-A
08-35016-02-CI
08-35019-A
08-35019-00-CI
08-46029-A
08-46029-00-CI
08-81023-A
08-81023-00-CI
08-83010-A
08-83010-00-CI
1
2
3
4
5
9.6
21.2
3.6
7.9
10.5
23.1
3.0
6.6
5
14.0
30.8
1.5
3.3
3
3-4
delivery.
helicopter.
delivery.
365 N3 09.101.01 E
28
®
®
Technical Data
conditions.
enhanced sound proofing. There
and the cockpit.
cabin and one 3-place divan is
installed in the rear part.
Weights / Range
Pilots (2 x 85 kg)
Useful load
Fuel tanks capacity
Standard fuel tanks
16
lb
2,841
6,263
170
4,300
1,289
375
9,480
2,842
897
1,039
1,977
2,291
Fuel:
14
12
NB of PAX @ 80 kg
kg
10
8
6
4
2
(2)
(1)
0
0
100
200
300
400
Range (nm)
365 N3 09.101.01 E
29
®
®
Technical Data
4.8 – 7-seat Corporate Configuration (4+3) – for hinged doors
Document
reference
Commercial
reference
00-10013-A
00-10013-00-CI
05-02037-A
05-02037-00-CI
05-31095-A
05-31095-00-CI
05-42026-A
05-85009-A
Name
kg
lb
2,411
5,315
3.0
6.7
0.0
0.0
05-42026-00-CI
45.4
100.1
05-85009-00-CI
3.5
7.7
06-41002-A
06-41002-00-CI
06-67012-A
06-67012-00-CI
Emergency locator Transmitter Kannad 406-AP
1.5
2.4
3.3
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
sliding doors)
12.0
26.5
00-50021-A
00-50021-01-CI
71.4
157.4
AA-82
1.8
4.0
4.0
8.8
0.1
0.2
1
Including:
2
3
08-17016-A
08-17016-00-CI
08-18029-A
08-18029-00-CI
08-18041-A
08-18041-00-CI
excluded)
08-31038-A
08-31038-00-CI
08-35016-A
08-35016-02-CI
08-35019-A
08-35019-00-CI
08-46029-A
08-46029-00-CI
08-81023-A
08-81023-00-CI
08-83010-A
08-83010-00-CI
1
2
3
4
5
9.6
21.2
3.6
7.9
10.5
23.1
3.0
6.6
5
14.0
30.8
1.5
3.3
3
3-4
delivery.
helicopter.
delivery.
365 N3 09.101.01 E
30
®
®
Technical Data
The AS365 N3 7-seat Corporate configuration (4+3) accommodates up to 7 passengers in excellent
comfort conditions.
sliding doors and improved
sound proofing. There is no
partition between the cabin and
the cockpit.
Weights / Range
Empty weight, 7 seat Corporate (4+3) Configuration
Pilots (2 x 85 kg)
Useful load
Fuel tanks capacity
Standard fuel tanks
16
lb
2,749
6,060
170
4,300
1,381
375
9,480
3,045
897
1,039
1,977
2,291
Fuel:
14
12
NB of PAX @ 80 kg
kg
10
8
6
4
2
(2)
(1)
0
0
100
200
300
400
Range (nm)
365 N3 09.101.01 E
31
®
®
Technical Data
4.9 – 7-seat Corporate Configuration (4+3) – for sliding doors
Document
reference
Commercial
reference
00-10013-A
00-10013-00-CI
05-02037-A
05-02037-00-CI
05-31094-A
05-31094-00-CI
05-42026-A
05-85009-A
Name
kg
lb
2,411
5,315
3.0
6.7
Limousine panes in the cabin (for sliding cabin door configuration)
0.0
0.0
05-42026-00-CI
45.4
100.1
05-85009-00-CI
3.5
7.7
06-41002-A
06-41002-00-CI
06-67012-A
06-67012-00-CI
1.5
2.4
3.3
5.3
07-25061-A
07-25061-00-CI
7-seat Corporate installation (4+3) – for sliding doors
96.5
212.7
00-50021-A
00-50021-01-CI
71.4
157.4
AA-82
1.8
4.0
1
Including:
2
3
08-17016-A
08-17016-00-CI
08-18029-A
08-18029-00-CI
4.0
8.8
08-18041-A
08-18041-00-CI
excluded)
0.1
0.2
08-31038-A
08-31038-00-CI
9.6
21.2
3
08-35016-A
08-35016-02-CI
08-35019-A
08-35019-00-CI
08-46029-A
08-46029-00-CI
08-81023-A
08-81023-00-CI
08-83010-A
08-83010-00-CI
1
2
3
4
5
3.6
7.9
10.5
23.1
3.0
6.6
5
14.0
30.8
1.5
3.3
3-4
delivery.
helicopter.
delivery.
365 N3 09.101.01 E
32
®
®
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
and the cockpit.
Weights / Range
Pilots (2 x 85 kg)
Useful load
Fuel tanks capacity
Standard fuel tanks
16
lb
2,736
6,032
170
4,300
1,394
375
9,480
3,073
897
1,039
1,977
2,291
Fuel:
14
12
NB of PAX @ 80 kg
kg
10
8
6
4
2
(2)
(1)
0
0
100
200
300
400
Range (nm)
365 N3 09.101.01 E
33
®
®
Technical Data
4.10 – 8-seat Corporate Configuration (4+4) – for hinged doors
Document
reference
Commercial
reference
00-10013-A
00-10013-00-CI
05-02037-A
05-02037-00-CI
05-31095-A
05-31095-00-CI
05-42026-A
05-85009-A
Name
kg
lb
2,411
5,315
3.0
6.7
0.0
0.0
05-42026-00-CI
45.4
100.1
05-85009-00-CI
3.5
7.7
06-41002-A
06-41002-00-CI
06-67012-A
06-67012-00-CI
1.5
2.4
3.3
5.3
07-25011-A
07-25011-00-CI
84.5
186.3
07-50010-A
07-50010-00-CI
sliding doors)
12.0
26.5
00-50021-A
00-50021-01-CI
71.4
157.4
AA-82
1.8
4.0
4.0
8.8
0.1
0.2
1
Including:
2
3
08-17016-A
08-17016-00-CI
08-18029-A
08-18029-00-CI
08-18041-A
08-18041-00-CI
excluded)
08-31038-A
08-31038-00-CI
08-35016-A
08-35016-02-CI
08-35019-A
08-35019-00-CI
08-46029-A
08-46029-00-CI
08-81023-A
08-81023-00-CI
08-83010-A
08-83010-00-CI
1
2
3
4
5
9.6
21.2
3.6
7.9
10.5
23.1
3.0
6.6
5
14.0
30.8
1.5
3.3
3
3-4
delivery.
helicopter.
delivery.
365 N3 09.101.01 E
34
®
®
Technical Data
The AS365 N3 8-seat Corporate Configuration (4+4) accommodates up to 8 passengers in excellent
comfort conditions.
sliding doors and specific sound
proofing.
cabin and two 2-place benchseats are installed in the rear
part.
Weights / Range
Pilots (2 x 85 kg)
Useful load
Fuel tanks capacity
Standard fuel tanks
16
lb
2,736
6,032
170
4,300
1,394
375
9,480
3,073
897
1,039
1,977
2,291
Fuel:
14
12
NB of PAX @ 80 kg
kg
10
8
6
4
2
(2)
(1)
0
0
100
200
300
400
Range (nm)
365 N3 09.101.01 E
35
®
®
Technical Data
4.11 – 8-seat Corporate Configuration (4+4) – for sliding doors
Document
reference
Commercial
reference
00-10013-A
00-10013-00-CI
05-02037-A
05-02037-00-CI
05-31094-A
05-31094-00-CI
05-42026-A
05-85009-A
Name
kg
lb
2,411
5,315
3.0
6.7
0.0
0.0
05-42026-00-CI
45.4
100.1
05-85009-00-CI
3.5
7.7
06-41002-A
06-41002-00-CI
06-67012-A
06-67012-00-CI
1.5
2.4
3.3
5.3
07-25052-A
07-25052-00-CI
84.5
186.3
00-50021-A
00-50021-01-CI
71.4
157.4
1.8
4.0
4.0
8.8
1
Including:
2
3
08-17016-A
08-17016-00-CI
08-18029-A
08-18029-00-CI
AA-82
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
9.6
21.2
08-35016-A
08-35016-02-CI
3.6
7.9
08-35019-A
08-35019-00-CI
10.5
23.1
08-46029-A
08-46029-00-CI
3.0
6.6
08-81023-A
08-81023-00-CI
5
14.0
30.8
08-83010-A
08-83010-00-CI
1.5
3.3
1
2
3
4
5
3
3-4
delivery.
helicopter.
delivery.
365 N3 09.101.01 E
36
®
®
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.
cabin and two 2-place benchseats are installed in the rear
part.
Weights / Range
Pilots (2 x 85 kg)
Useful load
Fuel tanks capacity
Standard fuel tanks
16
lb
2,724
6,005
170
4,300
1,406
375
9,480
3,100
897
1,039
1,977
2,291
Fuel:
14
12
NB of PAX @ 80 kg
kg
10
8
6
4
2
(2)
(1)
0
0
100
200
300
400
Range (nm)
365 N3 09.101.01 E
37
®
®
Technical Data
4.12 - Public services mission Configuration
Document
reference
Commercial
reference
00-10013-A
00-10013-00-CI
05-02037-A
05-02037-00-CI
05-31008-A
05-31008-00-CI
05-31009-A
05-85009-A
Name
kg
lb
2,411
5,315
3.0
6.7
Sliding window on the enlarged and bubble sliding door - RH Side
1.0
2.2
05-31009-00-CI
Sliding window on the enlarged and bubble sliding door- LH Side
1.0
2.2
05-85009-00-CI
3.5
7.7
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
8.6
19.0
(1,600 kg - 3,527 lb) - Fixed Parts
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
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
00-50021-01-CI
71.4
157.4
3.0
6.6
1
Including:
2
3
08-16015-A
08-16015-00-CI
08-31038-A
08-31038-00-CI
08-35016-A
08-35016-02-CI
08-35019-A
08-35019-00-CI
08-46029-A
08-46029-00-CI
1
2
3
4
3-4
3
9.6
21.2
3.6
7.9
10.5
23.1
3.0
6.6
delivery.
helicopter.
delivery.
365 N3 09.101.01 E
38
®
®
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 an EUROCOPTER sales representative.
Weights
Empty weight, public Service Configuration
Pilots (2 x 85 kg)
Useful load
Fuel tanks capacity
Standard fuel tanks
1400
lb
2,603
5,739
170
4,300
1,527
375
9,480
3,366
897
1039
1,977
2,291
Fuel:
1200
1000
Payload (kg)
kg
800
600
400
200
(2)
(1)
0
0
100
200
300
400
Range (nm)
365 N3 09.101.01 E
39
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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 particular 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 an EUROCOPTER sales representative.
Document
reference
Commercial
reference
Name
kg
lb
71.4
157.4
Minimum Equipment Package 1
00-50021-A
00-50021-01-CI
Including:
2
3
1
2
3
In addition to this package, a beacon must be selected in the possible optional equipment (ELT or/ and ADELT)
helicopter.
365 N3 09.101.01 E
40
®
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Technical Data
Document
reference
Commercial
reference
Name
kg
lb
General Equipment
05-01004-A
05-01004-00-CI
FAA certification kit
0
0
05-02011-A
05-02011-00-CI
05-02037-A
05-02037-00-CI
Customized external paint (level 1)
1.5
3.3
Customized external paint (level 2)
3.0
05-03010-A
6.7
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
1
2.8
6.2
05-25009-00-RP
Sand prevention filters, dynamic type - Removable Parts
11.0
24.3
1
05-25011-A
05-25011-00-CI
Re-inforced sand erosion protection strip on main rotor blades
0.4
0.9
05-26014-A
05-26014-00-CI
Enhanced anti-corrosion protection
3.5
7.7
05-26017-A
05-26017-00-CI
Dynol protection
2.0
4.4
05-27005-A
05-27005-00-CI
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
05-31036-A
05-31036-00-CI
Front panes in glass instead of plexiglass
05-31094-A
05-31094-00-CI
05-31095-A
05-31095-00-CI
05-32009-A
05-32009-00-CI
Windshield washer
05-42023-A
05-42023-00-CI
05-42026-A
05-51004-A
1.0
2.2
10.9
24.0
0
0
0
0
2.8
6.2
Air conditioning system (compact)
56.0
123.5
05-42026-00-CI
45.4
100.1
05-51004-00-CI
Heated windshield
1.3
2.9
05-52009-A
05-52009-00-CI
Icing detector (Rosemount)
05-62013-A
05-62013-00-CI
10-kVA A.C. alternator
05-81018-A
05-81018-00-FP
Auxiliary fuel tank in the hold (180 litres - 47 US gal.) - Fixed Parts
05-81018-00-RP Auxiliary fuel tank in the hold (180 litres - 47 US gal.) - Removable Parts
05-81036-A
05-81036-00-CI
6th fuel tank
05-81039-A
05-81039-00-CI
Reinforced skin fuel tanks
05-82021-A
05-82021-00-CI
Fuel jettison system
05-84003-A
05-84003-00-CI
Ferrying tank (475 litres - 125 US gal.) 2
05-85009-A
05-85009-00-CI
Fuel flowmeter displayed on GPS Freeflight 2101 I/O Approach +
1
2
1.1
2.4
27.8
61.3
3.9
8.6
23.7
52.2
9.0
19.9
21.8
48.1
6.6
14.6
26.5
58.4
3.5
7.7
Includes the supply of the standard cowlings.
It is forbidden to transport pax in cabin when ferrying tank is installed.
365 N3 09.101.01 E
41
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Technical Data
Document
reference
Commercial
reference
Name
kg
lb
3.6
8.0
Specific Mission Equipment
06-21022-A
06-24002-A
06-27010-A
06-21022-00-FP
Goodrich Class 1 electrical hoist (272 kg - 90 m) - Fixed Parts
06-21022-00-RP
Goodrich Class 1 electrical hoist (272 kg - 90 m) - Removable Parts
67.6
149.0
06-24002-00-FP
Rappelling installation (ropes excluded) - Fixed Parts
3.3
7.3
06-24002-00-RP
Rappelling installation (ropes excluded) - Removable Parts
2.6
5.7
06-27010-00-FP
Cargo sling with dynamometer and external mirrors (1,600 kg - 3,527 lb) - Fixed
Parts
Cargo sling with dynamometer and external mirrors (1,600 kg - 3,527 lb) Removable Parts
Cargo sling with dynamometer & ext. mirrors (1,600 kg), ext liferaft compatible Fixed Parts
Cargo sling with dynamometer & ext. mirrors (1,600 kg), ext liferaft compatible Removable Parts
8.6
19.0
19.0
41.9
4.6
10.1
19
41.9
7.0
15.4
06-27010-00-RP
06-27010-01-FP
06-27010-01-RP
06-31009-A
06-31009-00-FP
Electrical hailer with siren system - Fixed Parts
06-31009-00-RP
Electrical hailer with siren system - Removable Parts
11.0
24.3
06-41002-A
06-41002-00-CI
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 search light - Fixed Parts
06-45009-00-RP
Spectrolab SX-16 search light - Removable Parts
06-45034-00-FP
Spectrolab SX-5 search light - Fixed Parts
4.8
10.6
06-45034-00-RP
Spectrolab SX-5 search light - 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
-1.7
-3.7
63.6
140.2
4.6
10.1
77.6
171.1
06-45034-A
06-62026-A
1
1
06-62002-00-RP
Aerazur life-raft installation (2 x 10 pax) in cabin ceiling - Removable Parts
06-62026-00-FP
Fixed Parts
Removable Parts
06-62026-00-RP
06-66012-A
06-66012-00-CI
Helicopter Emergency Egress Lighting (HEEL)
06-67012-A
06-67012-00-CI
06-67012-02-CI
06-67041-A
06-67041-00-CI
Automatic deployable Emergency Locator Transmitter (ADELT) HR SMITH series
3
503
06-67052-A
06-67052-00-CI
06-68009-A
06-69004-A
06-81008-A
1
2
3
4.8
10.6
31.5
69.5
4.0
8.8
2.4
5.3
3.1
6.8
7.1
15.7
Personal Locator Beacon HR Smith PLB 500-12 YF
0.6
1.3
06-68009-00-CI
Under Water Acoustic Beacon Dukane DK 120
0.4
0.9
06-69004-00-CI
Automatic Voice Alarm Device Thales Avionics V 694
2.3
5.1
06-81008-00-FP
Fire-fighting "Bambi Bucket" (910 litres) - Fixed Parts
06-81008-00-RP
Fire-fighting "Bambi Bucket" (910 litres)- Removable Parts
3
3
4.0
7.1
61.0
113.8
Deliverable with standard upholstery.
ELT to be ordered separately (could be PLB 500-12 YF)
The Programming Data Sheet must be filled and communicated by the customer two months at the latest before the helicopter's
delivery.
365 N3 09.101.01 E
42
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Technical Data
Commercial
reference
Document
reference
Name
kg
lb
Interior Layout
07-25002-A
07-25009-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
07-25009-00-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
07-25011-A
07-25011-00-CI
10.0
22.0
185.7
409.4
07-25033-A
07-25033-00-CI
07-25034-A
07-25034-00-CI
4 points harnesses for 8 standard seats layout
3.1
6.8
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
185.7
409.4
07-25060-A
07-25060-00-CI
201.6
444.4
07-25061-A
07-25061-00-CI
201.6
444.4
204.4
07-30003-A
07-30003-00-CI
Comfort upholstery with improved sound-proofing and carpeting - for hinged doors
92.7
07-30033-A
07-30033-00-CI
Comfort upholstery with improved sound-proofing and carpeting - for sliding doors.
77.3
170.4
12.0
26.5
1.7
3.8
07-50010-A
07-50010-00-CI
sliding doors)
07-50038-A
07-50038-00-CI
LH sliding door opening extension (on ground)
07-71015-A
07-81001-A
07-81002-A
07-71015-00-FP
Casualty-carrying installation for 4 stretchers (excluding stretchers) - Fixed Parts
07-71015-00-RP
Casualty-carrying installation for 4 stretchers (excluding stretchers) - Removable
2
Parts
07-81001-00-CI
07-81002-00-CI
07-81003-A
07-81003-00-CI
3
07-81019-A
07-81019-00-CI
3
07-81046-A
07-82005-A
07-82005-A
1
2
3
4
1
07-81046-00-CI
07-82005-00-CI
2
1.8
4.0
9.5
20.9
3
240.5
530.2
3
6-seat VIP installation with galley and without partition (4+2)
3
4
Headrest (Qty 8) & floor inserts for 8-seat face-to-face installation
230.5
508.2
186.6
411.4
224.0
493.8
225.6
497.4
4.0
8.8
07-82005-01-CI
Headrest (Qty 8)
2.8
6.2
07-82005-02-CI
Headrest (Qty 7)
2.5
5.4
Ground Support equipment. The maximum extension of the LH sliding door can be performed on ground only.
The corresponding stretchers are not provided because they are not certified.
Refer to the specific VIP & Corporate Technical Data for the dedicated options.
Mandatory for seats facing backwards.
365 N3 09.101.01 E
43
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Technical Data
Document
reference
Commercial
reference
Name
kg
lb
Interior Layout (continuous)
• Optional installation For VIP configuration 1
07-40022-A
07-40022-00-CI
Additional hand tufted carpet for VIP cabin (spare)
15.0
33.1
07-81020-A
07-81020-00-CI
Two additional bench seats for VIP installation
42.5
93.7
07-81048-A
07-81048-00-CI
VVIP upgrade
21.0
46.3
07-81050-A
07-81050-00-CI
Foldable central back rest of the rear divan (3 seat)
8.5
18.7
07-83011-A
07-83011-00-CI
Blanking curtain for VIP partition (cabin side)
3.2
7.1
07-90011-A
07-90011-00-CI
Partition between cabin and cockpit
19.0
41.9
07-90026-A
07-90026-00-CI
Audio player for VIP installation
3.1
19.8
07-91003-A
07-91003-00-CI
Gold plated finishing of the visible cabin metallized parts
0.0
0.0
20.8
45.9
• Optional installation For CORPORATE configuration 1
07-81047-A
07-81047-00-CI
Executive upgrade - for hinged doors
• Optional installation For VIP & CORPORATE configuration 1
07-25062-A
07-25062-00-CI
Harmonized pilot seats harnesses for Fisher seats only
0.0
0.0
07-90009-A
07-90009-00-CI
VIP treatment of the cockpit
6.5
14.3
1
Refer to the specific VIP & CORPORATE Technical Data for the dedicated options
365 N3 09.101.01 E
44
®
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Technical Data
Document
reference
Commercial
reference
Name
kg
lb
23.0
50.7
2.5
5.5
Avionics
08-10001-A
08-10001-00-CI
HF/SSB Collins HF 9000
08-12011-A
08-12011-00-CI
VHF/FM Maritime NAT NPX 138 n°1
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)
2.4
5.3
08-16015-A
08-16015-00-CI
3.0
6.6
08-16019-A
08-16019-00-CI
Inter Communication System fourth control box TEAM TB 31
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
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
2.4
08-18029-A
08-18029-00-CI
Active noise canceling headsets Bose X (Qty 1)
08-18040-A
08-18040-00-CI
David Clark H 10-13 H headset (Qty 1)
08-18041-A
08-18041-00-CI
08-27017-A
1
1
0.5
1.1
0.3
0.6
excluded)
0.1
0.2
08-27017-00-CI
SAR Homer Chelton SYSTEM 7 (with stand alone indicator)
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
Weather radar RDR 2000 Honeywell (displayed on KMD-850 - not included)
9.6
21.2
08-31040-A
08-31040-00-CI
Weather/search radar Telephonics RDR-1600C (displayed on MFD 255)
15.2
33.5
08-35016-02-CI
08-35019-A
08-35019-00-CI
1
2
3.6
7.9
10.5
23.1
15.0
33.1
5.0
11.0
08-38004-A
08-38004-00-CI
Stormscope Goodrich WX1000E (displayed on KMD850 - not included)
08-46022-A
08-46022-00-CI
Moving map EUROAVIONICS EURONAV IV linked to GPS, and displayed on
10.4" MFD (MFD not included)
08-46029-A
08-46029-00-CI
3.0
6.6
08-65010-A
08-65010-00-CI
Display 10,4" Skyquest Aviation
2.6
5.7
08-81023-A
08-81023-00-CI
Solid State Cockpit Voice & Flight Data Recorder Honeywell AR COMBI (2 hrs
4
CVR and 10 hrs FDR rec)
14
30.9
08-83010-A
08-83010-00-CI
08-83012-A
08-83012-00-CI
HUMS - complement of UMS (health functions)
2-3
1.5
3.3
10.5
23.1
• Optional installation For VIP configuration 5
08-17056-A
08-17056-00-CI
Flight information display (ceiling)
08-17057-A
08-17057-00-CI
In-Flight Entertainment System in rear galley
1
2
3
4
5
1.0
2.2
40.0
88.2
Quantity to be defined.
helicopter.
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.
Refer to the specific VIP & CORPORATE Technical Data for the dedicated options.
365 N3 09.101.01 E
45
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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
kg
lb
Gross Weight
3,750
8,267
4,000
8,818
4,300
9,480
Max. speed, VNE
km/hr
kts
306
165
296
160
287
155
Fast cruise speed
km/hr
kts
279
151
274
148
269
145
Recommended cruise speed
km/hr
kts
276
149
274
148
269
145
Fuel consumption at recommended cruise speed
kg/hr
lb/h
309
681
313
690
314
692
Rate-of-climb
m/sec.
ft/min.
8.9
1,759
7.9
1,554
6.7
1,321
m
ft
3,900
12,795
3,300
10,827
2,620
8,596
m
ft
3,150
10,335
2,530
8,300
1,810
5,938
m
ft
3,110
10,203
2,500
8,202
1,150
3,773
m
ft
2,320
7,610
1,685
5,527
310
1,017
m
ft
5,865
19,242
5,290
17,355
4,640
15,223
km
n.m
827
446
811
438
792
427
km
n.m
963
520
945
510
923
498
hr
hr
4.3
5.0
4.2
4.9
4.1
4.75
Hover ceiling I.G.E. at Take-Off Power (6 ft)
ISA
ISA + 20°C
Hover ceiling O.G.E. at Take-Off Power
ISA
ISA + 20°C
Service ceiling (Vz = 0,5 m/sec. – 100 ft/min.)
ISA
Maximum range (without fuel reserve,
at recommended cruise speed)
with standard tanks
with optional auxiliary tank
Maximum endurance [without reserve
at 140 km/hr (75 kts)]
with standard tanks
with optional auxiliary tank
365 N3 09.101.01 E
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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
Rate-of-climb at continuous OEI power
Service ceiling (0.5 m/sec. - 100 ft/min.) continuous OEI
power
kg
lb
3,750
8,267
4,000
8,818
4,300
9,480
m/sec.
ft/min.
m
ft
4.6
905
3,125
10,252
3.8
748
2,515
8,259
2.9
570
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:
ISA:
MCP:
OEI:
OGE:
SL:
TAS:
In Ground Effect
International Standard Atmosphere
Maximum Continuous Power
One Engine Inoperative
Out of Ground Effect
Sea Level
True Airspeed
TOP:
VNE:
VTOL:
Vtoss:
Vy:
Vz:
Take-Off Power
Never Exceed Speed
Vertical Take-Off and Landing
Take-off Safety Speed
Optimum Climbing Speed
Rate-of-Climb
Units
nm:
kts:
ft/min:
m/sec:
° C:
nautical miles
knots
feet/minute
meters per seconds
degrees Celsius
hr:min:
Kg:
lb:
km:
hours:minutes
kilograms
pounds
kilometers
365 N3 09.101.01 E
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Technical Data
Blank
365 N3 09.101.01 E
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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 50
Take-off weight in hover OGE
on 2 engines at Maximum take-off power ................................................................................. page 51
Maximum Permissible Gross Weight on take-off from clear heliport
Category A
Vtoss : 65/75 kts – Vy : 75 kts................................................................................................... page 52
Maximum Permissible Gross Weight on take-off from helipad
Category A ................................................................................................................................ page 53
Rate of climb in oblique flight
on 2 engines at maximum continuous power
ISA; T.A.S. = 75 kts ................................................................................................................. page 54
on 2 engines at maximum continuous power
ISA+ 20°C; T.A.S. = 75 kts ..................................................................................................... page 55
on 1 engine OEI unlimited
ISA; T.A.S. = 75 kts ................................................................................................................. page 56
ISA + 20°C; T.A.S. = 75 kts .................................................................................................... page 57
Hourly fuel consumption in level flight
Pressure-altitude = 0 ft, ISA (temperature = 15°C) ................................................................. page 58
Pressure-altitude = 5000 ft, ISA (temperature = 5.1°C) .......................................................... page 59
Pressure-altitude = 10000 ft, ISA (temperature = -4.8°C) ....................................................... page 60
Pressure-altitude = 0 ft, ISA + 20°C (temperature = 35°C) ..................................................... page 61
Pressure-altitude = 5000 ft, ISA + 20°C (temperature = 25°C) ............................................... page 62
Pressure-altitude = 10000 ft, ISA + 20°C (temperature = 15.2°C) ......................................... page 63
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TAKE-OFF WEIGHT IN HOVER I.G.E. (6 ft)
on 2 engines at Maximum Take-Off Power
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TAKE-OFF WEIGHT IN HOVER O.G.E.
on 2 engines at Maximum Take-Off Power
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MAXIMUM PERMISSIBLE GROSS WEIGHT ON TAKE-OFF
FROM CLEAR HELIPORT
Category A
Vtoss: 65/75 kts - Vy: 75 kts
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MAXIMUM PERMISSIBLE GROSS WEIGHT ON TAKE-OFF
FROM HELIPAD
Category A
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RATE OF CLIMB IN OBLIQUE FLIGHT
on 2 engines at Maximum Continuous Power
ISA; T.A.S. = 75 kts
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on 2 engines at Maximum Continuous Power
ISA+20 °C; T.A.S. = 75 kts
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ISA; T.A.S. = 75 kts
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ISA+20°C; T.A.S. = 75 kts
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HOURLY FUEL CONSUMPTION IN LEVEL FLIGHT
Pressure-altitude = 0 ft ; ISA (Temperature = 15 °C)
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Pressure-altitude = 5000 ft ; ISA (Temperature = 5.1 °C)
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Pressure-altitude = 10000 ft ; ISA (Temperature = -4.8 °C)
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Pressure-altitude = 0 ft ; ISA + 20 °C (Temperature = 35 °C)
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Pressure-altitude = 5000 ft ; ISA+20 °C (Temperature = 25 °C)
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Pressure-altitude = 10000 ft ;ISA + 20 °C (Temperature = 15.2 °C)
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Blank
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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
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 795 helicopters in service world-wide. The total
flight hours accumulated at the end of 2008 are about 4,610,000 hours. The “lead the fleet” aircraft has
accumulated more than 25,000 flight hours.
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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
230 MMH
Scheduled Engine Inspection
Estimated Man Hour
ARRIEL 2C
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.
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Main components
Time Between Overhauls (TBO) / Service Life Limit (SLL)
Main Components
1
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
“*”: Target value within the Maturity Plan under progress.
Time Between Overhauls (TBO):
The component in question must be removed at each interval that corresponds to the value indicated, in
order to undergo the operations in a specialized workshop that will enable it to be put back into service for
the next interval.
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
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EUROCOPTER Maintenance Support Programs
EUROCOPTER offers its clients a comprehensive array of repair and overhaul services to ensure availability
and costs control. This array of services ranges from basic OEM repair and overhaul services up to
comprehensive Parts By the Hour (PBH) maintenance programs.
The different services are each tailored for 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.
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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.
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Engine Maintenance program
Always looking to maximize your efficiency and reduce your costs, Turbomeca, the engine manufacturer has
developed an improved service offering.
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:
Classic Repair and Overhaul
Standard Exchange
AOG services
Support By the Hour (SBH) services
Within the Support By the Hour® coverage Turbomeca developed specific maintenance packages, as
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
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Training
With more than 50 years of experience, the EUROCOPTER training centers provide the most
comprehensive, coherent and highest standard helicopter training in the world for pilots and technicians,
whether civilian or military.
Qualification training, allowing operators to comply with regulatory requirements, and services training, more
mission oriented and tailored to the customers’ operational needs, are addressed.
All training courses are established according to the relevant civil aviation authorities’ requirements. The
centers are approved by the relevant airworthiness authorities (EASA, FAA, DGAC, LBA, CAA…). We are
certified ISO 9001: V2000 and regularly audited by independent organisms such as Véritas, AFAQ…
EUROCOPTER training centers provide a wide range of courses and services, from basic training up to
preparation for the most sophisticated civil and military missions.
As part of the full range of services on offer, EUROCOPTER also plays an active role in helicopter pilot
development through its Ab Initio programs.
Centers are equipped with multimedia classrooms. This includes computers overhead projectors and stateof-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
Pilots
AS365 N3 Type Rating
Instructor Pilot Conversion (1)
10 days
-
9 1/2 hours
6 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 (mini 15 hours, within last 12 months, not included in Type Rating).
Note: length is given as information and depends on pilot or technician qualification or experience.
Complementary courses may be required.
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Engine Training Courses
Training courses dedicated to Engine Maintenance is also organized by Turbomeca training schools and
approved centers the world over.
Up-to-date course calendars, on-line tests and e-learning modules are also available on the Turbomeca
Operator On-Line Support (TOOLS site).
Technical publications
EUROCOPTER provides all the technical publications necessary for safely operating and maintaining its
aircraft cost effectively.
EUROCOPTER technical publications are available on an interactive electronic medium as a standard or in
hard copies as an option.
The OPEN DVD-ROM includes the Maintenance Program (PRE), the Maintenance Manual (MET), the
Wiring Diagram Manual (MCS), the Description and Operation Manual (MDF), the Fault and Isolation Manual
(MFI), the Storage and Preservation Manual (MST), the Repair Manual (MRR), the Standard Practices
Manual (MTC) and the Illustrated Parts Catalogue (IPC).
The component maintenance manual (CMM) is available on DVD-ROM or hard copy, depending on the
Vendor.
Along with the OPEN DVD-ROM, EUROCOPTER provides a hard copy of the Airworthiness Technical
Publication (Flight Manual, Pilots Check List, Master Servicing Manual…) as well as the Service Bulletin
Catalogue.
The DVD ROM is available in English; 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:
Emergency Alert Service Bulletin (formerly Télex Alert), Alert Service Bulletin , Safety Information Notice
(formerly Télex Information), Service Bulletin, Information Notice (formerly Service Letter,), Technical
Information Letter.
Airworthiness Limitations Section (ALS).
FLM revisions.
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.
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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

AS365N3 - Airbus Helicopters

Transcription

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