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.
130 B4 09.100.01 E
12
This document is the property of
EUROCOPTER
©
; no part of it shall be reproduced or transmitted without the express prior written authorization of
EUROCOPTER
©
and its contents shall not be disclosed.
©
EUROCOPTER-2009
AVIONICS
1 avionics master switch
1
gyro-horizon
1
gyro-compass
with
1 horizontal Situation Indicator
1 turn and bank indicator
1
VHF/VOR/LOC/GS
1 VHF/VOR/LOC/GS/GPS
1 transponder (mode A+C)
1 altitude encoder
1 Emergency Locator Transmitter
1 ICS + passenger interphone
POWER PLANT
1 Turboméca ARRIEL 2B1 632 kW (850 ch - 847 shp) turbine
engine complete with starting, fuel supply and dual channel
digital engine control system (FADEC) and 1 back-up fuel
control box that automatically controls the engine in case of a
total failure of the 2 digital channels of the FADEC
1 fuel system including 1 tank of 540 liters (143 US gal.) total
capacity
1 twist grip on pilot side (for engine reduction in case of tail
rotor failure and autorotation training)
1 magnetic plug and 1 chip detector
1 engine lubrication and oil cooling system
1 fire detection system
1 air-intake protection grids
1 torque-measurement pick-up
TRANSMISSION SYSTEM
1 main gearbox, anti-vibration mounted, with oil sight gauge,
chip detector, oil temperature and pressure switches, port for
endoscope and self sealing valve for oil sampling and draining
1 main gearbox oil cooling system
1 engine to main gearbox coupling shaft
1
rotor
brake
1 main rotor high and low r.p.m. warning device
1 tail drive carried by five anti-friction bearings
1 tail gearbox with oil sight gauge, chip detector and port for
endoscopic inspection
ROTORS AND FLIGHT CONTROLS
1
main rotor with 3
composite-material blades around a
STARFLEX
®
head fitted with spherical thrust bearings
1
anti-torque rotor (
FENESTRON
®
)
with 10
asymmetrical
blades, integrated in vertical fin
3 main rotor hydraulic servo units (duplex servos)
2 independent hydraulic generation systems
ELECTRICAL INSTALLATION
One 150 A, 28 VDC starter-generator
One 15 A.h cadmium-nickel battery
1 ground power receptacle
3 position lights (LED)
1 flashing anti-collision light (LED)
2 fixed landing lights
2
cabin light sets, each with 2
reading lights for 2
rear
passengers and 1 dome light
1 instrument panel lighting system
Integrated lighting in central console
1 reading map light on upper canopy strut for pilot
1 cockpit breaker panel
One 28 V DC cabin power outlet
AIRBORNE KIT (*)
1 pitot head cover
2 static port stoppers
1 engine air-intake blanking cover
1 tail-pipe plug
2 ground handling bogies c/w hydraulic jacking system
1 lifting ring
2 upper mooring rings
3 main-blade socks
1 document holder
1 airborne kit stowage bag
Manuals (CD ROM)
(*)
(weight not included in standard aircraft empty weight)