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.
350 B3 08.100.01 E
10
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
AVIONICS
1 avionics master switch
1
gyro-horizon
1
gyro-directional
1 course Deviation 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 (2 frequencies)
1 ICS + passenger interphone
POWER PLANT
1 Turboméca ARRIEL 2 632 kW (860 ch – 847 shp) turbine
engine complete with starting, fuel supply and dual channel
digital engine control system (FADEC) with back-up control
system that automatically controls the engine in case of total
failure of the 2 digital channels of the FADEC
1 fuel system including 1 tank of 540 litres (143 US gal.) total
capacity
1 magnetic plug and chip detector
1 engine lubrication and oil cooling system
1 fire detection system
1 air-intake protective 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 FLYING CONTROLS
1 main rotor with 3 composite-material blades around a
STARFLEX
®
head fitted with spherical thrust bearings
1 anti-torque rotor with 2 composite-material blades
3 main rotor hydraulic servo units
1 tail rotor hydraulic servo unit and a load compensator
ELECTRICAL INSTALLATION
One 150 A, 28 V DC 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 light
2 cabin dome lights
1 instrument-panel lighting system
Integrated lighting in central console
1 swivelling emergency and reading map light
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 GHW modification kit
1 lifting ring
2 upper mooring rings
3 main-blade socks
1 tail rotor locking device
1 document holder
1 airborne kit stowage bag
(*)
(weight not included in standard aircraft empty weight)
