2006 Airbus Helicopters AS355N
SoldS/N: 5743
Highlights
- VIP Configuration
- Emergency floatation gear Aerazur – Fixed Parts
- Wire strike protection system
- Fresh 12 Years inspection & Eng#1 Overhauled
Details
- Dual controls
- Pilot’s windshield wiper
- Copilot’s windshield wiper
- Engine flushing device without removing cowlings
- Engine fire-extinguishing system (CAA IFR certification Kit)
- RH landing-light swivelling in elevation
- LH landing-light, swivelling in elevation and azimuth (CAA IFR certification Kit)
- 2nd battery / 2nd altimeter (CAA IFR certification Kit)
- Tail rotor arch protection
- High skid landing gear with 2 long footsteps
- High visibility main rotor blades
- Reinforced sand-erosion protective strip M/R blades and T/R blades
- Emergency floatation gear Fixed part
- Remaining fuel flowmeter
- Wire strike protection system
- Cargo swing Fixed Parts
- RH side external mirror Fixed Part
- Hourmeter
- 1 Garmin GTX Transponder (mode S)
- 1 Kannad 406 AF-H Emergency Locator Transmitter
- Special IFR instrument panel
- Second anemo-barometric circuit
- 1 Flight director gyro-horizon Thales H140
- 1 Gyro-Compas Honeywell KCS55 A with Horizontal Situation Indicator Honeywell KI525A
- 1 Stand-by gyro-horizon Thales H140
- Rate-of Climb indicator with setter in place of the standard one
- Radio Magnetic Indicator Honeywell KNI 582 with 02 needles and twin switching
- 1 VHF/VOR/LOC/GS Honeywell KX165
- 1 VHF/VOR/LOC/GS/GPS Garmin GNS430
- 1 ADF Honeywell KR87
- 1 Marker beacon receiver Honeywell KR21
- 1 DME KN 63
- Altitude Encoder
- 1 Radio Altimeter Thales AHV 16
- Radar Altimeter Warning Aerotec with warning generator
- SFIM 85 T31 + SFIM CDV 85 T3 3 axis AP + FDC, VFR & IFR with failure passivation unit
- 250 VA AC 1st and 2nd generation system
- ICS Team TB39 or TB31
- Passenger Interphone
- ELT
- Electrical Extension for Bose Headsets
- 2 Arrius 1A turbine engines 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 a total failure of the 2 digital channels of the FADEC
- 1 twist grip on pilot side and co-pilot side (for engine reduction in case of tail rotor failure and autorotation training)
- magnetic plug and 1 chip detector
- engines lubrication and oil cooling system
- fire detection system
- air-intake protection grids
- torque-measurement pick-up
- 5 passengers seats + 1Pilot seat or 4 passengers seats + 1Pilot seat & 1 Co-pilot seat
- Left and Right read sliding door
- Sliding window, on left and right rear sliding door
- Comfort layout with sound proofing
- Energy absorbing front seats
- Customized painting Blue and gray with yellow lines
General equipment & Optional equipments
Avionics Single/ Dual Pilot Day and night VFR IFR Operations
Power Plant
Interior Layout
Exterior
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