Description
The AS355NP has a maximum Take-off Weight of 2,600kg and a useful load of 1,097kg. Powered by the Turbomeca (SAFRAN) Arrius 1A1 engines it has a FADEC engine control system and compared to the 'N' model it has improved OEI ratings and an upgraded Main Gear Box increasing the MAUW by 200 kgs on the hook. It will depart Cat A at MAUW at ISA + 12 at Sea Level. Engine display is via the VEMD system - still the industry standard for AIRBUS. The engine hours need attention but the SAFRAN PBH program will take care of those. Call for more information please.
ENGINES
Engine 1 Notes
Engine #1
TSN - 1942 hours (3000 hr OH) Remaining - 1058 hours
MO1 15Y calendar due Jan 2024
MO2 15Y calendar due Jan 2024
ENROLLED ON PBH
Engine #2
TSN - 1871 hours (3000 hr OH) Remaining - 1129 hours
MO1 15Y calendar due March 2031
MO2 15Y calendar due July 2038
ENROLLED ON PBH
Rotor
Main Rotor Blade Time Remaining 18275
Main Rotor Gearbox Time Remaining 857
Anti-Torque System Tail Rotor
Tail Rotor Blade Time Remaining 3992
Tail Rotor Gearbox Time Remaining 357
Maintenance
Avionics
Artificial Horizon
Single Pilot Operation
Auto Pilot
ELT
Avionics/Radios
VFR day and night package included in AIRBUS AS355 factory definition.
Auto Pilot
Vehicle and Engine Monitoring Display (VEMD)
Artificial Horizon with Turn Co-Ordinator (AH)
Horizon Situation Indicator (HSI)
Vertical Speed Indicator
Garmin GPS/NAV/COM
Garmin Transponder
Audio Panel and Intercom system (ICS)
Emergency locator transmitter
Exterior
Door Type Hinged and Sliding
Additional Info
Baggage Compartment
Air Conditioning
Autopilot
Pop-Out Floats
3 Point harness (rear)