AIRFRAME
GENERAL
-The H125® is certified with a pilot being on the right side
-The baseline aircraft is delivered with right side controls and capabilities for the removable dual controls (LH controls are optional)
-Fuselage comprising the cabin and 3 luggage holds, with floor tie-down nets and access doors
-Tail boom with stabilizer, anti-torque rotor and fin with tail skid
-High skid landing gear with long footsteps (on right side and on left side}, capable of taking handling wheels
-Lifting points
-Mooring fixtures
-Structural reinforcements for cable cutter system
-Structural reinforcements for RH external mirrors
-Single color exterior painting
-Internal paint: grey (prevailing colour)
-Interior signs and markings: available in either French or English
POWER PLANT
1 ARRIEL 20 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 a total failure of the 2 digital channels of the FADEC
Full available engine power of ARRIEL 2D
1 Crash Resistant Fuel System including 1 tank of 540 litres (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 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 r.p.m. sensor and 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 with 2 composite-material blades
3 main rotor hydraulic servo units
1 tail rotor hydraulic servo unit and load compensation systems
ELECTRICAL INSTALLATION
One 150 A, 28 V DC starter-generator
One 28 V DC cabin power outlet
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 adjustable emergency/reading map lights for crew
2 adjustable reading lights for passengers
1 integrated instrument-panel lighting system
1 integrated lighting in central console
2 cockpit breaker panels
1 USB charging dual-outlet (instrument panel
ENGINES
Safran Arriel 2D
S/N: 53935
TSN: 7:46