General Equipment:
• First Aid kit
• High visibility paint scheme on main rotor blades (RED)
• Tinted windows for standard and optional door configuration
• Bulged window on right rear door
• Bulged window on left rear door
• Pilot windshield wiper
• Dual controls
Mission Equipment
• LH landing light (swivelling in elevation and azimuth)
• Cargo swing (1400kg) (fixed parts)
• Emergency floatation (fixed parts)
Bose Headsets:
• Six (6) Bose A20 blue tooth aviation headsets compatible with the ICS installation
2.3: I pad Mounts
• 2 x Ipad mounts fitted either side of the main instrument panel – compatible with Apple Ipad Mini – note: I pad mini’s NOT included
2.4: Commissioning:
• EASA or CAA registered and certified
Definition of the Standard H125 aircraft
The helicopter meets the certification standards for day and night VFR operations, set by the following airworthiness authorities: EASA, FAA,TCCA, ANAC, CAAC, IAC-AR. This list is not restrictive and the status of approval by other airworthiness authorities must be checked. Additional equipment items may be required by the relevant operational authorities’ certification regulation
General:
• The H125 is certified with a pilot being on the right hand side
• Dual controls are fitted to this aircraft
• Fuselage comprises of the cabin and 3 luggage holds with floor, tie down nets and access doors
• Tail boom with stabiliser, anti-torque rotor and fin with tail skid
• High skid landing gear with long footsteps (on both sides) and capable of taking handling wheels
• Lifting points
• Mooring fixtures
• Structural reinforcements for cable cutter
• Structural reinforcements for RH external mirrors
• Internal paint (grey)
• Interior signs and markings
Instruments:
• Integrated Flight Display: Primary Flight Display / Navigation Display (PFD / ND)
• Primary Flight Display: airspeed, vertical speed, attitude, altitude, T&B, HIS with VOR
• Moving Map: Nav data, flight plan, high resolution helicopter dedicated terrain and obstacle databases
• 1 x LCD dual RPM tachometer (Rotor and Free Turbine)
• 1 x Stop watch
• 1 x warning panel
• 1 x heated pitot head
• 1 x external side slip indicator
• 1 x control box for light and electrical generation
• 1 x I.C.S. connected to aural warning issued from VEMD
• 1 x cockpit imaging and flight data monitoring device
Standby Instruments:
• 1 x electronic standby Instrument (ESI)
• 1 x Magnetic compass
• 1 x LCD Dual screen Vehicle and Engine Multifunction Display (VEMD) providing the following information:
• First limitation indicator (FLI)
• Torque meter
• Exhaust gas temperature (TOT)
• Gas generator tachometer (N1)
• Engine oil temperature / pressure
• Fuel quantity
• Fuel flow and estimated remaining time to fly
• Ammeter and voltmeter and battery temp
• Outside Air temperature (OAT
Enhanced usage monitoring functions:
• IGE/OGE performance calculations
• Engine cycles counting
• Engine power check
• Over limit display
• VEMD and peripheral maintenance information
• Data downloading capability