G-HITK Airbus H125

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.

OFFERED EXCLUSIVELY FOR SALE BY HILTI AIR

G-HITK Airbus H125

Price: Make Offer

Specifications

Baseline Helicopter:

H125 Baseline Aircraft I.A.W. H125 B3 20.100.01 E
VFR Day and night package with integrated Flight Display Garmin G500 TXi, included in baseline definition:
Emergency locator transmitter – Kannad 406 INTEGRA AP-H
VHF/VOR/LOC/GS – Garmin GNC 255A
Intercom System (ICS) – Garmin GMA 350H
Transponder (mode S) – Garmin GTX 335R – ADS-B out capable
VHF/VOR/LOC/GPS – Garmin GTN 650H
Avionic display system Garmin G500H TXi

Engine(s)

1 x Turbomeca Arriel 2D turbine engine complete with starting, fuel supply and dual channel digital engine control system (FADEC) and 1 back up control that automatically controls the engine in case of total failure of the 2 digital channels of the FADEC
1 x fuel system including 1 tank of 540 litres (143 US Gallons) total capacity
1 x twist grip on pilot side (for engine reduction in the case of tail rotor failure and auto rotation training)
1 x magnetic plus and chip detector
1 x engine lubrication and oil cooling system
1 x fire detection system
1 x air intake protective grids
1 x torque measurement pick up

1 x 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 x main gearbox oil cooling system
1 x engine to main gearbox coupling shaft
1 x rotor brake
1 x main rotor high sensor and high and low RPM warning device
1 x tail drive carried by five anti friction bearings
1 x tail gearbox with oil sight gauge, chip detector and port for endoscopic inspection

Avionics

ICS installation compatible with Bose headsets
Hour meter

Equipment

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

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

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

Interior

Comfort layout

Six (6) Bose A20 blue tooth aviation headsets compatible with the ICS installation
2 x Ipad mounts fitted either side of the main instrument panel – compatible with Apple Ipad Mini – note: I pad mini’s NOT included

Cabin floor in light alloy sheet metal with tie down rings
Cabin floor has grey carpet
Pilot and co-pilot high back energy absorbing seats, adjustable in reach, removable, complete with cushions, safety belts and dual strap shoulder harness
2 jettisonable crew doors each fitted with sliding windows and improved side visibility windows: 1 large right hand front door and 1 LH front door
Hinged rear right door extension for passenger and cargo
1 left hand rear sliding door
Locks on every access to cabin and luggage compartments
Lock on fuel
2 tinted upper panes
1 ceiling housing the ventilation ducts and controls (ventilation controls, rotor brake and fuel cut off)
Cabin heating
Demisting system for front windscreen
Ram Air ventilation duct
•Fixed parts for pilot and co-pilot windshield wipers
1 pilot document holder
1 fire extinguisher
1 flight manual

Exterior

LH landing light (swivelling in elevation and azimuth)
Cargo swing (1400kg) (fixed parts)
Emergency floatation (fixed parts)

Helicopter painted Black / White – see pictures

Remarks

EASA or CAA registered and certified

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

Specifications and details are subject to verification upon inspection. Aircraft are offered
subject to prior sale or withdrawal from the market.

G-HITK Airbus H125

G-HITK Airbus H125

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