manufacturer
Airbus
configuration
Utility
condition
New
year
2024
time
4.5
helicopter location
United Kingdom
listing ID
HT19979
Description
H125, YOM Nov. 2024, TT 4.5 hours, Dual Hydraulic, Dual controls, Slim Panel with G500H TXi, Tablet holder L/H & R/H, Helisas 2-Axis Autopilot, Fixed Provisions for Cargo Hook and Mirror, Cargo Hook Load Indicator, Fixed Provisions Floats, Windshield wipers, L/H sliding door, Bulked window R/H door, Bulked window L/H sliding door, Bose headsets x 6 with ICS, Cockpit camera, Transponder S - ADSB-Out, High Vis. Rotorblades.
Immediately available for sale
avionics
VFR Day and Night Package, with Integrated Flight Display with Garmin
G500H TXi included in Baseline Aircraft Definition
Emergency locator transmitter - Kannad INTEGRA 406 AP-H
VHFNOR/LOC/GS - Garmin GNC 255A
lntercom system (ICS) - Garmin GMA 350H
Transponder (mode S) - Garmin GTX 335R - ADS-B out
VHFNOR/LOC/GS/GPS - Garmin GTN 650Xi
Avionic display system Garmin G500H TXi lncluding:
Display- PFD RH Unit
Air Data Attitude and Heading Reference System Unit (ADAHRS)
Magnetometer Unit
Outside Air Temperature probe
equipment
Kit to increase lnternal Gross Weight to 2370 kg 5,225 Ib), including the Dual hydraulic circuit
First Aid Kit
High visibility paint scheme on main rotor blades (white, red or yellow strips)
(extrados) (red)
Tinted windows for standard and optional door configuration
Bulged window on right rea r door
Bulged window on left rear door
Pilot windshield wiper
Dual controls
Lean Instrument Panel (UP) in place of the baseline Instrument Panel Tablet holder on Lean Instrument Panel (UP)
Tablet holder on Lean Instrument Panel (UP) - R/H side
interior
Cabin floor in light-alloy sheet-metal with tie down
rings
2 pilot and co-pilot high-back energy-absorbing seats,
adjustable in reach, removable, complete with cushions, safety belts and dual-strap shoulder harnesses
2 two-place rear bench-seats, foldable separately, complete with cushions, safety belts and single-strap shoulder harnesses
2 pilot and co-pilot jettisonable doors each fitted with a sliding window and with improved side-visibility window
1 ceiling housing the ventilation duets and controls (ventilation controls, rotor brake and fuel cut oft)
Cabin heating
Demisting system for front windscreens
Ram air ventilation duet
engine 1
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 Crash Resistant Fuel System including 1 tank of 540 litres ( 143 U S 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 chip detector
1 engine lubrication and oil cooling system
1 fire detection system
1 air-intake protective grids
1 torque-measurement pick-up
