2014 AIRBUS H145D2
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Aircraft Location:Alresford, United Kingdom
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Description
Specifications
Year2014
ManufacturerAIRBUS
ModelH145D2
Serial Number20010
ConditionUsed
Total Time6,661
Airframe NotesTotal Airframe Time: 6,661 hours (@ 1st Nov 2026)
Landings: 23,168 (@ 1st Nov 2026)
Location: Ahlen, Germany
Rotor and Flight Controls
Basic provisions for an easy integration of a balancing system
Dual hydraulic boost system for cyclic and collective blade control of the main rotor
Tail rotor control system with flexball cable and dual hydraulic booster
Vector Mast Moment System (VMMS)
Dual Duplex 4-axis Digital Automatic Flight Control System including upper modes
Electrical Installation
Two starter/generators (2 x 200 A, 28 VDC)
Nickel-Cadmium battery, (24 V, 44 Ah)
External power connector (STANAG 3302)
Two primary busbars
Two essential busbars
Two shedding busbars
Two non-essential busbars (80 A) - for optional equipment only
Battery bus
One utility receptacle in cargo compartment (28VDC, 20A)
DC power control
Lighting
Anti-collision warning light (red flashing), LED
Fixed landing light (250 W)
Three position lights (red, green, white), LED
Adjustable instrument lighting
One utility light in the cockpit
Lights in the cabin and cargo compartment
Engine 1 NotesTwo SAFRAN (TURBOMECA) ARRIEL 2E turbine engines with electronic engine control (double channel FADEC)
Crash resistant fuel system with a flexible bladder-type fuel main tank and supply tank (split into two sections)
Two independent oil cooling and lubrication systems of the engines
Chip detectors with quick-disconnect plugs
Twin-engine OEl-training mode
Automatically controlled variable rotor speed system
Fire detection and extinguishing system
Modifications/ConversionsInstallation of EMS Equipment BUCHER - AC70 EASA STC 10051657
Installation of EuroNav RN7 Moving Map - ALT Minor Change EC145-04094
Installation of Floor Protection Kit - ALT Minor Change H145-06388
Installation of Multifunction EMS Groundplate - EASA STC 10073970
Installation of ISEI Helicom V2 System - EASA STC 10047437
Installation of Trakka Control Panel - DRF Minor Change
Installation of bracket for scavenge pump LCSU4 - DRF Minor Change
Installation of Single Hand Latching Device - ALT Minor Change EC145-04103
Avionics/RadiosCOM/NAV/GPS #1 Garmin GTN 750
COM/NAV/GPS #2 Garmin GTN 750
DME Collins DME 4000
MKR Becker MKR3300-1
Audio Control Becker ACU 6100-2 (2 ICS – Pilot/Copilot)
Audio Control Becker ACU 6101-2 (2 ICS – Pax)
Radio Alt Bendix King KRA405B
XPDR Garmin GTX 33
ELT Kannad AP-H lntegra (ER)
WXRAD Honeywell ART 2000
TAS Avidyne TAS 620
Moving Map Euro Avionics RN7
FLARM Euro Avionics RN7
CVFDR L3 FA5001
ADC #1 Thales ADU 3200
ADC #2 Thales ADU 3200
Fixed provisions for tactical Com System (power supply, ICS interface, Antenna)
Flight Display Subsystem (FDS) composed of 2 smart multifunction displays 6x8 inch for Navigation & Vehicle monitoring
Vehicle Management Subsystem (VMS) including 2 duplex Aircraft Management Computer (AMC)
3 Attitude and Heading Reference Sensors (AHRS)
One hundred feet “alert”
2 Air Data sensors Directional Gyro Free Steering Mode
2 Three Axis Magnetometers (TAM)
Warning unit
Integrated Electronic Standby Instrument (IESI)
Data Transfer Device (DTD)
Stand-by compass
Engine switch panel
Usage Monitoring System (UMS)
Radar altimeter
Additional EquipmentEnergy absorbing fuselage
Map case in pilot's & copilot´s door
Cold weather kit
Two rear hinged clam-shell doors
7" copilot instrument panel with glare shield
Copilot flight controls
Map case in copilot door Built-in maintenance steps and grips
Tinted sunshades for cockpit windshield
Ventilation for avionics deck
Engine compressor wash kit Headset holder in the cockpit, rotatable
Sliding door fastener, max. position, LH & RH
Windscreen wiper for pilot and copilot
Long boarding steps, LH and RH
Door open warning
Window in clam-shell door, RH
Cable cutter system, fixed provisions
Bleed air heating system
Height adjustable pilot & copilot seat
Glazed canopy
Two hinged cockpit doors with sliding window
Ram-air and electrical ventilating system for cockpit and cabin
Longitudinally adjustable energy absorbing pilot and copilot seats with head rest
Fuzz burner for engines, main transmission and Fenestron gearbox
Instrument panel with extension on pilot's side and glare shield
Illuminated chart holder, pilot & copilot side
Two wide passenger sliding doors with window of pushout type
Interior panelling with integrated basic sound insulation
One-level cabin and cargo compartment floor with integrated rails
Specific Mission Equipment
S/L LIGHT 400/200W DIMMABLE
2nd portable fire extinguisher
NVG compatible standard cockpit, cabin and cargo compartment
Settling protectors, fixed provisions & detachable parts
ELT AP-H INTEGRA (ER) (Kannad)
Separation curtain for cockpit/ cabin, fixed provisions
Curtain cockpit/cabin washable DP
Snow skids, fixed provisions
Strobe lights
Searchlight Trakka, basic LH FWD, fixed provisions