2015 Airbus H145 Turbine Helicopter (SOLD)

BK117D-2 in HEMS configuration, SP/DP IFR, NVIS Certified. Including full PbH and SbH funds, Includes fresh 800 hrs inspection, D3 conversion kit may follow.

Type:
Aircraft (Turbine Helicopter)
Manufacturer:
Airbus
Model:
H125
Year:
2015
Serial Number:
20039
Reg. Number:
LN-OOS
Total Time:
3,882 hours
Seats:
4
Price:
€6,500,000

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Description

Operated and based in Norway.
Fully covered by PbH and SbH contracts

• Aerolite Medical interior
EASA STC 10052111
EMS P/N 145-0045739-501
• Flightcell DZMx cellular and Iridium satellite
system, with GPS tracking solution
• Flightcell external WIFI router
• BAM Ice Grip Plate instead of standard wear
plates.
• Wireless intercom system Polycon NG
• Tactical radio VHF-FM NPX-138N – NVG
• Retrofit of Inlet Barrier Filter (IBF) system
• Increased T45 limits on both engines

Customized options configuration

Airbus Helicopters extra options from 2015
• Copilot flight controls
• Battery (44 Ah, 24 V) instead of standard
battery
• Electrical Heating System
• Additional electrical unit
• Dual landing & search light, 450W (white &
NVG)
• ELT AP-H Integra (ER)
• Night vision (NVIS) certification
• Surface protective coating (Airglaze)
• Cable cutter system
• Fuzz burner for engines, main transmission
and Fenestron® gearbox
• Improved heat protection for engine cowlings
• Engine compressor wash kit
• Vector Mast Moment System (VMMS, circular)
• Sliding doors fastener for intermediate and
max position
• Tinted sunshades
• Window in clam-shell door LH
• Push-out cabin windows
• Performance improvement kit for bleed air
heating system
• Alternating Current (AC) system
• Fuel management system (Fuel flow meters)
• Settling protectors
• External hoist, RH, fixed provisions
• Dual cargo hook
• Tail flood light for clam-shell doors
• Strobe lights
• Emergency floats (Safran)
• Separation curtain for cockpit/cabin
• Active vibration control system
• Washable floor covering for cockpit
• Height adjustable cockpit seats
• Jettisonable cockpit doors
• iPad holders for pilot and copilot with 5VDC
USB supply

Avionic Package single/dual pilot IFR
• Becker DVCS 6100 audio system with 3x ACU 6100,
pilot + copilot + cabin
• Transponder GTX 33 ES incl. mode S and ADS-B Out
(Garmin)
• Distance Measuring Equipment DME-4000 (Rockwell
Collins)
• Marker beacon receiver MKR3300-1 (Becker)
• GPS/NAV/COM GTN 750 (Garmin) pilot and copilot
w/COM 16w
• SBAS RNP approach capability
• Flight Display Subsystem (FDS), copilot
• Integrated Helicopter Terrain Awareness System
(HTAWS)
• Cockpit Voice and Flight Data Recorder (CVFDR)
• Lightweight Aircraft Recording System (LARS) Vision
1000 (Appaero)
• Cobham dual tetra radio system with dual control
head in cockpit and cabin (Provision only, no radios
or control panel delivered)
• Search and Rescue weather radar RDR-1600
(Telephonics)
• Traffic Advisory System TAS 620 (Avidyne)
• Synthetic Vision System (SVS)
• Moving map Euronav – RN 7 (Hensholdt Avionics)
interfaced with FDS, with the following:
• Sky track option (Iridium)
• GSM/UMTS option
• FLARM option

Standard helicopter definition
Basic instrumentation:
• Flight Display Subsystem (FDS) composed of 2
smart multifunction displays (6 x 8 inch) providing
the following functions:
o Flight Navigation Display (FND) format
o Vehicle Monitoring Display (VMD) format
• Vehicle Management Subsystem (VMS) including:
o 2 duplex Aircraft Management Computer
(AMC)
• Reference sensors:
o 3 Attitude and Heading Reference Systems
(AHRS)
o 2 Air Data sensors (electrically heated pitot
tube and static port)
o 2 Three Axis Magnetometers (TAM)
• Standby instruments:
o Integrated Electronic Standby Instrument
(IESI)
o Stand-by compass
• Usage Monitoring System (UMS)
• “One hundred feet” alert
• Directional Gyro Free Steering Mode
• Warning unit:
o Engine fire warning with fuel emergency
shut-off
o Warning lights
o Fire extinguishing system warning
• Cockpit Control Panel (CCP) for FDS
• Data Transfer Device (DTD)
• Engine switch panel:
o Digital engine control (FADEC)
• Radar altimeter

Transmission system:
• Main transmission including an independent
redundant lubrication system and monitoring
sensors
• Chip detector system with quick-disconnect plug
(main transmission)
• Free wheel assemblies in the engine input drives
• Rotor brake system
• Tail rotor transmission system with splash
lubrication and oil level sight gauge
• Chip detector system with quick-disconnect plug
(tail rotor gearbox)

Rotor and Flight controls:
• Hingeless main rotor (System Bölkow) with 4 glass
and carbon fiber reinforced blades with erosion
protection strip
• Fenestron®-type tail rotor with ten composite
blades (asymmetric blade spacing) and stator
• Tail rotor gearbox cover
• 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
• Main rotor blade tip painting (yellow)
• Mast moment system
• Dual Duplex 4-axis Digital Automatic Flight Control
System (AFCS) including upper modes

Power plant:
Two Safran Arriel 2E turbine engines with electronic
engine control (double channel FADEC)
• Crash resistant fuel system with a flexible bladdertype fuel main tank and supply tank (split into two
sections)
• Two independent oil cooling and lubrication
systems of the engines
• Fire detection and extinguishing system
• Chip detectors with quick-disconnect plugs
• Twin-engine OEI-training mode
• Automatically controlled variable rotor speed
system
• Cycle counter
• Drain system
• Fire wallS