Agusta AW139
2010 · USA
Description
Base data Type: Helicopter (Turbine) Make: Agusta Model: AW139 Year built: 2010 Attributes: IFR certified Commercially registered Location: United States, Pennsylvania Total Time (TTAF): 1720 h Price: on request No. of passengers: 6 Landings: 2789 Engine(s) Number of engines: 2 Make/Model: PT6C-67C PT6C-67C Total Time: 1720 h 1720 h TBO (hours): 5000 h 5000 h Description/Details of engines Engine 1 cycles 2,075 IMP/2,152 CT/2,493 PT Engine 2 cycles 1,988 IMP/2,029 CT/2,489 PT Avionics Moving Map Euronav V Lightning detector system Honeywell LSZ-860 Weather radar Primus 660 Honeywell TCAS 1 KTA-970 Honeywell Bendix/King EGPWS Transponder x2 DME x2 GPS x2 4 axis enhanced DAFCS with hover mode 5th central display SIRIO in cockpit SATCOM Iridium ST3100 Aircell PFD and MFD x2 AHRS x2 Air data modules x2 Flux valves x2 Display controllers x2 Cursor control devices x2 Reversion control panel Display dimming control panel SAS control panel Remote instrument controllers x2 Modular avionic units x2 Vehicle monitoring system x2 Monitor warning system x2 Aural warning generator Central maintenance computer Provision for CVR/FDR data interface Flight director system x2 Pilot and Co-pilot interphone control cyclic grip and floor switches VHF COMM x2 VOR/LOC/GS/MB x2 ADF Multi control function display units Radar altimeter RT-300 x2 Emergency Locator Transmitter (ELT) One Flight Guidance Controller Pilot and co-pilot digital audio panels with remote ICS audio port for ground operation Clock x2 Magnetic compass Outside air temperature indicator Master warning lights x2 Two master caution lights x2 Engine fire light x2 Baggage compartment smoke detector light CVR/FDR with ULB Equipment IBF Camera on tail fin Pilot and co-pilot approach plates charts holders Pilot and co-pilot headset hooks Emergency floats provisions Auxiliary heavy-duty battery 27 A/H Auxiliary transversal fuel tank 132 USG provision Secondary swivelling landing light Separation wall rolling curtain Cockpit entrance/exit handle Co-pilot storm window Cockpit tinted upper window Leather pocket on separation wall Painted pockets in pilot & co-pilot doors Passenger cabin hinged doors with specific ceiling and liners Electrically operated passenger's steps RH and LH with boarding lights Separation wall sliding window Nose landing gear doors AVCS Passenger cabin thermo acoustic double layer tinted windows ICS in cabin for all passengers Air conditioning Super silent soundproofing New "'Silent Shell cabin interior liners leatherette covered Other remarks YOM 2010 Total Time 1,720 hours/2,789 landings Configuration VIP Engine 2x PT6C-67C Avionics Phase 7 Flight rule Dual Pilot IFR Crew/passengers 2 crew/6 passengers Engine 1 TT 1,720 hours Engine 1 cycles 2,075 IMP/2,152 CT/2,493 PT Engine 1 TT 1,720 hours Engine 1 cycles 1,988 IMP/2,029 CT/2,489 PT MTOW 6,800 kgs Highlights Air conditioning Super silent soundproofing AVCS, HUMS, IBF Electrically operated passenger's steps RH and LH Auxiliary transversal fuel tank 132 USG provision Emergency floats provisions CVR/FDR with ULB, EGPWS 4 axis enhanced DAFCS with Hover mode Moving Map Euronav V Lightning detector system Honeywell LSZ-860 Weather radar Primus 660 Honeywell TCAS 1 KTA-970 Honeywell Bendix/King
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