2007 LEONARDO AW139

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    Aircraft Location:Kuala Lumpur, マレーシア

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    Rotortrade

    お問い合わせ先:Aurelien Blanc

    電話番号:+60 12-267 8099

    +60 12-267 8099

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    仕様

    年式2007
    メーカーLEONARDO
    モデルAW139
    状態中古
    FlightRulesIFR
    Total Time3,228
    Max Takeoff Weight3,084.43 kg
    Basic Empty Weight2,106.03 kg
    AirframeYOM 31/1/2007 Total time 3,228 hours/15,018 cycles Configuration VIP Flight rule IFR Crew/passengers 2 crew/8 passenger Avionics phase 4 Highlights •LH and RH electrically operated passengers steps •Super silent soundproofing •Vibration absorber (3rd mass) •Emergency floats provision •Air conditioning system •Ripple damper •Moquette finishing on cabin floor •TCAS I, EGPWS, HF Antenna •Autopilot 4-axis software FDR enhanced
    Main Rotor Blade Time Remaining16772
    Main Rotor Gearbox Time Remaining1910
    Tail Rotor Gearbox Time Remaining4272
    Engine 1 Make/ModelPRATT & WHITNEY PT6C-67C
    Engine 1 Time3,228 SNEW
    Engine 1 TBO5000
    Engine(s)Engine 1 cycles 5,003 IMP/3,489 CT/4,095 PT
    Engine 2 Make/ModelPRATT & WHITNEY PT6C-67C
    Engine 2 Time2,924 SNEW
    Engine 2 TBO5000
    Engine 2 NotesEngine 2 cycles 4,602 IMP/2,999 CT/4,090 PT
    Radar Altimeterはい
    Auto Pilotはい
    ELTはい
    Airborne Weather Radarはい
    Traffic Avoidance Systemはい
    Avionics/Radios•Autopilot 4-axis software FDR enhanced •EGPWS Honeywell Mark 22 •Weather radar Primus 660 •TCAS I Honeywell KTA-970 model •Kit auxiliary battery 27 AH •HF Antenna •PFD and MFD x2 •ESIS (attitude, airspeed, altitude, vertical speed, compass and ILS data) •AHRS x2 •Air data module x2 •Flux valve x2 •Display controller x2 •Cursor control device x2 •Reversion control panel •Display dimming control panel •stability augmentation system control panel •Remote instrument controller x2 •Vehicle monitoring system x2 •Monitoring 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/HF Comm x2 •Mode S diversity transponder •VOR/LOC/GS/MB x2 •ADF •DME •MCDU x2 •Radar altimeter RT – 300 x2 •ELT – 121.5/243/406 MHz •Flight guidance controller •Honeywell GPS module with FPMS •Pilot and co-pilot digital audio panels remote ICS audio port for ground operation •Digital clock x2 •One magnetic compass •Master Warning Lights x2 •Master Caution Lights x2 •Engine 1 & 2 Fire Light x2 •Baggage compartment smoke detector light •Dual electrical power connection for CVR/FDR •CVR/FDR with ULB
    Dual Controlsはい
    Air Conditioningはい
    Baggage Compartmentはい
    Additional Equipment•LH and RH electrically operated passengers steps with light •Standard passenger cabin ceiling liners •Composite liners leather/leatherette covered •Dome lights •Moquette finishing on cabin floor •Cabin handles •Cabin loudspeakers •Passenger cabin thermo acustic double layer windows •Ripple damper •Vibration absorber (3rd mass) •Nose landing gear door •Super silent soundproofing •ICS in cabin for all passengers •Air conditioning system •Coat hangers x3 •Emergency floats provision •Crew crashworthy seats with inertial reels and safety belts •Cockpit dome/storm light •Cockpit utility lights x2 •28 V DC cockpit/cabin power outlet •Cockpit panel sun-glare shields •Overhead cockpit windows sun shades •Floor provisions for 15 seat configuration •Fluorescent lighted emergency exit signs •Cockpit map and data case in central console •Two flash lights for pilot and co-pilot •Map and data cases in pilot and co-pilot doors •ICS panel with plug for one headset •Air ventilation system •First aid kit
    Door Typeスライド式
    ConfigurationCorporate
    Number of Seats8
    Soundproofingはい
    年式2007|
    メーカーLEONARDO|
    モデルAW139|
    状態中古|
    FlightRulesIFR|
    Total Time3,228|
    Max Takeoff Weight3,084.43 kg|
    Basic Empty Weight2,106.03 kg|
    AirframeYOM 31/1/2007 Total time 3,228 hours/15,018 cycles Configuration VIP Flight rule IFR Crew/passengers 2 crew/8 passenger Avionics phase 4 Highlights •LH and RH electrically operated passengers steps •Super silent soundproofing •Vibration absorber (3rd mass) •Emergency floats provision •Air conditioning system •Ripple damper •Moquette finishing on cabin floor •TCAS I, EGPWS, HF Antenna •Autopilot 4-axis software FDR enhanced|
    Main Rotor Blade Time Remaining16772|
    Main Rotor Gearbox Time Remaining1910|
    Tail Rotor Gearbox Time Remaining4272|
    Engine 1 Make/ModelPRATT & WHITNEY PT6C-67C |
    Engine 1 Time3,228 SNEW |
    Engine 1 TBO5000|
    Engine(s)Engine 1 cycles 5,003 IMP/3,489 CT/4,095 PT|
    Engine 2 Make/ModelPRATT & WHITNEY PT6C-67C |
    Engine 2 Time2,924 SNEW |
    Engine 2 TBO5000|
    Engine 2 NotesEngine 2 cycles 4,602 IMP/2,999 CT/4,090 PT|
    Radar Altimeterはい|
    Auto Pilotはい|
    ELTはい|
    Airborne Weather Radarはい|
    Traffic Avoidance Systemはい|
    Avionics/Radios•Autopilot 4-axis software FDR enhanced •EGPWS Honeywell Mark 22 •Weather radar Primus 660 •TCAS I Honeywell KTA-970 model •Kit auxiliary battery 27 AH •HF Antenna •PFD and MFD x2 •ESIS (attitude, airspeed, altitude, vertical speed, compass and ILS data) •AHRS x2 •Air data module x2 •Flux valve x2 •Display controller x2 •Cursor control device x2 •Reversion control panel •Display dimming control panel •stability augmentation system control panel •Remote instrument controller x2 •Vehicle monitoring system x2 •Monitoring 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/HF Comm x2 •Mode S diversity transponder •VOR/LOC/GS/MB x2 •ADF •DME •MCDU x2 •Radar altimeter RT – 300 x2 •ELT – 121.5/243/406 MHz •Flight guidance controller •Honeywell GPS module with FPMS •Pilot and co-pilot digital audio panels remote ICS audio port for ground operation •Digital clock x2 •One magnetic compass •Master Warning Lights x2 •Master Caution Lights x2 •Engine 1 & 2 Fire Light x2 •Baggage compartment smoke detector light •Dual electrical power connection for CVR/FDR •CVR/FDR with ULB|
    Dual Controlsはい|
    Air Conditioningはい|
    Baggage Compartmentはい|
    Additional Equipment•LH and RH electrically operated passengers steps with light •Standard passenger cabin ceiling liners •Composite liners leather/leatherette covered •Dome lights •Moquette finishing on cabin floor •Cabin handles •Cabin loudspeakers •Passenger cabin thermo acustic double layer windows •Ripple damper •Vibration absorber (3rd mass) •Nose landing gear door •Super silent soundproofing •ICS in cabin for all passengers •Air conditioning system •Coat hangers x3 •Emergency floats provision •Crew crashworthy seats with inertial reels and safety belts •Cockpit dome/storm light •Cockpit utility lights x2 •28 V DC cockpit/cabin power outlet •Cockpit panel sun-glare shields •Overhead cockpit windows sun shades •Floor provisions for 15 seat configuration •Fluorescent lighted emergency exit signs •Cockpit map and data case in central console •Two flash lights for pilot and co-pilot •Map and data cases in pilot and co-pilot doors •ICS panel with plug for one headset •Air ventilation system •First aid kit|
    Door Typeスライド式|
    ConfigurationCorporate|
    Number of Seats8|
    Soundproofingはい|
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