1979 PIPER NAVAJO CHIEFTAIN
説明
1979 Piper Navajo Chieftain – C-GMKO
Well-maintained 1979 Piper Navajo Chieftain featuring upgraded Garmin avionics and recent engine overhauls. This aircraft offers a strong combination of performance, reliability, and comfort — ideal for charter, corporate, or private operations. Equipped with a cargo door, air conditioning, and numerous STC upgrades, C-GMKO is ready for work or travel.
Airframe
Total Time: 15,016 Hours
Engines
Lycoming TIO-540-J2BD (350 HP each)
Left Engine: 2,019.7 Hours SMOH
Right Engine: 1,004.1 Hours SMOH
Propellers
Hartzell HC-E3YR-2ATF (3-Blade Constant Speed)
Avionics
Garmin GNS-430W (GPS/NAV/COMM)
Garmin GNS-530W (GPS/NAV/COMM)
Garmin GMA-340 Audio Panel
Garmin GTX-330 Transponder
Collins DME-451
KR-87 ADF
Artex 406 MHz ELT
TDR-950
Equipment & Features
Cargo Door
Air Conditioning
Oxygen System
Tanis Engine Heaters
Cleveland Wheels & Brakes
Electric Propeller Anti-Ice System
STCs & Modifications
VG Kit – Gross Weight Increase (SA00192SE)
Landing Weight Increase Kit (SA00202SE)
Wing Rib Reinforcement (SA00378SE)
Concorde RG-24-20 Battery Installation (SA01147)仕様
年式1979
メーカーPIPER
モデルNAVAJO CHIEFTAIN
シリアル番号31-7952063
Registration #C-GMKO
状態中古
FlightRulesIFR
Total Time15,016
Max Takeoff Weight3,175.15 kg
Fuel Capacity Volume401.25 L
Complete Logsはい
Engine 1 Make/ModelLYCOMING TIO-540-J2BD
Engine 1 Horsepower260.99 kW
Engine 1 Time2,019.7 SMOH
Engine 1 TBO1800
Engine 1 Turbochargedはい
Engine 2 Make/ModelLYCOMING TIO-540-J2BD
Engine 2 Horsepower260.99 kW
Engine 2 Time1,004.1 SMOH
Engine 2 TBO1800
Engine 2 Turbochargedはい
Prop 1 ManufacturerHARTZELL
Prop 1 ModelHC-E3YR-2ALTF
Prop 1 Time2919.1 SMOH
Prop 2 ManufacturerHARTZELL
Prop 2 ModelHC-E3YR-2ATF
Prop 2 Time2919.1 SMOH
Vortex Generatorsはい
Modifications/ConversionsSTCs & Modifications
VG Kit – Gross Weight Increase (SA00192SE)
Landing Weight Increase Kit (SA00202SE)
Wing Rib Reinforcement (SA00378SE)
Concorde RG-24-20 Battery Installation (SA01147)
GPS 1 ManufacturerGARMIN
GPS 1 ModelGNS430W
GPS 2 ManufacturerGARMIN
GPS 2 ModelGNS530W
Transponder 1 ManufacturerGARMIN
Transponder 1 ModelGTX330
WAASはい
Avionics/RadiosGarmin GNS-430W (GPS/NAV/COMM)
Garmin GNS-530W (GPS/NAV/COMM)
Garmin GMA-340 Audio Panel
Garmin GTX-330 Transponder
Collins DME-451
KR-87 ADF
Artex 406 MHz ELT
TDR-950
Oxygen Systemはい
Air Conditioningはい
Additional EquipmentEquipment & Features
Cargo Door
Air Conditioning
Oxygen System
Tanis Engine Heaters
Cleveland Wheels & Brakes
Electric Propeller Anti-Ice System
Number of Seats8
ConfigurationPassenger
Airworthyはい
年式1979|
メーカーPIPER|
モデルNAVAJO CHIEFTAIN|
シリアル番号31-7952063|
Registration #C-GMKO|
状態中古|
FlightRulesIFR|
Total Time15,016|
Max Takeoff Weight3,175.15 kg|
Fuel Capacity Volume401.25 L|
Complete Logsはい|
Engine 1 Make/ModelLYCOMING TIO-540-J2BD |
Engine 1 Horsepower260.99 kW|
Engine 1 Time2,019.7 SMOH |
Engine 1 TBO1800|
Engine 1 Turbochargedはい|
Engine 2 Make/ModelLYCOMING TIO-540-J2BD |
Engine 2 Horsepower260.99 kW|
Engine 2 Time1,004.1 SMOH |
Engine 2 TBO1800|
Engine 2 Turbochargedはい|
Prop 1 ManufacturerHARTZELL|
Prop 1 ModelHC-E3YR-2ALTF|
Prop 1 Time2919.1 SMOH |
Prop 2 ManufacturerHARTZELL|
Prop 2 ModelHC-E3YR-2ATF|
Prop 2 Time2919.1 SMOH |
Vortex Generatorsはい|
Modifications/ConversionsSTCs & Modifications
VG Kit – Gross Weight Increase (SA00192SE)
Landing Weight Increase Kit (SA00202SE)
Wing Rib Reinforcement (SA00378SE)
Concorde RG-24-20 Battery Installation (SA01147)|
GPS 1 ManufacturerGARMIN|
GPS 1 ModelGNS430W|
GPS 2 ManufacturerGARMIN|
GPS 2 ModelGNS530W|
Transponder 1 ManufacturerGARMIN|
Transponder 1 ModelGTX330|
WAASはい|
Avionics/RadiosGarmin GNS-430W (GPS/NAV/COMM)
Garmin GNS-530W (GPS/NAV/COMM)
Garmin GMA-340 Audio Panel
Garmin GTX-330 Transponder
Collins DME-451
KR-87 ADF
Artex 406 MHz ELT
TDR-950|
Oxygen Systemはい|
Air Conditioningはい|
Additional EquipmentEquipment & Features
Cargo Door
Air Conditioning
Oxygen System
Tanis Engine Heaters
Cleveland Wheels & Brakes
Electric Propeller Anti-Ice System|
Number of Seats8|
ConfigurationPassenger|
Airworthyはい|
