説明
Low-time Citation CJ1 with only two U.S. owners since new and equipped with Tamarack Active Winglets. Motivated Seller offers an attractive opportunity to acquire a well-maintained aircraft with improved performance and efficiency.仕様
年式2000
メーカーCESSNA
モデルCITATION CJ1
シリアル番号525-0374
Registration #N12GY
状態中古
Total Time2,035.2
Total Landings1,676
Max Ramp Weight4,853.44 kg
Max Takeoff Weight4,808.08 kg
Max Landing Weight4,445.21 kg
Max Zero Fuel Weight3,810.18 kg
Basic Empty Weight3,035.89 kg
Fuel Capacity1,460.57 kg
Wingletsはい
Engine 1 Maintenance ProgramNone
Engine 1 Make/ModelWILLIAMS FJ44-1A
Engine 1 Serial Number1695
Engine 1 Time2,035.2
Engine 1 Cycles Since Overhaul1,676
Engine 2 Make/ModelWILLIAMS FJ44-1A
Engine 2 Serial Number1694
Engine 2 Time2,035.2
Engine 2 Cycles Since Overhaul1,676
Flight Deck Manufacturer/ModelROCKWELL COLLINS PRO LINE 21
Avionics/RadiosCollins Pro Line 21
Dual Collins AHC-3000 AHRS Computers
Collins ADC-3000 Air Data Computers
Dual BendixKing KY-196B COMM Transceivers
Dual AlliedSignal KN-53 NAV Receivers
Dual BendixKing KT-74 Transponder
Universal UNS-1K Flight Management System
BendixKing KN-63 DME Receiver
L3Harris WX-1000E Stormscope
Collins AFD-3010 2-Tube
Collins RTA-800 Weather Radar
Artex 110-4 ELT
Additional EquipmentATLAS Tamarack Winglets
Dual Executive Writing Tables
Enclosed Lavatory
ExteriorThe aircraft is painted in a White Base with Hunter Green accent stripes.
InteriorThe five-passenger interior is configured with a four-place club arrangement in the main cabin, complemented by a single side-facing seat positioned opposite the forward entry door. All passenger seating is completed in camel leather, set against ivory patterned fabric sidewalls and pewter accent trim. Dual executive writing tables, finished in ebony wood with ivory laminate inlay, are fitted on both sides of the club arrangement. The aft lavatory is enclosed by a privacy curtain.
年式2000|
メーカーCESSNA|
モデルCITATION CJ1|
シリアル番号525-0374|
Registration #N12GY|
状態中古|
Total Time2,035.2|
Total Landings1,676|
Max Ramp Weight4,853.44 kg|
Max Takeoff Weight4,808.08 kg|
Max Landing Weight4,445.21 kg|
Max Zero Fuel Weight3,810.18 kg|
Basic Empty Weight3,035.89 kg|
Fuel Capacity1,460.57 kg|
Wingletsはい|
Engine 1 Maintenance ProgramNone|
Engine 1 Make/ModelWILLIAMS FJ44-1A |
Engine 1 Serial Number1695|
Engine 1 Time2,035.2|
Engine 1 Cycles Since Overhaul1,676|
Engine 2 Make/ModelWILLIAMS FJ44-1A |
Engine 2 Serial Number1694|
Engine 2 Time2,035.2|
Engine 2 Cycles Since Overhaul1,676|
Flight Deck Manufacturer/ModelROCKWELL COLLINS PRO LINE 21 |
Avionics/RadiosCollins Pro Line 21
Dual Collins AHC-3000 AHRS Computers
Collins ADC-3000 Air Data Computers
Dual BendixKing KY-196B COMM Transceivers
Dual AlliedSignal KN-53 NAV Receivers
Dual BendixKing KT-74 Transponder
Universal UNS-1K Flight Management System
BendixKing KN-63 DME Receiver
L3Harris WX-1000E Stormscope
Collins AFD-3010 2-Tube
Collins RTA-800 Weather Radar
Artex 110-4 ELT|
Additional EquipmentATLAS Tamarack Winglets
Dual Executive Writing Tables
Enclosed Lavatory|
ExteriorThe aircraft is painted in a White Base with Hunter Green accent stripes.|
InteriorThe five-passenger interior is configured with a four-place club arrangement in the main cabin, complemented by a single side-facing seat positioned opposite the forward entry door. All passenger seating is completed in camel leather, set against ivory patterned fabric sidewalls and pewter accent trim. Dual executive writing tables, finished in ebony wood with ivory laminate inlay, are fitted on both sides of the club arrangement. The aft lavatory is enclosed by a privacy curtain.|
