説明
Aircraft based and registered in Brazil.
All maintenance current controlled by CAMP.
Airframe Program: EEC Enhanced.
Engine Program: JSSI 100%.
Equipped w/ ADS-B and Galley.
Executive interior configured for 5 passengers + 1 pilot.
Always kept in hangar.仕様
年式2009
メーカーEMBRAER
モデルPHENOM 100
状態中古
Total Time3,200
Maintenance TrackingCamp
Parts Maintenance ProgramEEC Enhanced
Engine 1 Maintenance ProgramJSSI
Engine(s)JSSI 100%
Engine 1 Make/ModelPRATT & WHITNEY PW617F
Engine 1 Time3,200 SNEW
Engine 1 TBO3500
Engine 1 Notes300 Hours Remaining
Engine 2 Make/ModelPRATT & WHITNEY PW617F
Engine 2 Time3,200 SNEW
Engine 2 TBO3500
Engine 2 Notes300 Hours Remaining
Avionics/RadiosGarmin G1000 “Prodigy” Avionics Suite
Triple 12” Garmin Displays
Autopilot
Garmin GFC-700 AFCS (Automatic Flight Control System)
Class-B TAWS (Terrain Awareness and Warning System)
Dual Garmin GTX-33D Mode S Transponder with Diversity
ADSB-Out
Digital Weather Radar
Dual AHRS (Attitude Heading and Reference System)
Dual RVSM Compliant Digital Air Data Computers
Dual Radio Modules
Dual Digital Auto Control Systems
EICAS (Engine Indication and Crew Alerting System)
Computer like Functionality
Additional EquipmentCockpit Sunshades and Sunvisor
Cockpit Seats Sheepskin Cover
Cockpit Flood Lights
Air Conditioning
InteriorExecutive interior configured for 5 passengers + 1 pilot.
Inspection StatusAll maintenance current controlled by CAMP.
Airworthyはい
年式2009|
メーカーEMBRAER|
モデルPHENOM 100|
状態中古|
Total Time3,200|
Maintenance TrackingCamp|
Parts Maintenance ProgramEEC Enhanced|
Engine 1 Maintenance ProgramJSSI|
Engine(s)JSSI 100%|
Engine 1 Make/ModelPRATT & WHITNEY PW617F |
Engine 1 Time3,200 SNEW |
Engine 1 TBO3500|
Engine 1 Notes300 Hours Remaining|
Engine 2 Make/ModelPRATT & WHITNEY PW617F |
Engine 2 Time3,200 SNEW |
Engine 2 TBO3500|
Engine 2 Notes300 Hours Remaining|
Avionics/RadiosGarmin G1000 “Prodigy” Avionics Suite
Triple 12” Garmin Displays
Autopilot
Garmin GFC-700 AFCS (Automatic Flight Control System)
Class-B TAWS (Terrain Awareness and Warning System)
Dual Garmin GTX-33D Mode S Transponder with Diversity
ADSB-Out
Digital Weather Radar
Dual AHRS (Attitude Heading and Reference System)
Dual RVSM Compliant Digital Air Data Computers
Dual Radio Modules
Dual Digital Auto Control Systems
EICAS (Engine Indication and Crew Alerting System)
Computer like Functionality|
Additional EquipmentCockpit Sunshades and Sunvisor
Cockpit Seats Sheepskin Cover
Cockpit Flood Lights
Air Conditioning|
InteriorExecutive interior configured for 5 passengers + 1 pilot.|
Inspection StatusAll maintenance current controlled by CAMP.|
Airworthyはい|
