説明
Aircraft based and registered in Brazil.
All maintenance current controlled by CAMP.
Engine Program: ESP.
Airframe Program: Embraer Corporate Care Standard.
Equipped w/ ADS-B, Galley and Belted Lavatory.
Executive interior configured for 6 passengers + 1 pilot.
No accident or incident history.
Always kept in hangar.仕様
年式2011
メーカーEMBRAER
モデルPHENOM 100
状態中古
Total Time4,400
Maintenance TrackingCamp
Parts Maintenance ProgramEEC
Engine 1 Maintenance ProgramESP
Engine 1 Make/ModelPRATT & WHITNEY PW617F
Engine 1 Time2,300 SNEW
Engine 1 TBO3500
Engine 1 Notes1,200 Remaining Hours
Engine 2 Make/ModelPRATT & WHITNEY PW617F
Engine 2 Time2,250 SNEW
Engine 2 TBO3500
Engine 2 Notes1,250 Remaining Hours
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
Belted Lavatory
InteriorExecutive interior configured for 6 passengers + 1 pilot.
Inspection StatusAll maintenance current controlled by CAMP.
Airworthyはい
年式2011|
メーカーEMBRAER|
モデルPHENOM 100|
状態中古|
Total Time4,400|
Maintenance TrackingCamp|
Parts Maintenance ProgramEEC|
Engine 1 Maintenance ProgramESP|
Engine 1 Make/ModelPRATT & WHITNEY PW617F |
Engine 1 Time2,300 SNEW |
Engine 1 TBO3500|
Engine 1 Notes1,200 Remaining Hours|
Engine 2 Make/ModelPRATT & WHITNEY PW617F |
Engine 2 Time2,250 SNEW |
Engine 2 TBO3500|
Engine 2 Notes1,250 Remaining Hours|
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
Belted Lavatory|
InteriorExecutive interior configured for 6 passengers + 1 pilot.|
Inspection StatusAll maintenance current controlled by CAMP.|
Airworthyはい|
