1987 Beechcraft King Air C90A
Description
The Beechcraft King Air C90A is a twin turboprop aircraft, manufactured by Beechcraft. It is a version of the King Air series and entered service in 1994. The King Air C90A features a maximum cruise speed of 270 knots, a range of 1,500 nautical miles, and a maximum payload of 1,800 lbs. It is powered by two Pratt & Whitney PT6A-21 turboprop engines and can seat up to 8 passengers. It is commonly used for passenger and cargo transport, as well as aerial survey and observation missions. The King Air C90A has an airframe life of 25,000 flight hours or 36,000 cycles, whichever comes first.
Features
- Total Time: 7165
- Engine 1 Time: 2650 SMOH
- Engine 2 Time: 2650 SMOH
- MFD: Avidyne EX-500 w/XM Weather and Radar
- GPS: Avidyne IFD-540 Touch Screen
- WAAS FMS/GPS/NAV/COM/WIFI/BT/FLTA/SVS with ADSB OUT
- Audio System: Dual King DB-415 Audio System
- #2 Nav: King KNR-634
- #2 Com: King KTR-908
- Transponder: Avidyne IFD-540 ADS-B Out
- Encoder: Trans-Cal Blind Encoder
- DME: King KDM-706
- ADF: King KDF-806
- Radar: Bendix RDS-81
- Radar Altimeter: King KRA-10A
- HSI: King KPI-552 and KI-525A
- King KFC-250 Autopilot and Flight Director
- BFG WX11 Stormscope
- Shadin DIGIDATA Fuel Flow / Airdata Computer
Location
