1980 King Air F90
Description
The King Air F90 was a twin-engined turboprop aircraft produced by Beechcraft from 1980 until 1992. It was the successor to the King Air E90 and the predecessor to the King Air 200. The aircraft was powered by two Pratt & Whitney Canada PT6A-135 engines and had a maximum take-off weight of 12,500 lbs. It had a maximum speed of 355 mph, a range of 1,400 miles, and a service ceiling of 35,000 feet. It typically seated up to eight passengers, with a maximum of nine.
Features
- Total Time 10,906
- Engine(s)
- Pratt & Whitney PT6A-135
- Serial Number: PCE92113 / PCE92125
- Time Since Overhaul: 3,680 / 3,680
- Time Between Overhauls: 8,000 / 8,000
- Engines Overhauled by Dallas Airmotive (4/2002)
- Prop Details
- Hartzell 4-Blade Constant-Speed Reversible Props
- Serial Number: EAA-1621 / CDA-3883
- Time Since Overhaul (4/2016): 560 / 560
- Prop overhaul done by H&H Propeller Service (2016)
- Avionics
- Sperry/King/Collins/Bendix
- King Multi-Function Display
- Electric Trim
- Full Copilot Instruments
- ADS-B Out
- Raisbeck Dual Aft Body Strakes
- Nacelle Wing Lockers
- Electronic Flight Bag
- Hartzell 4-Blade Constant-Speed Reversible Props with Autofeather
- Rudder Boost
- High Flotation Gear
- Window Polarizers
- Maintenance Status
- Available Upon Request
- Complete English Logbooks
Location
