1976 King Air 200
Description
The Beechcraft King Air 200 is a twin-engine turboprop aircraft that was designed and manufactured by Beechcraft. It is a variant of the King Air and has been in production since 1974. It is powered by two Pratt & Whitney PT6A-41 engines, each producing 850 horsepower. It has a cruising speed of 290 knots and a range of 1,500 nautical miles. The King Air 200 can carry up to nine passengers and has a maximum take-off weight of 13,500 pounds. It can operate from both land and sea and is primarily used for corporate and executive travel.
Features
- 9,516 Hours Total Time
- 8,605 Landings
- Engine(s)
- (2) Pratt & Whitney PT6A-41
- TT: 9,184 / 4,994
- TSOH: 2,732 / 1,493
- TBO: 3,600 / 3,600
- Hours Since Hot Section: 80 / 80
- Avionics
- Dual Garmin GMA1347D Audio Panels
- Dual Garmin GRS77 AHRS
- Garmin GFC700 Autopilot
- Dual Garmin GDC7400 ADC’s
- Garmin GWX70 Color Radar
- Dual Garmin GTX33ES Transponders
- Collins ALT-50A Radar Alt
- Collins DME-42
- L3 SKY899 TCAS1
- Garmin TAWS-B
- Garmin GDL69A Data Link
- Garmin Synthetic Vision
- XM Satellite Radio
- XM Satellite Weather
- Jeppesen Electronic Charts
- Mid-Continent MD302 Standby Attitude Module
- RVSM Capable
- ADS-B Out
- Maintenance Status
- Recent Phase 1 & 2
- Recent Landing Gear Overhaul
- Recent Prop Overhauls
- Features/Options
- Raisbeck 4 Blade Props
- Raisbeck Ram Air Recovery
- Raisbeck Dual Aft Body Strakes
- Raisbeck Enhanced Performance Leading Edges
- Hangar One, Inc. Ground Air Cooling System
- High Float Gear
- Cleveland Wheels & Brakes
- Cleveland Hot Air Manifold
- Concorde Lead Acid Battery
- Whelen LED Landing/Taxi Lights
- Rosen Sunvisor System
Location
