THC 001 - King-Air B200 Tech Data sheet Last revision: 22.12.1999
| PERFORMANCE | U.S. | METRIC | | Max Cruise Speed (336 mph) | 292 kt | 541 kph | | Certified Ceiling | 35,000 ft | 10,668 m | | Max Range | 1,883 nm | 3,487 km | ENGINES: Pratt & Whitney | | PT6A-42 | 850 shp | | WEIGHTS | Basic operating weight (Std. BEW plus one pilot at 200 lb) | 8,420 lb | 3,819 kg | | Useful load | 4,170 lb | 1,891 kg | DIMENSIONS (External) | | Wingspan | 54 ft 6 in | 16.61 m | | Max airplane length | 43 ft 9 in | 13.34 m | | Max tail height | 15 ft 0 in | 4.57 m | DIMENSIONS (Internal) CABIN | | Length | 16 ft 8 in | 5.08 m | | Height | 4 ft 9 in | 1.45 m | | Width | 4 ft 6 in | 1.37 m | | | | | | | | PM Data: | | | | | | | 2* Turboprop | 0.55 lb/lb*h | | | redline rpm | 2000 | | | reverse pitch | yes | | | Prop | 3 blades | | | 4.2 ft rad. | | | 178 in/rev. | | | | | | Optimal RPM | 1800 | | | Optimal Speed | 264 kts | | | | | | Empty weight: | 8158 lb | | | Max. weight: | 12590 lb | | | Fuel load: | 3645 lb | | | | | | Vso | 75 kts | | | Vs | 99 kts | | | Vfe | 200 kts | | | Vno | 259 kts | | | Vne | 259 kts | | | Mmo | 0.53 | | | | | | | | | | | | | Aircraft Logbook & Data Pilot Operating Handbook (PDF - download) Current Location History Stall Chart Flight licence Request (download)
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