Performance Database
 |
|
King Air 200 |
|
Engines |
|
| Make | Pratt & Whitney |
| Model | PT6A-41 / PT6A-42 |
| HP/Thrust lbs per engine | 850 |
| TBO (hours) | 3.600 |
Fuselage Dimension |
|
| Length (ft) | 43.80 |
| Height (ft) | 15.00 |
| Wing Span (ft) | 54.70 |
| Passengers | 2+8 |
| Pressurization (psi) | 6.0 |
Weights (lbs) |
|
| Max Ramp | 12.590 |
| Max Takeoff | 12.500 |
| Zero Fuel | 10.400 |
| Basic Operating | 7.940 |
| Max Landing | 12.500 |
Fuel Capacity |
|
| Standard lbs/gal | 3.645 / 544 |
Takeoff Performance (BFL) |
|
| SL ISA BFL (ft) | 3.445 |
| 5000 +20C BFL (ft) | 3.890 |
Landing Performance (ft) |
|
| FAA Field Length | 2.845 |
Range (NM) |
|
| Max Range | 1.870 |
Climb (SL ISA MTOW) |
|
| Normal (fpm) | 2.450 |
| Engine Out (fpm) | 740 |
Speeds (Knots) |
|
| Vso (Landing) | 75 |
| Normal Cruise TAS | 272 |
| Vmo (Max Operating) IAS | 260 |
Ceiling (ft) |
|
| Certified Ceiling | 31.000 |
Specifications are provided as introductory information only and
are subject to verification by the buyer during a prepurchase inspection
of the aircraft. The aircraft is offered subject to prior sale,
price changes and/or removal from the market without notice.
This website and all of its contents are owned and copyrighted by aircraftsales.com.
The use of any information without a written permission is strictly prohibited.
