Performance Database
 |
|
King Air A/B90 |
|
Engines |
|
| Make | Pratt & Whitney |
| Model | PT6A-20 / PT6A-21 / PT6A-28 |
| HP/Thrust lbs per engine | 550 SHP |
| TBO (hours) | 3.600 |
Fuselage Dimension |
|
| Length (ft) | 36.50 |
| Height (ft) | 14.70 |
| Wing Span (ft) | 50.30 |
| Passengers | 2+6 |
| Pressurization (psi) | 4.6 |
Weights (lbs) |
|
| Max Ramp | 9.710 |
| Max Takeoff | 9.650 |
| Zero Fuel | 8.880 |
| Basic Operating | 6.345 |
| Max Landing | 9.170 |
Fuel Capacity |
|
| Standard lbs/gal | 2.573 / 384 |
Takeoff Performance (BFL) |
|
| SL ISA BFL (ft) | 2.260 |
| 5000 +20C BFL (ft) | 3.600 |
Landing Performance (ft) |
|
| FAA Field Length | 1.670 |
Range (NM) |
|
| Max Range | 1.175 |
Climb (SL ISA MTOW) |
|
| Normal (fpm) | 2.000 |
| Engine Out (fpm) | 555 |
Speeds (Knots) |
|
| Vso (Landing) | 74 |
| Normal Cruise TAS | 215 |
Ceiling (ft) |
|
| Certified Ceiling | 30.000 |
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.
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