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General| Manufacturer | Beechcraft |
|---|---|
| Model | KING AIR C90A |
| Engine | Pratt & Whitney Canada PT6A-21 |
| Number of Engines | 2 |
| Height | 14 ft 3 in (4.34 m) |
| Max Takeoff Weight | 10, 100 lb (4, 581 kg) |
| Service Ceiling | 30, 000 ft (9, 144 m) |
| Cabin Height | 4 ft 9 in (1.45 m) |
| Crew | 1-2 |
| Seating Capacity | 8 |
| Type | Twin-turboprop aircraft |
| Engine Power | 550 shp (410 kW) each |
| Passenger Capacity | 7 |
Outlines critical operating limits for the power plant systems.
Details the maximum permissible weights for various operational phases.
Specifies the allowable center of gravity ranges for the aircraft.
Procedures for engine failure during the take-off phase.
Data and charts for aircraft takeoff and climb performance.
Performance data for normal cruise at 1750 RPM.
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