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Beechcraft King Air A100
The A100 is the King Air 100 approved by the FAA in May 1971, also flown by the US Army as the U-21F; the first Model 100 was approved in July 1969, and the A100A, A100C and B100 followed under the same code, BE10. Two Pratt and Whitney Canada PT6A-28 or PT6A-34 turboprops of 680 shaft horsepower turn four-blade Hartzell propellers 90 inches across. The FAA data sheet gives a maximum takeoff weight of 11,500 lb, or 5,216 kg, up to 15 seats including 2 for the crew, 470 US gallons of fuel and a maximum operating altitude of 31,000 feet. No source read gives its dimensions, so this page has no drawing.
- Seats
- Up to 13 passengers
- Engines
- Two Pratt and Whitney Canada PT6A-28 or PT6A-34 turboprops on the wings
- Max takeoff weight
- 11,500 lb (5,216 kg)
Photos from members
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Specifications
| Ceiling | 31,000 ft (9,400 m) |
|---|---|
| Fuel capacity | 470 US gal (1,779 L) |
| Status | Still flying with a few operators |
| Type codes | ICAO BE10 |
Private aircraft show specs and photos.