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Beechcraft Super King Air 300
The Super King Air 300 is the first of the 300 series, approved by the FAA in January 1984, with the lighter 300LW following in 1988; the later 350 and 360 file under a different ICAO code, B350. Two Pratt and Whitney Canada PT6A-60A turboprops of 1,050 shaft horsepower turn four-blade Hartzell propellers up to 105 inches across. The FAA data sheet gives a maximum takeoff weight of 14,100 lb, or 6,396 kg, up to 15 seats including the crew, 539 US gallons of usable fuel and a maximum operating altitude of 35,000 feet. No source read gives its dimensions, so this page has no drawing.
- Engines
- Two Pratt and Whitney Canada PT6A-60A turboprops on the wings
- Max takeoff weight
- 14,100 lb (6,396 kg)
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Specifications
| Ceiling | 35,000 ft (10,700 m) |
|---|---|
| Fuel capacity | 540 US gal (2,040 L) |
| Status | In service |
| Type codes | ICAO BE30 |
Private aircraft show specs and photos.