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Beechcraft Baron 58P and 58TC
The 58P and 58TC are the turbocharged Baron 58s: the FAA approved the 58P, with a pressurized cabin, in 1974 and the unpressurized 58TC in 1976. Both first had Continental TSIO-520-L engines and later two 325 hp TSIO-520-WB. The figures are the later 58P's, from the FAA data sheet: two 325 hp TSIO-520-WB engines, a maximum weight of 6,200 pounds, 166 US gallons of usable fuel with the standard tanks and a maximum operating altitude of 25,000 feet. It seats four, and up to six with the optional seats.
- Seats
- About 4 (up to 6)
- Engines
- Two piston engines on the wings: Continental TSIO-520-WB; TSIO-520-L or TSIO-520-LB on early aircraft
- Max takeoff weight
- 6,200 lb (2,812 kg)
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Specifications
| Fuselage width | 4 ft 1 in (1.25 m) |
|---|---|
| Ceiling | 25,000 ft (7,600 m) |
| Fuel capacity | 170 US gal (628 L) |
| Status | In service |
| Type codes | ICAO B58T |
Private aircraft show specs only. No flight data is shown for them.