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Socata TBM 700
The TBM 700 is the first TBM, a pressurized single-engine turboprop for one pilot and five passengers, or six with an option. The TBM700 A was approved in France in January 1990, the B in 1998 and the C1 in 2002, and the C2 followed in 2004; all of them file under the ICAO code TBM7. The figures here are the EASA data sheet's for the TBM700 C2: a Pratt and Whitney Canada PT6A-64 of 700 shaft horsepower with a four-blade Hartzell propeller, a wingspan of 12.68 meters, a length of 10.65 meters, a maximum takeoff weight of 3,354 kg, 1,066 liters of usable fuel and a ceiling of 31,000 feet.
- Seats
- Up to 5 passengers
- Engines
- One Pratt and Whitney Canada PT6A-64 turboprop in the fuselage
- Max takeoff weight
- 7,400 lb (3,354 kg)
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Specifications
| Length | 34 ft 11 in (10.65 m) |
|---|---|
| Wingspan | 41 ft 7 in (12.68 m) |
| Height | 14 ft 3 in (4.36 m) |
| Ceiling | 31,000 ft (9,400 m) |
| Fuel capacity | 280 US gal (1,066 L) |
| Status | Still flying with a few operators |
| Type codes | ICAO TBM7 |
Private aircraft show specs and photos.