TBM 850

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    TBM 850 is high performance single engine turboprop light business and utility aircraft manufactured by SOCATA. The TBM 700 was offered until 2006, when the TBM 850 was introduced.

    The TBM 850 is the production name for the TBM 700N, an improved version with the more powerful Pratt & Whitney PT6A-66D engine flat rated at 850 shp (634 kW). The TBM 850 is limited to 700 shp (522 kW) for takeoff and landing, but in cruise flight the engine power can be increased to 850 shp (634 kW). This extra power gives it a higher cruising speed than the TBM 700 models, especially at high altitudes (due to the flat-rating). The outside appearance of the TBM 850 has remained the same as that of the TBM 700. The TBM 850 has a typical range of 1,520 nautical miles (2,820 km).

     

    General characteristics

     

    Crew: 1 or 2 pilots

    Capacity: 4 to 6 (including one passenger in the cockpit if there is no co-pilot)

    Length: 10.65m (34 ft11 in)

    Wingspan: 12.68m (41 ft7 in)

    Height: 4.36m (14 ft3 in)

    Wing area: 18m2 (193.7ft2)

    Empty weight: 2,132 kg (4,699 lb)

    Max. takeoff weight: 3,354 kg (7,394 lb)

    Powerplant: 1 × Pratt & Whitney Canada PT6A-66D turboprop, 634 kW (850 hp)

    Max payload full fuel: 385 kg (849 lb)

     

    Performance

     

    Maximum speed: 593 km/h (320 knots, 368 mph)

    Cruise speed: 467 km/h (252 kts, 290 mph)

    Range: 2,813 km (1,519 nm, 1,784 mi)

    Service ceiling: 9,450 m (31,000 ft)

    Rate of climb: 12.09 m/s (2,380 ft/min)

    Time to climb to 26,000 ft: 15 min

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