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The TBM 850 is the production name for the TBM 700N, an improved version of the aircraft powered by a single Pratt & Whitney PT6A-66D engine, which is flat rated at 850 shp (634 kW). The TBM 850 is limited to 700 shp (522 kW) for takeoff and landing; however, during cruise flight, the engine power can be increased to 850 shp (634 kW); this ...
A tactical ballistic missile (TBM), or battlefield range ballistic missile (BRBM), is a ballistic missile designed for short-range battlefield use. Typically, range is less than 300 kilometres (190 mi).
A TBF-1 dropping a torpedo TBM-3Ds of VT(N)-90 January 1945 Six U.S. Navy Grumman TBM-3E Avenger anti-submarine aircraft of Composite Squadron VC-22 Checkmates flying over the Mediterranean Sea US Navy TBMs (foreground) and SB2C Helldivers drop bombs on Hakodate in July 1945 A TBM-3R COD plane in the early 1950s TBM-3W TBF Avenger Torpedo ...
Retrieved from "https://en.wikipedia.org/w/index.php?title=Socata_TBM-850&oldid=317414771"This page was last edited on 2 October 2009, at 04:12 (UTC). (UTC).
Ballistic missiles vary widely in range and use, and are often divided into categories based on range. Various schemes are used by different countries to categorize the ranges of ballistic missiles: Tactical ballistic missile (TBM): Range less than 300 km; Short-range ballistic missile (SRBM): Range from 300 to 1,000 kilometres (190 to 620 mi)
The following is a partial list of ICAO type designators for a range of multi-engined and turbine aircraft, with corresponding IATA type codes where available ...
The history of SOCATA can be traced back to the founding of the French aircraft manufacturer Morane-Saulnier in 1911. During 1966, Morane-Saulnier changed its name to SOCATA (which is an abbreviation for Societe de Construction d'Avions de Tourisme et d'Affaires, French for "Company for the construction of aircraft for tourism and business") following the company's acquisition by the state ...
Data from www.socata.org SOCATA TB user group and TB21 POH General characteristics Crew: 1 Capacity: 4 passengers Length: 7.75 m (25 ft 5 in) Wingspan: 9.85 m (32 ft 4 in) Height: 2.85 m (9 ft 4 in) Airfoil: RA 16 3C3 Empty weight: 911 kg (2,008 lb) EFIS and MTV 9 propeller Max takeoff weight: 1,400 kg (3,086 lb) Fuel capacity: 336 Liters (88.8 U.S. Gallons) Powerplant: 1 × LYCOMING TIO-540 ...