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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 ...
Download as PDF; Printable version; In other projects Wikidata item; Appearance. ... SOCATA TBM-700; SOCATA TBM-850; SOCATA TBM-900; SOCATA Gabier; SOCATA 110ST ...
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).
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 ...
Single engine piston aircraft with tricycle landing gear [1]; Model Engine Power hp Seats Wing Sq. Ft. MTOW lb Empty lb Cruise knots Range nmi AS 202 Bravo NG: L. AEIO-360: 180: 3: 149: 2,202: 1,389
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 ...
Download as PDF; Printable version; In other projects Wikidata item; ... Daher TBM 700; Daher TBM 850; Daher TBM 900; Daher TBM 910; Daher TBM 930; Daiichi Kosho.
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