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Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.2 or any later version published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts.
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 ...
Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.2 only as published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts.
Stauffer and the pilot, his fiancee Karen Dodds, were in a Socata TB-20 Trinidad when the plane disappeared. Searchers find a missing plane and human remains in Michigan's Lake Huron after 17 ...
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 ...
Utility aircraft; ATR 72 Italy: Utility/Transport: C-72 3 [36] Built under Meltem-III project by TAI and Alenia Aermacchi. [33] CASA CN-235 Spain: CN-235M-100 1 [37] Leased from Air Force for one year for transport and training purposes. [38] [39] Trainer aircraft; SOCATA TB Family [40] France: Basic trainer: TB-20 4 [40] Unmanned aerial ...
In 1995 the type certificate for the GA-7 was sold to SOCATA of France who intended to produce the aircraft as the TB 320 Tangara for the training market. [5] It was also to develop a variant with two Lycoming O-360-A1G6 engines of 180 hp (134 kW) each and a re-designed cockpit, it was designated the TB 360. The first Tangara was a modified ...
The new aircraft was expected to have tandem seating, be powered by a 224 kW (300 hp) piston engine and have a three-hour endurance. Similar designs were proposed by the SOCATA subsidiary of Aérospatiale (based on their TB 10 Tobago light aircraft) and by GEPAL (the GEPAL Mk II). The SOCATA proposal, the TB 30B, was chosen in February 1979. [1]
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