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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 ...
The Ohio State vs. Indiana game will be played at noon ET on Saturday at Ohio Stadium. Watch Ohio State vs Northwestern FREE on Fubo. Ohio State vs Indiana odds. Odds courtesy of BetMGM as of ...
Ohio State will continue its 2023 home schedule Saturday afternoon.. Coming off a 35-7 win against Youngstown State in their home opener at Ohio Stadium, the Buckeyes will take the field in ...
Pages in category "SOCATA aircraft" The following 7 pages are in this category, out of 7 total. This list may not reflect recent changes. E. Socata TB 30 Epsilon; H.
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 ...
The SOCATA proposal, the TB 30B, was chosen in February 1979. [ 1 ] The first of two prototypes flew on 22 December 1979, [ 2 ] but testing showed that the Epsilon had poor handling and it was redesigned with a new swept back fin supplemented by a ventral strake and a larger tailplane , while the wing was fitted with elliptical tips increasing ...
The SOCATA TBM (now Daher TBM) is a family of high-performance single-engine turboprop business and utility light aircraft manufactured by Daher. It was originally collaboratively developed between the American Mooney Airplane Company and French light aircraft manufacturer SOCATA .
The Barnstormer was intended to meet the requirements of the US FAR 103 Ultralight Vehicles category, including that category's maximum 254 lb (115 kg) empty weight. [2] The aircraft is a single-seat ultralight with an unusual reverse-stagger on its biplane wings, the top wing being behind the bottom wing. The airfoil used is a NACA 2305 section.