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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 ...
SOCATA ST 10 Diplomate; SOCATA Rallye; SOCATA TB-9 Tampico; SOCATA TB-10 Tobago; SOCATA TB-11 – Powered by a 134-kW (180-hp) engine. SOCATA TB-15 – Proposed version. Not built. SOCATA TB-16 – Proposed version. Not built. SOCATA TB-20 Trinidad; SOCATA TB-21 Trinidad; SOCATA TB-30 Epsilon; SOCATA TB-60 [citation needed] SOCATA TB-200 Tobago ...
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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 ...
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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 .
I know the TB-200 has a 2-bladed constant speed propeller. I know the TB-10 has a 2-bladed propeller, but not sure whether fixed pitch or constant speed. It appears the TB-20 was offered with either 2-bladed or 3-bladed constant speed propellers; It appears that all TB-21 have a 3-bladed constant speed propeller.