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Socata TB-20 Trinidad SX-ATK

Pictures of Socata TB20 Trinidad SX-ATK based at Megara, Athens.

Specific Socata TB-20 spec's: S.No. 1800, year 1996 model, 250Hp Fuel Injected Lycoming IO-540 engine, 2 blade Hartzell Constant Speed Propeller, Retractable landing gear, main gear with trailing link suspension, 150 Kts TAS cruise, 25 Kts demonstrated crosswind limit, 5 passengers, 1400 Kg MTOW, 490 Kg useful load, 86 US Gal's AVGAS fuel capacity, 6.5 hrs Endurance, 900nm operational range. Two axis KFC150 Autopilot with Altitude Capture, IFR instrumentation incl. 8,33Khz comm's, Air Data Computer and Mode S Transponder, TAS (Avidyne Traffic Info.) displayed in GNS530 GPS, L3 Stormscope.

An article in Aviation Consumer on the Socata TB20 & 21 including many pictures from SX-ATK

A very good book on the Socata TB including many pictures from SX-ATK

A nice mid 80's retro video on the Socata TB series (Report on TB series from beginning until 17:20)

A presentation (in Greek language) with videos of two complete IFR and VFR flights in SX-ATK

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