The SOCATA TBM700 is a single engine turboprop, six to seven seat low-wing light business and utility monoplane manufactured by EADS SOCATA. The TBM700 was offered until 2006, when the TBM850 was introduced.
Initial production version with one Pratt & Whitney Canada PT6A-64 turboprop engine.
Variant with wide entrance door, increased maximum zero fuel weight and other improvements.
Improved version with rear unpressurised cargo compartment, reinforced structure, new air conditioning system and other improvements.
C1 with increased maximum take off weight.
Variant with increased maximum cruise/climb power, one Pratt & Whitney Canada PT6A-66D turboprop engine, produced as the TBM850
|Manufacturer/Designer:||EADS SOCATA (Aérospatiale).|
|Task:||Liaisons and Utility roles.|
|First Flight:||July 14, 1988.|
|First Delivery:||May 1992.|
|Wing Span:||12,56 m.|
|Wing Area:||18,00 m².|
|Engine (s):||One Pratt & Whitney Canada PT-6A-64 turboprop rated at 522 kW.|
|Weight:||– Empty: 1.826 Kg.
– Internal fuel: 866 Kg.
– Max payload: 647 Kg.
|Max. Take off weight:||Max. take off: 2.991 Kg.|
|Max. Landing weight:||Max. landing: 2.835 Kg.|
|Cruise Speed:||555 km/h.|
|Operating altitude:||7.925 m, max. 9.150 m.|
|Max. Range:||2.985 km.|
|Radar:||Bendix/King RDR 2000 with digital and vertical