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The National Aerospace Laboratories designed the
Saras as a development aircraft for a light transport requirement by the
Indian Air Force. The engines are mounted in pusher configuration. The
Saras is expected to enter production in 2008.
VT-XSD
c/n 1
India
15 seat light transport first flown in 2004
Engines: 2X 850shp(633kW) P&W PT6A-66
Length: 49’5"(15.0m)*
Height: 16’6"(5.0m)* Wingspan: 50’0"(15.18m)*
No.built: 2+ Range: 906miles(1456km)
Cruising speed: 273mph(440kmh) Empty weight: u/k
Maximum take-off weight: 13,450lb(6092kg) |
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