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FLS Sprint


Designed by Sydney Holloway, the Sprint aerobatic primary trainer was built by Trago-Mills Ltd. as the Trago-Mills SAH-1. FLS Aerospace took over the design in 1991 and built a further three examples.

FLS Sprint G-SAHI

G-SAHI               c/n 01               United Kingdom

2 seat light aircraft first flown in 1983

Engine: 118hp(88kW) Lycoming O-235-L2A                                                                                  Length: 21’10.5"(6.66m)                                                                                     Height: 7’7.5"(2.32m)Wingspan: 30’8.5"(9.36m)                                                                                                 No.built: 4 Range: 700miles(1126km)                                                              Cruising speed: 107mph(172kmh) Empty weight: 1100lb(499kg)                                                 Maximum take-off weight: 1650lb(749kg)

 

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