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FFV-Aerotech BA.14 Starling

ffvba14starling

Construction of the BA-14 Starling recreational trainer (SE-KFV, first flight 25August 1988), designed by Bjorn Andreasson, began 1987. It became a joint venture project between MFI and FFV Aerotech, but later redesigned by MFI to FAR Pt 23A. Development delayed by other work, but resumption of flight testing apparently still awaited.

Engine : Lycoming O 235, 85 hp
Length : 21.654 ft / 6.6 m
Height : 8.858 ft / 2.7 m
Wingspan : 37.402 ft / 11.4 m
Wing area : 122.71 sq.ft / 11.4 sq.m
Max take off weight : 1797.1 lb / 815.0 kg
Weight empty : 1058.4 lb / 480.0 kg
Max. weight carried : 716.6 lb / 325.0 kg
Max. speed : 124 kt / 230 km/h
Landing speed : 40 kt / 75 km/h
Cruising speed : 103 kt / 190 km/h
Initial climb rate : 590.55 ft/min / 3.0 m/s
Service ceiling : 11155 ft / 3400 m
Wing load : 14.56 lb/sq.ft / 71.0 kg/sq.m
Range : 346 nm / 640 km
Crew : 2
 


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