Robertson Skylark SRX-1 | |
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Role | STOL aircraft |
National origin | United States of America |
Manufacturer | Robertson Development Corp |
Designer | James L. Robertson |
First flight | 1955 |
The Robertson Skylark SRX-1 is a five place high performance STOL aircraft designed in the 1950s. It was intended to operated out of 120 ft (37 m) landing strips with 150 mph (241 km/h) cruise speeds.[1]
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The aircraft was designed by James L. Robertson, son of William B. Robertson, Robertson Aircraft Corporation founder at the age of 27. The aircraft is limited to be stall-proof and spin-proof. It is capable of a 25 mph (40 km/h) minimum flight speed. It was also the first light aircraft in America to be designed to accommodate a turboprop engine.[2]
The Skylark is all metal, with a steel tube internal structure. It incorporates shrouds, Robertson flaps, spoilerons, turbulator control, stabilators, elevances, and spinner duct cooling.[3]
Test flights were performed by aerobatic pilot Marion Cole. He featured the aircraft as part of his Cole Brothers airshows. The aircraft is able to take off in 100 feet.
Data from Experimenter
General characteristics
Performance
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