Shavrov Sh-5
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Shavrov Sh-5

The Sh-5 was developed for the purpose of aerial mapping. The first prototype flew on 19 March 1934. Project was cancelled by the end of the year with only one prototype built.

Shavrov Sh-5A three-view drawing (800 x 540)

 ENGINE2 x M-22, 480hp
    Take-off weight5000 kg11023 lb
    Empty weight3470 kg7650 lb
    Wingspan24.0 m79 ft 9 in
    Length15.0 m49 ft 3 in
    Height6.2 m20 ft 4 in
    Wing area73.2 m2787.92 sq ft
    Max. speed213 km/h132 mph
    Ceiling4900 m16100 ft
    Range800 km497 miles

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