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.
|A three-view drawing (800 x 540)|
| ENGINE||2 x M-22, 480hp|
| Take-off weight||5000 kg||11023 lb|
| Empty weight||3470 kg||7650 lb|
| Wingspan||24.0 m||79 ft 9 in|
| Length||15.0 m||49 ft 3 in|
| Height||6.2 m||20 ft 4 in|
| Wing area||73.2 m2||787.92 sq ft|
| Max. speed||213 km/h||132 mph|
| Ceiling||4900 m||16100 ft|
| Range||800 km||497 miles|
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