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History Brief, by Johan Visschedijk

October 15, 2003

Shavrov Sh-7


The Sh-7 was intended for operation by Aeroflot and Glavsevmorput and design started late 1938. Water trials started in the spring of 1940 and on June 16 the amphibian made its maiden flight with Ye.O. Feydorenko at the controls. Factory trials ended in September, after that it was tested by the SNII (aeroplane scientific test institute) and declared ready for series production in December 1940. WW II prevented this, but the sole prototype, registered CCCP-359, was used intensively during war in the south-east of Russia, flying urgent goods along the southern leg of the Volga.

The aircraft had a hull of metal as was the construction of the flying surfaces, the latter being fabric covered. The main landing gear was manually operated and folded upwards until wheels where flush in side of hull. The aircraft seated six persons of which two in the cockpit, cargo could also be loaded through a roof hatch just aft of the wing.

Sh-7 Jacques Trempe Collection

Specifications

Type:

Light amphibious transport aircraft

Engine:

Kossov developed MG-31F nine-cylinder of 330 hp

Span:

42 ft 7.75 in (13 m)

Length:

30 ft 10 in (9.4 m)

Height:

11 ft 5 in (3.48 m)

Wing area:

251 sq.ft (23.3 sq.m)

Empty Wt:

2,712 lb (1,230 kg)

Max T/O Wt:

4,189 lb (1,900 kg)

Max speed:

135.5 mph (218 km/h) at sea level

Max climb:

656 ft (200 m)/min

Ceiling:

9,700 ft (2,960 m)

Range:

572 mls (920 km)

Models

Sh-7:

prototype only