The Westland PV.7 was a private venture entry to Air Ministry specification G.4/31, which called for a multi role replacement for the Westland Wapiti able to do level bombing, army co-operation, dive bombing, reconnaissance, casualty evacuation and torpedo bombing. It was a large, tall, single engined high wing monoplane with two crew in separate cockpits, an all metal wing with Handley Page slats and split flaps that doubled as dive brakes, and a tall split axle undercarriage able to carry a torpedo. It was powered by a Bristol Pegasus radial and first flew on 30 October 1933 with Harald Penrose at the controls. After promising early trials at Martlesham Heath, it was lost on 25 August 1934 when its port wing collapsed in a high speed dive during a centre of gravity test; Penrose escaped by parachute through a side window, and Westland could not afford a replacement.
Facts
Engine Class Comparison
Body StyleAircraft (no road body style) 1 Connections
Of Make
Source Westland PV.7 (Wikipedia)
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Manufactured By
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Source Westland PV.7 (Wikipedia)Design and development, manufacturerQuote, Design and development, manufacturer
others, like Westland, built aircraft as private ventures
Originated In
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Source Westland PV.7 (Wikipedia)Lead, country of originQuote, Lead, country of origin
The Westland PV.7 was a private venture submission to a 1930s British specification for a general-purpose military aircraft with two crew.
Sources
1. Westland PV.7 (Wikipedia)
Design and development
It flew for the first time on 30 October 1933
Lead
a 1930s British specification for a general-purpose military aircraft with two crew
Design and development, engine class
chose the nine-cylinder Bristol Pegasus radial
Lead, status
but was destroyed early in official tests
Design and development, manufacturer
others, like Westland, built aircraft as private ventures
Lead, country of origin
The Westland PV.7 was a private venture submission to a 1930s British specification for a general-purpose military aircraft with two crew.
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