This single engine, two seat, general purpose and torpedo carrying biplane was built as a private venture to Air Ministry Specification G4/31. The aircraft first flew on 28th February 1934 and although many hours of test flying were spent, no production order ensued and the specification was cancelled.
| Power Plant: | One Armstrong Siddeley Tiger VI 810 h.p. double row air cooled radial engine. | |
| Dimensions: |
Span 49 ft. 8 in. Length 42 ft. 2 in. Height 13 ft. Wing Area 654.2 sq. ft. |
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Weight:
8,750 lb. A.U.W. as Torpedo Carrier.
7,250 lb. A.U.W. as General Purpose or Day Bomber.
4,298 lb. Empty.
367 lb. Military Load (Fixed).
Performance:
Without Torpedo: Max. Speed at 6,500 ft 175 mph.
Climb to 15,000 ft. 12.5 min.
With Torpedo: Max. Speed at 6,500 ft 160 mph.
Climb to 15,000 ft. 23.0 min.
Armament:
1 Vickers gun firing forward.
1 Lewis gun on a ring in rear cockpit.
Racks for up to 1,000 lb. of bombs.
Provision for an 18" torpedo.