Westland Wallace Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
31 October 1931 |
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PV.6: |
1 - Westland (converted from Wapiti) |
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Wallace I: |
66 - Westland (58 converted from Wapiti) |
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Wallace II: |
107 - Westland |
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Type Specification | |
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Applies to: |
Westland Wallace II |
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Type: |
General purpose aircraft |
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Wing: |
Two bay, staggered, unswept, equal span biplane. Metal structure, fabric covered. Ailerons on all for wings |
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Fuselage: |
Fuselage mounted on lower wing. Metal structure with fabric covering |
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Tail Unit: |
Braced fin and tailplane with unbalanced elevator and balanced fin |
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Landing Gear: |
Divided type fixed main gear with tail wheel |
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Power Plant: |
One 665 hp Bristol Pegasus IV in nose |
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Accommodation: |
Pilot and gunner in enclosed cockpits aft of wing |
Armament: |
One fixed Vickers forward and one Lewis aft. Bomb load of 580 lb |
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Dimensions | |
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Span: |
46 ft 5 in |
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Length: |
34 ft 2 in |
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Height: |
11 ft 6 in |
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Wing Area: |
488 sq ft |
Weights | |
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Empty: |
3,680 lb |
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Loaded: |
5,750 lb |
Performance | |
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Max Speed: |
158 mph |
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Initial Climb: |
1,350 ft/min |
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Service Ceiling: |
24,100 ft |
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Range: |
470 miles |
Preserved in British Museums | |
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Wallace II: |
K6035 - Royal Air Force Museum, Hendon - Fuselage |
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Wallace Replica: |
Unmarked - Suttleworth Collection, Old Warden - Fuselage frame |
Web Sites | |