Wight Converted Seaplane Aircraft
| |
Production Details | |
Design Company: |
|
First Flight: |
1916 |
Bomber: |
5 - J. Samuel White & Co Ltd |
Converted Seaplane: |
40 - J. Samuel White & Co Ltd (plus 4 converted from bomber) |
Type Specification | |
Applies to: |
Wight Converted Seaplane |
Type: |
Anti-submarine patrol aircraft |
Wing: |
Three bay biplane with unswept, unequal span, unstaggered wings. Upper wing with larger chord than lower wing. Wooden structure with fabric covering. Ailerons on upper wings |
Fuselage: |
Box section fuselage with curved upper decking mounted on lower wing |
Tail Unit: |
Braced tailplane with split elevator together with single fin and rudder |
Landing Gear: |
Twin float under fuselage with additional floats at tail and wing tips |
Power Plant: |
One 322 hp Rolls-Royce Eagle VI engine mounted in the nose driving a four bladed propeller |
Accommodation: |
Tandem open cockpits for crew aft of wing. Pilot forward, gunner behind |
Armament: |
One Lewis gun aft and provision for up to four 112 lb bombs below the wings |
Dimensions | |
Span: |
65 ft 6 in |
Length: |
44 ft 8 in |
Height: |
16 ft |
Wing Area: |
715 sq ft |
Weights | |
Empty: |
3,758 lb |
Loaded: |
5,556 lb |
Performance | |
Max Speed: |
84 mph at 2,000 ft |
Climb: |
4 min 20 sec to 2,000 ft |
Service Ceiling: |
9,600 ft |
Endurance: |
3.5 hours |
Preserved in British Museums | |
None known | |
Web Sites | |
None known |