Wight Converted Seaplane
| Converted Seaplane | |
|---|---|
| 300px | |
| Wight Converted Seaplane (No. 9583) | |
| Role | Biplane floatplane |
| Manufacturer | John Samuel White & Company Limited (Wight Aircraft) |
| First flight | 1916 |
| Primary user | Royal Naval Air Service |
| Number built | 37 |
The Wight Converted Seaplane was a British twin-float patrol seaplane produced by John Samuel White & Company Limited (Wight Aircraft).
Contents
Design and development
Developed from the unsuccessful Wight Bomber for use as an anti-submarine patrol aircraft, the "Converted" Seaplane was a straightforward adaptation of the landplane bomber to a seaplane. The aircraft was a three-bay biplane with unswept, unequal span, unstaggered wings. It had twin floats under the fuselage and additional floats at tail and wings tips. Initial production aircraft were powered by a 322 hp Rolls-Royce Eagle IV engine mounted in the nose driving a four-bladed propeller, with later production batches being powered by a 265 hp (198 kW) Sunbeam Maori engine owing to shortages of Eagles.[1] Fifty were ordered for the RNAS, of which only 37 were completed.[2]
Operational history
The Converted Seaplane entered service with the RNAS in 1917,[1] operating from bases at Calshot, Dover, Portland and Cherbourg.[2] On 18 August 1917, a Wight Converted Seaplane flying from Cherbourg sank the German U-boat UB-32 with a single 100 lb bomb, the first submarine to be sunk in the English Channel by direct air action.[1] Seven remained in service with the RAF at the end of the First World War.
Operators
Specifications (Seaplane - Eagle engine)
Data from The British Bomber since 1914 [1]
General characteristics
- Crew: 2
- Length: 44 ft 8½ in (13.63 m)
- Wingspan: 65 ft 6 in (19.97 m)
- Height: 16 ft (4.88 m)
- Wing area: 715 ft² (66.4 m²)
- Empty weight: 3,758 lb (1,708 kg)
- Max. takeoff weight: 5,556 lb (2,525 kg)
- Powerplant: 1 × Rolls-Royce Eagle IV V-12, 322 hp (240 kW)
Performance
- Maximum speed: 73 knots (84 mph, 135 mph)
- Service ceiling: 9,600 ft (2,900 m)
- Climb to 6,500 ft (2,000 m): 18 min 20 sec
- Endurance: 3½ hours
See also
- Related development
- Aircraft of comparable role, configuration and era
- Related lists
References
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