Engineering:SPAD S.XIV
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Short description: French WW1 fighter aircraft
| XIV | |
|---|---|
| |
| Role | seaplane fighter |
| National origin | France |
| Manufacturer | SPAD |
| First flight | 15 November 1917[1] |
| Introduction | 1918 |
| Number built | 40[2] |
| Developed from | SPAD XII |
The SPAD XIV was a French biplane floatplane fighter aircraft built by Société Pour L'Aviation et ses Dérivés (SPAD) and flown by the French Navy during World War I.
Development and design
The SPAD XIV was a development of the SPAD XII. It was single-seat biplane powered by a 149 kW (200 hp) Hispano-Suiza 8Bc engine. 40 were constructed and flew in the French Navy during 1918.[2]
Operators
France
- Aeronavale
Specifications
Data from aviafrance.com[1]
General characteristics
- Crew: 1
- Length: 7.40 m (24 ft 3 in)
- Wingspan: 9.80 m (32 ft 1.75 in)
- Height: 4.00 m (13 ft 5.5 in)
- Wing area: 26.20 m2 (282.0 sq ft)
- Empty weight: 770 kg (1,697 lb)
- Gross weight: 1,060 kg (2,336 lb)
- Powerplant: 1 × Hispano-Suiza 8BeC , 149 kW (220 hp)
Performance
- Maximum speed: 205 km/h (127.3 mph, 110.6 kn)
- Range: 249.4 km (155 mi, 135 nmi)
- Service ceiling: 4,998.7 m (16,400 ft)
Armament
- 1 x 7.70 mm (0.303 in) synchronised Vickers machine gun
- 1 x 37 mm (1.46 in) S.A.M.C. cannon
References
- Taylor, John W. R., and Jean Alexander. "Combat Aircraft of the World" New York: G.P. Putnam's Sons, 1969 Library of Congress Catalog Card Number 68-25459 (Pg.128-129
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