Developed 1940-41. Entered Service 1942. Phased out beginning 1960.
RAF Camel
General characteristics
· Crew: 1 or 2 pilots
· Capacity: up to 23 troops or freight
· Length: 51 ft 10 in (15.80 m)
· Wingspan: 80 ft 5 in (24.50 m)
· Height: 15 ft 1 in (4.60 m)
· Wing area: 693 ft² (64.4 m²)
· Empty weight: 11,517 lb (5,225 kg)
· Max takeoff weight: 17,196 lb (7,800 kg)
· Powerplant: 2 × Austral14N, 700 kW (950 hp) each
· * Aspect ratio: 16:1
Performance
· Maximum speed: 157 kn, 180 mph (290 km/h)
· Cruise speed: 145 kn, 168 mph at 12,795 ft (270 km/h at 3,900 m)
· Range: 400 nmi, 460 mi (740 km)
· Service ceiling: 25,100 ft (7,650 m)
Armament
· 4 × .303 MG
Sphinx Seaplane Transport/Scout Bomber - ICAAC, FAA
Developed 1935-36. Entered service 1938. Phased out beginning 1973.
General characteristics
· Crew: 3+
· Length: 22 m (72 ft 2 in)
· Wingspan: 27 m (88 ft 6 in)
· Height: 5.9 m (19 ft 3 in)
· Wing area: 108 m² (1,162 ft²)
· Empty weight: 13,470 kg (29,700 lb)
· Loaded weight: 18,400 kg (40,565 lb)
· Powerplant: 3× Brahma 9-cylinder radial engines, 746 kW (1,000 hp) each
Performance
· Maximum speed: 341 km/h (212 mph)
· Combat radius: 2,900 km (1,802 mi)
· Service ceiling: 5,900 m (19,357 ft)
Armament
· 1 × 20 mm
· 2 × .303 MG
· 12 × 50 kg (110 lb) bombs