Specifications |
---|
Country of Origin | USA.
|
Similar Aircraft | G.222, C-160 Transall, Aviocar C-212.
|
Crew | Four.
|
Role | STOL transport, cargo (60 equipped troops).
|
Armament | Usually none.
|
Length | 76 ft, 3 in (23.93 m)
|
Span | 110 ft (33.53 m).
|
Wings | High-mounted and unequally tapered with blunt tips.
|
Engine(s) | Pratt & Whitney R-2800-99W, 18 cylinder Double Wasp piston engines. Later variant included two J-85-17 general Electric turbojet engines producing 2,850 lbs of thrust.
|
Wing Area | 1223 Sq Ft
|
Gross Weight | 60,000 lbs
|
Empty Weight | 29,900 lbs
|
Cargo | 15,000 lbs or 61 troops or 50 litter with six sitting wounded and six attendants
|
Cruise Speed | 170.00 mph
|
Max Speed | 245.00 mph
|
Service Ceiling | 29,000 Ft
|
Range | 1,470 mi
|
Crew | Two pilots
|
|
|
Fuselage | Wide, cigar-shaped. Upswept rear section and solid, rounded nose. Stepped cockpit.
|
Tail | Back-tapered fin with square tip and a large, angular fairing. Flats are high-mounted on the body and unequally tapered with square tips.
|
USER COUNTRIES |
Canada, Egypt, El Salvador, Honduras, South Korea, Taiwan, Thailand, USA, Venezuela.
|