United States' Douglas C-54 Skymaster transport
Photos
Design
The Douglas C-54 Skymaster was based on the DC-4.1,2,3 The DC-4 was to be a civilian transport and 24 were in production at the time of the Japanese attack on Pearl Harbor.1 The United States Army Air Force took over the aircraft and designated it the C-54.1
Prototype
The C-54 first flew on February 14, 1942.1
Production
Only 34 C-54s were ordered in the first order placed.2
- Douglas C-54: 241
- Douglas C-54A: 2071
- Douglas C-54B: 2201
- Douglas C-54D: 3501
- Douglas C-54E: 751
- Douglas C-54G: 761
- Douglas XC-54K: 11
- Douglas R5D-1: 581
- Douglas R5D-2: 301
- Douglas R5D-3: 981
- Douglas R5D-4: 201
- Douglas XC-114: 11
- Douglas YC-116: 11
- Douglas DC-4: 791
- Total: >1,1002, 1,2421
- Manufacturer: Douglas Aircraft Company2
Variants
- Douglas C-54:
- Douglas C-54A / Douglas R5D-1: Had a stronger floor.1 Added a cargo door and freight hoist.1 Could be converted from passengers, troops, or freight.1
- Douglas C-54B / Douglas R5D-2: Had integral wing tanks.1 Could carry stretchers.1
- Douglas C-54C: Conversion of one C-54A for use by President Roosevelt.1
- Douglas C-54D / Douglas R5D-3: Had R-2000-11 engines.1
- Douglas C-54E / Douglas R5D-4: Had extra fuel capacity.1
- Douglas C-54G / Douglas R5D-5: Had R-2000-9 engines (1,450 HP).1
- Douglas XC-54K: Long range.1
- Douglas XC-114 / Douglas YC-116: Allison V-1710 engines.1
Usage
Britain and the United States used the C-54.1
The C-54s flew 79,6422 / ~80,000 ocean crossings and only lost three aircraft.1,2
United Kingdom
The Royal Air Force (RAF) received 23 C-54s and designated them Skymaster Mk. Is.1 Winston Churchill used one.1
Berlin Airlift
C-54s were used extensively during the Berlin Airlift.2
1960s
The last of the C-54s were withdrawn from active service.2
Specifications
| Douglas C-54 Skymaster1,3 | Douglas C-54A Skymaster1,2 | Douglas C-54B Skymaster1 | |
|---|---|---|---|
| Type | Transport1 | Transport2 | |
| Crew | 42 | ||
| Passengers | 501 | 502 | |
| Engine (Type) | 4: Pratt & Whitney R-2000-71 | 4: Pratt & Whitney R-2000-7 Twin Wasp2 | |
| OR | 4: Pratt & Whitney R-2000-11 Twin Wasp1 | ||
| Cylinders | Radial 141 | Radial 142 | |
| Cooling | Air2 | ||
| HP | 1,350 each1 | 1,290 each2 | |
| Propeller blades | 3 each1 | ||
| Capacity | |||
| Dimensions | |||
| Span | 117' 6"1,3 35.81 m1 |
117' 6"2 | |
| Length | 93' 10"1,3 28.6 m1 |
93' 10"2 | |
| Height | 27' 6"1, 27' 9"3 8.38 m1 |
27' 6"2 | |
| Wing area | |||
| Weight | |||
| Empty | 37,300 lb1 16,919 kg1 |
38,200 lb1 17,327 kg1 |
|
| Loaded | 52,000 lb3 | 62,000 lb2, 68,000 lb1 30,845 kg1 |
|
| Maximum load | 73,000 lb1 33,113 kg1 |
||
| Performance | |||
| Speed | 250 mph3 | 265 mph2 | |
| Speed @ 14,000' / 4,267 m |
275 mph1 442 kph1 |
||
| Cruising speed | 190 - 239 mph1 306 -385 kph1 |
||
| Climb | 1,010'/minute1 308 m/minute1 |
||
| Service ceiling | 22,000'2, 22,500'1 6,858 m1 |
||
| Range with maximum payload |
1,500 miles1 2,414 km1 |
||
| Maximum range | 2,540 miles3 | 3,900 miles1,2 6,276 km1 |
|
| Armament | None2 |
Sources:
- Aircraft of WWII, Stewart Wilson, 1998
- World War II Airplanes Volume 2, Enzo Angelucci, Paolo Matricardi, 1976
- Aeronautics Aircraft Spotters' Handbook, Ensign L. C. Guthman, 1943

