General Characteristics
- Crew: 4
- Capacity: 50 troops
- Length: 93 ft 10 in (28.6 m)
- Wingspan: 117 ft 6 in (35.8 m)
- Height: 27 ft 6 in (8.38 m)
- Wing area: 1,460 ft² (136 m²)
- Empty weight: 38,930 lb (17,660 kg)
- Loaded weight: 62,000 lb (28,000 kg)
- Max takeoff weight: 73,000 lb (33,000 kg)
- Powerplant: 4× Pratt & Whitney R-2000-9 radial engines, 1,450 hp (1,080 kW) each
Performance
- Maximum speed: 275 mph (239 knots, 442 km/h)
- Cruise speed: 190 mph (165 knots, 310 km/h)
- Range: 4,000 mi (6,400 km)
- Service ceiling: 22,300 ft (6,800 m)
- Wing loading: 42.5 lb/ft² (207 kg/m²)
- Power/mass: 0.094 hp/lb (160 W/kg)
Variants
- C-54 - First production variant adapted from DC-4
- C-54A - First military version. Navy designation R5D-1.
- C-54B - Increased fuel capacity in the wing. One was used by Winston Churchill.
- VC-54C - VIP transport version used by Franklin D. Roosevelt.
- C-54D - Same as C-54B but with different version of the R2000 engine. Most common version.
- AC-54D - Small number of aircraft modified with special electronic calibration and communications equipment. The aircraft were redesignated EC-54D.
- JC-54 - Nine C-54Ds converted for missile nose-cone recovery.
- SC-54D - 38 aircraft converted by Convair, as search and rescue aircraft. Later redesignated HC-54D.
- TC-54D - C-54Ds converted into multi-engine training aircraft.
- VC-54D - C-54Ds converted into VIP transport aircraft.
- C-54E - Further revision to fuel tanks and provision for rapid conversion from passenger to cargo.
- XC-54F - One experimental paratroop version built.
- C-54G - Same as C-54E but with different version of the R2000 engine.
- VC-54G - C-54Gs converted into VIP/staff transport aircraft.
- C-54GM - The designation of the DC-4 version made by Canadair.
- C-54H - Paratroop transport. None built.
- C-54J - Staff transport project, none built. Navy designation R5D-6.
- XC-54K - One aircraft built with Wright R-1820 engines.
- C-54L - One aircraft built with an experimental fuel system.
- C-54M - Specialized modification of C-54E to carry coal during the Berlin Airlift.
- MC-54M - Specialized modification of C-54E for medical evacuation.
- EC-54U - US Navy version, modified with electronic countermeasures equipment. Used for training and evaluation.
- R5D-1 - The designation of 56 C-54As transferred to the US Navy.
- R5D-1C - Modified in US Navy service, with a fuel system based on the one used in the C-54B.
- R5D-1F - Naval staff transport version of the R5D-1. Later redesignated VC-54N.
- R5D-1Z - Interim designation of the R5D-1F.
- C-54P' - Naval variant of the C-54B. Navy designation R5D-2.
- VC-54P - Naval staff transport version, Navy designation R5D-2F.
- R5D-2Z - Interim designation of the R5D-1F.
- C-54Q - Naval variant of the C-54D. Navy designation R5D-3.
- RC-54V - Naval Photographic reconnaissance version.
- VC-54Q - Naval Staff transport version.
- R5D-3Z - Interim designation of the VC-54Q.
- R5D-4 - The designation of 20 C-54Es transferred to the US navy.
- C-54R - Naval variant of the C-54E. Navy designation R5D-4R.
- C-54S - Naval variant of the C-54G. Navy designation R5D-5.
- VC-54S - Naval staff transport version. Navy designation R5D-5Z.
- VC-54T - Naval Personnel transport version. Navy designation R5D-5R.
- R5D-6 - Unbuilt project.
- XC-112 - Pressurized variant with Pratt & Whitney R-2800 engines. None built.
- XC-112A - As XC-112. One built. Developed into DC-6 / C-118 family.
- XC-114 - Stretched C-54E powered by Allison V-1710 engines. One built.
- XC-115 - XC-114 with Packard V-1650 engines. None Built.
- XC-116 - XC-114 with thermal de-icing rather than rubber boots. None built.
- Skymaster Mk I - RAF designation of one C-54B and 22 C-54Ds.
