United States
(OPERATORS list includes past, present, and future operators when applicable)
Length
131.2 ft
(40.00 m)
Width/Span
174.1 ft
(53.06 m)
Empty Wgt
101,413 lb
(46,000 kg)
MTOW
194,007 lb
(88,000 kg)
Wgt Diff
+92,594 lb
(+42,000 kg)
(Showcased structural values pertain to the base Douglas C-124 Globemaster II production variant)
Installed:
4 x Pratt & Whitney R-4360 Wasp Major radial engines delivering 3,800hp each.
Max Speed
323 mph
(520 kph | 281 kts)
Ceiling
32,808 ft
(10,000 m | 6 mi)
Range
2,175 mi
(3,500 km | 6,482 nm)
♦ MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.