United States
(OPERATORS list includes past, present, and future operators when applicable)
Width/Span
132.5 ft
(40.40 m)
Empty Wgt
76,778 lb
(34,826 kg)
MTOW
175,001 lb
(79,379 kg)
Wgt Diff
+98,223 lb
(+44,553 kg)
(Showcased structural values pertain to the Lockheed HC-130H Hercules production variant)
Installed:
4 x Allison T56-A-15 turboprop engines delivering 4,300 shaft horsepower each.
Max Speed
380 mph
(611 kph | 330 kts)
Ceiling
32,808 ft
(10,000 m | 6 mi)
Range
5,179 mi
(8,334 km | 15,435 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.