Length
112.9 ft
(34.40 m)
Width/Span
131.2 ft
(40.00 m)
Empty Wgt
77,713 lb
(35,250 kg)
MTOW
154,985 lb
(70,300 kg)
Wgt Diff
+77,272 lb
(+35,050 kg)
(Showcased structural values pertain to the Lockheed L-100-30 Hercules production variant)
Installed:
4 x Allison 501-D22A turboprop engines developing 4,510 horsepower each.
Max Speed
354 mph
(570 kph | 308 kts)
Ceiling
22,966 ft
(7,000 m | 4 mi)
Range
5,592 mi
(9,000 km | 16,668 nm)
Rate-of-Climb
1,830 ft/min
(558 m/min)
♦ 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.