United States
(OPERATORS list includes past, present, and future operators when applicable)
Width/Span
84.6 ft
(25.80 m)
Empty Wgt
21,605 lb
(9,800 kg)
MTOW
36,376 lb
(16,500 kg)
Wgt Diff
+14,771 lb
(+6,700 kg)
(Showcased structural values pertain to the Airbus Military HC-144A production variant)
Installed:
2 x General Electric CT7 turboprop engines developing 1,870 shaft horsepower each driving four-bladed propeller units in puller arrangement.
Max Speed
272 mph
(437 kph | 236 kts)
Range
1,802 mi
(2,900 km | 5,371 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.