Empty Wgt
9,259 lb
(4,200 kg)
MTOW
14,804 lb
(6,715 kg)
Wgt Diff
+5,545 lb
(+2,515 kg)
(Showcased structural values pertain to the base IOMAX Archangel production variant)
Installed:
1 x Pratt & Whitney PT6A-67F turbo-prop engine developing 1,600 horsepower driving five-bladed propeller unit at nose.
Max Speed
242 mph
(389 kph | 210 kts)
Ceiling
25,000 ft
(7,620 m | 5 mi)
Range
1,553 mi
(2,500 km | 4,630 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
(Showcased performance specifications pertain to the base IOMAX Archangel production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)
Various munitions including air-to-surface missiles, anti-tank Hellfire missiles (Hellfire), gun pods, cannon pods, guided bombs, unguided bombs, and rocket pods spread across six underwing hardpoints (three per wing). Mission sensors and pods also supported.
(Not all ordnance types may be represented in the showcase above)
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.