Lockheed Martin - USA / Elbit Systems; Israel Aerospace Industries - Israel
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Israel
(OPERATORS list includes past, present, and future operators when applicable)
Width/Span
32.2 ft
(9.80 m)
Empty Wgt
19,842 lb
(9,000 kg)
MTOW
37,479 lb
(17,000 kg)
Wgt Diff
+17,637 lb
(+8,000 kg)
(Showcased structural values pertain to the Lockheed F-16I production variant)
Installed:
1 x Pratt & Whitney F100-PW-229 afterburning turbofan engine developing 27,000lb of thrust.
Max Speed
1,501 mph
(2,415 kph | 1,304 kts)
Ceiling
52,493 ft
(16,000 m | 10 mi)
Range
2,001 mi
(3,220 km | 5,963 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 Lockheed F-16I 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)
STANDARD, FIXED:
1 x 20mm M61A1 internal automatic cannon.
2 x Short-range, air-to-air missiles on wingtip launchers.
Approximately 17,000lb of externally-held drop/launch stores across nine total hardpoints (three under each wing, three under the fuselage). Supported weapon systems include additional short-range or medium-range air-to-air missiles, air-to-surface missiles, precision-guided bombs, conventional drop bombs, and rocket pods. Also supported are 3 x Jettisonable drop tanks.
(Not all ordnance types may be represented in the showcase above)
F-16I "Sufa" - Base Series Designation.
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.
