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F-16C/D Barak Externally, the Israeli F-16C differs from other F-16C`s by having an extension to the base of its vertical stabilizer, similar to the Norwegian F-16s parachute brake compartment; however, no parachutes are used on IAF F-16s. Israeli F-16s have extensive local modifications, with different avionics fits and higher gross weights, requiring changes in the landing gear and the use of new wheels. The maximum all-up weight of an Israeli F-16 is 48,000 pounds, as compared to 42,300 pounds for a USAF Block 40 F-16C. The third batch of F-16C/D`s is fitted with Elta`s EL/L-8240 ECM, replacing Lockheed Martin Defense Systems` (LMDS, formerly Loral) AN/ALQ-178 Rapport III internal ECM. F-16C`s appear to have larger navigation lights mountings on the intake. These most likely house electronics. The F-16C/D`s ordered to compensate for the cancelled Lavi Project received Israeli ECM systems (manufactured by Elisra), and flight management computers (made by Elbit).
While the F-16B is a two seat version of the F-16A used for pilot conversion, the Israeli F-16D is completely different from the F-16C. The back seat is reserved for the F-16s Weapon System Operator, just as one can find at the F-4 Phantom. Externally, this fighter differs from other F-16D`s by having a boxlike extension from the cockpit to the vertical stabilizer, referred to as a dorsal spine.
The dorsal fairing was designed, mocked up, fabricated and installed during regular routine assembly while these aircraft were on the production line in Fort Worth. At no time has IAI had anything to do with initial design, fabrication of assemblies or production installation of any dorsal assemblies. The dorsal spine is believed to accommodate Wild Weasel equipment (amongst others Elisra`s SPS-3000 self-protection jammer) which detects emissions from enemy radar sites and pinpoints their locations, and specialized weapon delivery systems, such as `smart bombs` guided using the back seat`s side stick for control. The IDFAF would confirm only that this space is filled with various electronic systems.
According to the IDFAF Magazine, this version of the F-16D is much heavier than the `standard` production F-16D`s. Its empty weight is 9,525 kg, while the standard version weighs just 7,900 kg. The maximum takeoff weight was extended to 21,770 kg - 4,760 kg more than the standard version, a fact made possible by modifications made to the landing gear. The extent of the modifications called for a different (non-official) model designation, hence the Israeli F-16D was designated IF-16D. As the F-16C`s in service by the IDFAF, the IF-16D is powered by a General Electric F110-GE-100 engine, with an enlarged air intake.
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