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This was the Last C-7 Kfir variant to serve in the Israeli Air force (IAF). The C-7 was used during the war with Lebanon in the 80s after which the type was retired and sold abroad to other countries like Ecuador and south Africa. this aircraft had a slightly larger dropped nose to accommodate a new ranging radar and new avionics and had a boosted General electric J-79 Turbofan engine. Pylons centerline to wing tip Ag 1 belly tank. 2 bombs. 3 wing tanks. 4 guardians. 6 drag chute. 7 Gyroscope. vtol down for speed brakes and trim for flight trim.
Specifications
General Characteristics
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- Wingspan 32.5ft (9.9m)
- Length 54.8ft (16.7m)
- Height 17.8ft (5.4m)
- Empty Weight 14,382lbs (6,523kg)
- Loaded Weight 31,182lbs (14,143kg)
Performance
- Power/Weight Ratio 1.081
- Wing Loading 62.3lbs/ft2 (304.0kg/m2)
- Wing Area 500.8ft2 (46.5m2)
- Drag Points 6788
Parts
- Number of Parts 156
- Control Surfaces 5
- Performance Cost 652
