The A-4H Skyhawk, operated by the Israeli Air Force (IAF), was a customized variant of the Douglas A-4 series, extensively modified to meet Israel’s unique operational requirements. Renowned for its rugged design, agility, and low operating cost, the A-4H played a crucial role in ground-attack and close air support missions from the late 1960s through the 1980s.
Powered by the Pratt & Whitney J52-P-8A turbojet engine, the A-4H reached a top speed of 675 mph (1,086 km/h) and could carry up to 9,900 lbs (4,490 kg) of ordnance across five external hardpoints. The aircraft was equipped with two internal 30mm DEFA cannons, replacing the original 20mm Mk 12s, providing superior firepower in strafing and close engagements.
Key upgrades and features of the A-4H included:
Enhanced weapons systems, with compatibility for Israeli and NATO-standard munitions.
Installation of Israeli-made avionics and ECM (Electronic Countermeasure) suites.
Reinforced airframe and landing gear for high-tempo operations from forward airstrips.
Tail pipe extension to reduce vulnerability to heat-seeking missiles.
The A-4H saw extensive combat service during the War of Attrition and the Yom Kippur War, where it became a backbone of IAF tactical strike operations. Its robust performance and adaptability earned it a strong legacy within the Israeli military aviation community.
Controls:
AG1: Jettison fuel tank
AG2: Jettison bomb
AG6: Extend parachute
AG7: Extend tail hook
AG8: Light
VTOL: Flaps
Trim: Elevator Trim
Specifications
General Characteristics
- Predecessor A-4F Skyhawk VA-164
- Created On Android
- Wingspan 17.2ft (5.2m)
- Length 26.8ft (8.2m)
- Height 11.6ft (3.5m)
- Empty Weight N/A
- Loaded Weight 7,706lbs (3,495kg)
Performance
- Power/Weight Ratio 1.207
- Wing Loading 25.1lbs/ft2 (122.4kg/m2)
- Wing Area 307.4ft2 (28.6m2)
- Drag Points 1169
Parts
- Number of Parts 290
- Control Surfaces 9
- Performance Cost 1,388