The A-4L Skyhawk, operated by Fleet Composite Squadron 13 (VC-13), was a modified variant of the Douglas A-4 series tailored to extend the operational life of early Skyhawks through upgrades suited for training and adversary roles. Derived from the A-4C airframe, the A-4L incorporated select avionics enhancements to meet evolving Navy requirements during the late 1960s and 1970s.
Compact, agile, and carrier-capable, the A-4L remained a reliable platform well-suited for its new role simulating enemy aircraft in dissimilar air combat training. It was powered by the Pratt & Whitney J52-P-6A turbojet engine, offering solid thrust performance and enabling a top speed of approximately 670 mph (1,079 km/h). Its payload capacity of 9,900 lbs (4,490 kg) across five hardpoints allowed it to carry a versatile mix of ordnance for both training and light attack missions.
Key features of the A-4L included:
Upgraded avionics package for improved navigation and communication (borrowed from A-4F systems).
Retention of the lightweight, maneuverable A-4C airframe for excellent handling.
Enhanced cockpit instrumentation to support pilot training and transition.
VC-13, known as the "Saints", utilized the A-4L extensively in the adversary role, preparing U.S. Navy pilots for real-world combat through simulated dogfights and threat replication. The A-4L’s small profile, agility, and reliability made it ideal for these missions, and it became a staple of aggressor training squadrons during the Cold War era.
Controls:
AG7: Extend tail hook
AG8: Light
VTOL: Flaps
Trim: Elevator Trim
Credits: @Inuyasha8215
Specifications
General Characteristics
- Predecessor A-4F Skyhawk VA-164
- Created On Android
- Wingspan 17.2ft (5.2m)
- Length 26.5ft (8.1m)
- Height 11.9ft (3.6m)
- Empty Weight N/A
- Loaded Weight 5,284lbs (2,396kg)
Performance
- Power/Weight Ratio 1.76
- Wing Loading 17.7lbs/ft2 (86.2kg/m2)
- Wing Area 299.4ft2 (27.8m2)
- Drag Points 1441
Parts
- Number of Parts 251
- Control Surfaces 9
- Performance Cost 1,170