![]() |
Douglas
A-4A (A4D-1) "Skyhawk"
|
![]() |

The A-4 was originally designed to provide the US Navy and USMC with a simple, low-cost, light-weight attack and ground support aircraft. The design of the A-4 was heavily influenced by the experience gained during the Korean War. The initial requirements for the A-4 called for US Navy operation. Given this requirement, special design considerations were given to provide low-speed stability and control during take-offs and landings. The A-4 was also dimensionally configured to negotiate the standard US Navy aircraft carrier lifts without the added complexity and weight of folding wings. The A-4 was nicknamed "Heinemann's Hotrod" in honor of its designer, Ed Heinemann.
Initial production of the "Skyhawk" took place in September of 1953. The prototype XA-4A (originally designated XA4D-1) was powered by a Wright J65-W-2 turbojet rated at 7,200 lb. thrust. The first flight of the XA-4A took place on 22 June 1954.
The A-4A Skyhawk was the initial production version of the aircraft. The A-4A was fitted with a Wright J65-W-4 turbojet rated at 7,700 lb. thrust. The first flight of an A-4A Skyhawk took place on 14 August 1954. The A-4A Skyhawk entered service with the US Atlantic and Pacific Fleets on 26 October 1956. The production run for the A-4A was 166 aircraft. Uprated engines, rated at 8,500 lb. thrust, were progressively fitted to all the aircraft.
The Western Museum of Flight's A-4A was acquired from the USN China Lake Weapons Center.
| A-4A "Skyhawk" Specifications | |
|---|---|
| Manufacturer | Douglas Aircraft |
| Wing Span | 27 feet, 6 inches |
| Overall Length | 38 feet, 4 inches |
| Overall Height | 15 feet |
| Wing Area | 260 sq. feet |
| Empty Weight | 8,400 lbs. |
| Gross Weight | 14,875 lbs. |
| Maximum Weight | 20,000 lbs. |
| Speed (Maximum) | 664 mph |
| Powerplants | (1) Wright J65-W-4 turbojet rated at 7,700 lbs. thrust. Later upgraded to 8,500 lbs. thrust. |
| Armament | (2) 20-mm Mark 12 Cannon with 200 rounds each |
