Aircraft record
Douglas A-4 Skyhawk
A-4 · Douglas Aircraft Company · United States
- Roles
- Attack (Primary)
- Era
- Cold War
- Status
- Retired

Reference data
Quick facts
- First flight
- 1954
- Manufacturer
- Douglas Aircraft Company
- Country
- United States
- Status
- Retired
Reference data
Historical Content
Development and History
Aircraft family
The Douglas A-4 Skyhawk was developed as a compact, lightweight carrier-based attack aircraft for the United States Navy. Its design reflected engineer Ed Heinemann's determination to reduce the increasing weight and complexity of military aircraft. [1]
Aircraft family
The prototype made its first flight on June 22, 1954. The Skyhawk became an important part of U.S. naval aviation, combining a relatively small airframe with a substantial capacity for externally carried weapons. [1]
Design and Features
Aircraft family
A defining feature of the A-4 was its compact delta-wing design. Its small wingspan eliminated the need for a folding-wing mechanism, reducing structural complexity and saving weight aboard aircraft carriers. [1]
Aircraft family
Douglas also simplified several onboard systems to keep the aircraft light. These design decisions helped make the Skyhawk a practical attack aircraft for carrier operations. [1]
Operational History
Aircraft family
The A-4 played a major role in U.S. naval aviation during the Vietnam War. Skyhawks carried out attacks against military targets in North Vietnam and provided close air support for forces operating in South Vietnam. [1]
Aircraft family
Beyond frontline combat, the Skyhawk served in training and adversary roles. The U.S. Navy's Blue Angels demonstration team operated the aircraft from 1974 to 1986. [1]
Variants and Legacy
Aircraft family
The Skyhawk family included multiple single-seat attack versions and two-seat training aircraft. The A-4E was among the variants used during the Vietnam War. [1][2]
Aircraft family
The aircraft also entered service with several foreign air forces and naval aviation organizations, extending its operational history beyond the United States. [1]
Reference data
Specifications
Representative Variant Specifications
A-4E
These specifications apply to the A-4E variant and should not be read as values for every A-4 Skyhawk version.
Dimensions
| Measurement | Value |
|---|---|
| Length | 12.23 m40 ft 1.5 in |
| Wingspan | 8.38 m27 ft 6 in |
| Height | 4.62 m15 ft 2 in |
Weight
| Measurement | Value |
|---|---|
| Empty weight | 4,469.2 kg9,853 pound |
Performance
| Measurement | Value |
|---|---|
| Maximum speed | 1,083 km/h673 mph |
| Range | 4,064 km2,525 mile |
| Ceiling | 10,302.2 m33,800 foot |
Powerplant
turbojet · A-4E
Pratt & Whitney J52-P-6A
Quantity: 1
Reference data
Variants
Recorded variants of this aircraft family. Variant entries here do not create separate public pages.
Reference data
Sources
- A-4 SkyhawkNaval History and Heritage Command / National Naval Aviation MuseumA-4E representative variant specifications · Development and History · Aircraft family · Design and Features · Aircraft family · Operational History · Aircraft family · Variants and Legacy · Aircraft family
- A-4E/F SkyhawkNational Naval Aviation MuseumVariants and Legacy · Aircraft family