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Douglas A-4 Skyhawk

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Also known as McDonnell Douglas A-4, Douglas A4D, Attack Design 4, A4D Skyhawk, McDonnell Douglas A-4 Skyhawk, A4, Douglas A4D Skyhawk, Skyhawk

1954 attack aircraft family by the Douglas Aircraft Company

Key facts

Type
Attack aircraft , fighter , aggressor aircraft
National origin
United States
Manufacturer
Douglas Aircraft Company , McDonnell Douglas
Status
In service with the Brazilian Navy
Primary users
United States Navy (historical) United States Marine Corps (historical) , Israeli Air Force (historical)
Number built
2,960
Manufactured
1954–1979
Introduction date
1 October 1956 ; 69 years ago ( 1956-10-01 )
First flight
22 June 1954 ; 71 years ago ( 1954-06-22 )
Retired
USMC (1998), U.S. Navy (2003), Israeli Air Force (2015) , Royal New Zealand Air Force (2001)
Variants
Lockheed Martin A-4AR Fightinghawk , McDonnell Douglas A-4G Skyhawk , ST Aerospace A-4SU Super Skyhawk

via Wikipedia infobox

Wikidata facts

Subclass of
attack aircraft
Country of origin
United States
Developer
Douglas
Manufacturer
McDonnell Douglas
Designed by
Ed Heinemann
Image
Last bulit A-4 Skyhawk in flight in February 1979.jpg
Height
5
Length
12.27
Show 16 more facts
armament
Zuni
United States Navy aircraft designation
A4D
topic's main category
Category:Douglas A-4 Skyhawk
Commons category
Douglas A-4 Skyhawk
Commons gallery
A-4 Skyhawk
total produced
2960
first flight
1954-06-22
service retirement
1998-00-00
wingspan
8.38
maximum operating altitude
14000
military designation
A-4
vehicle range
3220
nickname
Skyhawk
service entry
1956-10-00
wing area
20.6
Sources (8)

via Wikidata · CC0

~40 min read

Encyclopedic overview

The Douglas A-4 Skyhawk is a single-seat, subsonic, carrier-capable, light attack aircraft designed and produced by American aerospace manufacturer Douglas Aircraft Company, later built by McDonnell Douglas. It was originally designated A4D under the United States Navy's pre-1962 designation system.

The Skyhawk was developed during the early 1950s on behalf of the Navy and United States Marine Corps as a replacement for the propeller-driven Douglas A-1 (AD) Skyraider. The A-4 is a compact, straightforward, and lightweight aircraft for the era; its maximum takeoff weight of 24,500 pounds (11,100 kg) was roughly half of the Navy's weight specification. The Skyhawk has a short-span, delta wing configuration and tricycle undercarriage, and is powered by a single turbojet engine. The U.S. Navy issued a contract for the aircraft on 12 June 1952. On 22 June 1954, the XA4D-1 prototype performed its maiden flight; it went on to set a world speed record of 695.163 mph on 15 October 1955. On 1 October 1956, the Skyhawk was introduced to operational service.

Excerpted from Wikipedia’s “Douglas A-4 Skyhawk” article, available under the CC BY-SA 4.0 licence.