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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

In the Vinony graph

Within Vinony's link graph, Douglas A-4 Skyhawk is referenced by 1,204 other articles, and connects out to United States Navy Strike Fighter Tactics Instructor program, United States Navy and General Dynamics F-16 Fighting Falcon.

Vinony files it under 1950s United States attack aircraft, Aircraft first flown in 1954 and Aircraft with retractable tricycle landing gear.

Its subject is documented across 37 Wikipedia language editions.

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.

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