Douglas A-4E Skyhawk

Explore the Douglas A-4E Skyhawk in side view and top view to compare its silhouette and proportions.

Douglas A-4E Skyhawk, side profile
Douglas A-4E Skyhawk, side profile
12.23 m
Douglas A-4E Skyhawk, top view
Douglas A-4E Skyhawk, top view
8.38 m

From Wikipedia

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.

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Summary of “Douglas A-4 Skyhawk” from Wikipedia, the free encyclopedia, used under CC BY-SA 4.0. Retrieved 2026-10-11.

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Use these drawings for anything, commercial too, under Creative Commons Attribution 4.0 International. Credit us like this:

Drawing of the Douglas A-4E Skyhawk by AirwayControl Aircraft Library (https://aircraft.intelsystems.ai/aircraft/A4/), CC BY 4.0

Specifications

Length
12.23 m
Wingspan
8.38 m
Max take-off weight
11.11 t
Max speed
1,083 km/h
Range
1,867 km
Ceiling
10,302 m
Engines
1 × Pratt & Whitney J52-P-6A turbojet engine
Power
8,500 lbf (38 kN) thrust
First flight
1954
In service
1956

From the AirwayControl spec register, curated from Wikipedia and manufacturer pages. Figures vary by variant.