McDonnell-Douglas A-4 Skyhawk
Nickname: Heinemann's Hot Rod; Scooter. |
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The Douglas A-4 Skyhawk was designed by Edward Henry Heinemann as a single-seat carrier-borne attack bomber. The prototype Skyhawk, XA4D-1, flew for the first time on 22 June 1954, only eighteen months after design
work was initiated and features a simplified airframe and reduced equipment as compared to other deck-landing combat aircraft. No wing folding mechanism is used as the Skyhawk is sufficiently small without wings folded to ascend and descend on the elevators of U S Navy aircraft carriers. The Skyhawk entered service in October 1956 and provided the US Navy and the USMC with their principal light attack platform for over 20 years. Total production of all variants reached 2,960.
Early models comprised the
Wright J65-W2 powered A-4A/B/Cs (differing in avionics and engine power), the Pratt & Whitney J52-P engined A-4Es and A-4Fs with a dorsal avionics hump. Export models comprised
A-4G (Australia), A-4H (Israel), A-4K (New Zealand), A-4KU (Kuwait) and A-4P & 4Q (Argentina). The A-4L was a re-built A-4C for the USN Reserve. A-4Ns were similar to the
A-4H but featured uprated avionics, including a HUD. The last major production model was
the A-4M, based on the A-4F but introducing a Pratt & Whitney J52-P-408 engine.
A-4 trainer variants feature two cockpits in
tandem with a single canopy, and some combat capability. The USMC's OA-4M was used for FAC
duties, and has been retired. The definitive TA-4J was a simplified version which lacks
cannon armament and combat capability. In USN service this is the major operational model,
used for advanced training, including carrier qualification.
Singapore has the most capable
Skyhawks, having upgraded surplus A-4B/Cs as A-4Ss. Three modification standards exist:
the basic refurbished aircraft, the A-4S-1 Super Skyhawk,
re-engined with the GE-F404 turbofan, and the A-4SU with F404 and a new digital
avionics suite which include a Pave Penny laser designator, pilot's HUD and an inertial
navigation system (INS).
A- 4S-1 Super Skyhawk Specifications |
Length (including IFR probe): |
12.72 m |
Height: |
4.57 m |
Wingspan: |
8.38 m |
Wing
area: |
24.4 sq.m |
Performance |
Weight
(operating empty): |
4,649 kg |
Maximum
take off weight: |
10,206 kg |
Maximum
speed: |
1,128 km
/h |
Maximum
rate of climb: |
3,326 m
per minute |
Service
ceiling: |
12,190m |
Range
with maximum ordnance: |
625 nm
(1,158 km) |
Propulsion |
One General
Electric F404-GE-100D
non-afterburning turbofan rated at 48.04 kN |
Armament |
Two Mk 12
20-mm cannon in wingroots;
plus ordnance including :
- bombs,
- rockets,
- ASMs,
AIM-9P AAMs and
fuel tanks.
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McDonnell Douglas Skyhawk Variants |
XA4D-1 |
Prototype, first flown on 22
June 1954.
Test pilot was Robert O. Rahn. |
A-4A (A4D -1) |
First production Skyhawk. |
A-4B (A4D -2) |
First flown on 26 March
1956. |
A-4C (A4D-2N) |
First flown on 21 August
1959. |
A-4D |
Designation was skipped to
avoid confusion with the earlier A4D designation. |
A-4E (A4D-5) |
First flown on 21 July 1961. |
A-4F |
Has a dorsal avionics hump. |
A-4G |
Similar to E, manufactured
for the Royal Australian Navy. |
A-4H |
Similar to E, manufactured
for Israel. |
A-4K |
Similar to E, manufactured
for New Zealand. |
A-4KU |
Similar to E, manufactured
for Kuwait. |
A-4L |
Modified version of 4C,
assigned to US Naval Reserve. |
A-4M |
First A-4M prototype flew on
10 April 1970.
Specially manufactured for the Marine Corps. |
A-4N |
Has a new nav/attack system
and a revised cockpit layout including a HUD. First A-4N prototype flown on 12 June 1972.
Same powerplant and airframe as the A-4M. |
EA-4F |
Specially modified from
TA-4F for use by the USN FEWSG (Fleet Electronics Warfare Service Group). |
OA-4M |
Modified TA-4F, used by the
USMC for forward air control (FAC) duties. |
TA-4J |
The definitive trainer
variant, featuring two cockpits. |
A-4PTM |
Peculiar to Malaysia, these
were surplus USN A-4Cs and A-4Ls. |
A-4P & 4Q |
Manufactured B models for
sale to Argentina.
Ps to the Air Force and Qs to the Naval Air Arm. |
A-4S |
Surplus A-4Bs re-worked for
the Republic of Singapore Air Force. |
A-4S-1 |
Upgraded & re-engined by
Singapore Technologies Aerospace Ltd (STAL).
Also known as "Super Skyhawk". |
A-4SU |
Super Skyhawk upgraded &
re-engined by Singapore Technologies Aerospace Ltd with a new avionics suite. |
Skyhawk Operators |
Argentina |
Australia |
Indonesia |
Israel |
Kuwait |
Malaysia |
New Zealand |
Singapore |
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Click on the thumbnails below to view a larger image.
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This page was updated on Monday, 10 September 2001.