Lockheed Martin A-4AR Fightinghawk

Airplanes

Length

12.3 m

Flat Wing Span

8.38 m

Height

4.57 m

Flat Wing Area

24.15 m²

Max Speed

1080 km/h

Max Ceiling

12880 m

Number of Engines

Aircraft Engine

First Flight

1997-12-01

Entry Into service

1997-12-01

Number Built

Maximum Take-Off Weight

11.136 t (paragliders: kg)

Maximum Range

3220 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Lockheed Martin A-4AR Fightinghawk	11.136	3220

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
McDonnell Douglas A-4G Skyhawk	Pratt & Whitney J52	12.27	8.38	Compare
Douglas A-4 Skyhawk		12.192	8.2296	Compare
Rockwell XFV-12		13.1064	8.5344	Compare
Venga TG-10	General Electric J85	11.89	8.23	Compare
KAI T-50 Golden Eagle	General Electric F404	13.14	9.45	Compare
Blériot IX		12	9	Compare

All data (25 fields)

Name: Lockheed Martin A-4AR Fightinghawk
Manufacturer: McDonnell Douglas
Description: The Lockheed Martin A-4AR Fightinghawk is a major upgrade of the McDonnell Douglas A-4M Skyhawk attack aircraft developed for the Argentine Air Force which entered service in 1998.
First Flight: 1997-12-01
Entry Into service: 1997-12-01
Production End: 1999-01-01
Service End: 2026-05-15
Designer: McDonnell Douglas
Type: Ground attack fighter
Length (m): 12.3
Height (m): 4.57
Cockpit Crew: 1
Max Speed (km/h): 1080
Max Ceiling (m): 12880
Rate of Climb (m/s): 43
Armament: 2× 20 mm (0.787 in) Colt Mk 12 cannon, 100 rounds/gun; 9,900 lb (4,490 kg) on five external hardpoints; ; Air-to-air missiles:; 4× AIM-9 Sidewinder; Air-to-surface missiles:; 4× ARM-657 Mamboretá
Number Built: 36
Powerplant Description: 1 × Pratt & Whitney J52-P-408A turbojet, 50 kN thrust each
Primary Users: Argentine Air Force (historical)
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/Lockheed_Martin_A-4AR_Fightinghawk
Flat Wing Span (m): 8.38
Flat Wing Area (m²): 24.15
Aircraft Engine: Pratt & Whitney J52
Number of Engines: 1