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At a glance
Measured figures
AMX · Length
Single source13.23 m (43 ft 5 in)[source]
Length
Single sourceConfiguration
| Specification | AMX International AMX | Fairchild AU-23 Peacemaker |
|---|---|---|
| Type | Ground-attack aircraft[source] | Armed gunship, counter-insurgency, utility transport[source] |
| National origin | Italy / Brazil[source] | United States[source] |
| Manufacturer | AMX International[source] | Fairchild Aircraft[source] |
| Status | Active service[source] |
36 ft 10 in (11.23 m)[source]
Empty; AMX · Empty weight
Single sourceGross; AMX · Gross weight
Single sourceMaximum take-off; AMX · Max takeoff weight
Single source6,700 kg (14,771 lb)[source]
10,750 kg (23,700 lb)[source]
13,000 kg (28,660 lb)[source]
Gross; Gross weight
Single source6,100 lb (2,767 kg)[source]
Maximum; AMX · at 10,975 m (36,007 ft)
Single source1,053 km/h (654 mph, 568 kn) at 10,975 m (36,007 ft)[source]
Cruise; at maximum continuous power
Single sourceCruise; combat cruise
Single sourceMaximum; at take-off power, 5,000 ft (1,524 m) altitude, 6,000 lb (2,722 kg) gross weight
Single source148 kn (170 mph, 274 km/h) at take-off power, 5,000 ft (1,524 m) altitude, 6,000 lb (2,722 kg) gross weight[source]
77 kn (88 mph, 142 km/h) at maximum continuous power, 129 kn (239 km/h) combat cruise[source]
1 × Garrett TPE-331-1-101F turboprop engine
Single source1 × Garrett TPE-331-1-101F turboprop engine, 650 hp (480 kW)[source]
AMX · 1 × Rolls-Royce Spey 807 turbofan engine thrust
Single source1 × Rolls-Royce Spey 807 turbofan engine, 49.1 kN (11,000 lbf) thrust[source]
AMX · Wing area
Single source21 m 2 (230 sq ft)[source]
AMX · Service ceiling
Single source13,000 m (43,000 ft)[source]
AMX · 10,260 ft/min
Single source52.1 m/s (10,260 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Primary users | Italian Air Force (historical) Brazilian Air Force[source] | United States Air Force Royal Thai Air Force[source] |
|---|
| Number built | 230[source] | 35[source] |
|---|
| Manufactured | 1986–1999[source] | — |
|---|
| Introduction date | 1989[source] | — |
|---|
| First flight | 15 May 1984[source] | 1971[source] |
|---|
| Retired | 2024 (Italy)[source] | — |
|---|
| Fuel capacity | 3,555 L (939 US gal; 782 imp gal) / 2,700 kg (5,952 lb) internal[source] | — |
|---|
| Wing loading | 512 kg/m 2 (105 lb/sq ft)[source] | — |
|---|
| Thrust/weight | 0.47[source] | — |
|---|
| Rockets | rocket pods[source] | — |
|---|
| Missiles | 2× AIM-9 Sidewinders or MAA-1 Piranha or A-Darter , carried on wingtip rails[source] | — |
|---|
| Bombs | 3,800 kg (8,378 lb) on 5 external hardpoints, including MAR-1 missiles, general-purpose and laser-guided bombs[source] | — |
|---|
| Guns | 1× 20 mm (0.787 in) M61A1 Vulcan 6-barreled Gatling cannon (Italian aircraft) 2× 30 mm (1.181 in) Bernardini Mk-164 cannon (Brazilian aircraft)[source] | — |
|---|
| Hardpoints | Bombs: 3,800 kg (8,378 lb) on 5 external hardpoints, including MAR-1 missiles, general-purpose and laser-guided bombs[source] | — |
|---|
| Developed from | — | Pilatus PC-6 Porter[source] |
|---|
| Capacity | — | 5 troops or 6 passengers or 1 litter patient, 3 ambulatory patients with 1 medical attendant[source] |
|---|