Credit
Carlos Menendez San Juan · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
AMX · Length
Single source13.23 m (43 ft 5 in)[source]
F-16V C/D Block 70/72 · /15.027 m
Single sourceConfiguration
| Specification | AMX International AMX | Lockheed Martin F-16V Viper |
|---|---|---|
| Type | Ground-attack aircraft[source] | Multirole fighter[source] |
| National origin | Italy / Brazil[source] | United States[source] |
| Manufacturer | AMX International[source] | Production plant of the Lockheed Martin in Greenville, South Carolina[source] |
| Status | Active service[source] |
49.3 ft/15.027 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]
Empty; F-16V C/D Block 70/72 · /9,207 kg
Single source20,300 lb/9,207 kg[source]
Ferry; AMX · Ferry range
Single source3,336 km (2,073 mi, 1,801 nmi)[source]
AMX · hi-lo-hi profile, with 900 kg (1,984 lb) of external stores
Single source889 km (552 mi, 480 nmi) hi-lo-hi profile, with 900 kg (1,984 lb) of external stores[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 · Endurance
Single source4 hours, 15 minutes[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.
In service[source] |
| Primary users | Italian Air Force (historical) Brazilian Air Force[source] | — |
|---|
| Number built | 230[source] | — |
|---|
| Manufactured | 1986–1999[source] | 2019–present (serial production)[source] |
|---|
| Introduction date | 1989[source] | — |
|---|
| First flight | 15 May 1984[source] | 2015[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] | 1 x M61A1 20 mm Vulcan Cannon[source] |
|---|
| Hardpoints | Bombs: 3,800 kg (8,378 lb) on 5 external hardpoints, including MAR-1 missiles, general-purpose and laser-guided bombs[source] | — |
|---|
| Designer | — | Lockheed Martin[source] |
|---|
| Primary user | — | See users[source] |
|---|
| In service | — | 2021–present[source] |
|---|
| Developed from | — | F-16 Fighting Falcon[source] |
|---|
| Maximum TOGW | — | 48,000 lb/21,772 kg[source] |
|---|
| Optional Conformal Fuel Tanks (Right/Left) | — | 220 Gallon[source] |
|---|
| Powerplant | — | 1 x GE F110-GE-129 engine for Block 70 aircraft (PW F100-PW-229 engine for Block 72 aircraft)[source] |
|---|
| Engine Thrust Class | — | 29,000 lb/13,000 kg[source] |
|---|