FMA IA 63 Pampa

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IA 63 Pampa
Type Basic trainer
Light attack
Manufacturer Fabrica Militar de Aviones
Lockheed Martin
Maiden flight 6 October 1984
Status Operational
Primary user Argentine Air Force
Number built 20

The FMA IA 63 Pampa is an advanced trainer aircraft with combat capability, produced in Argentina by FMA with assistance from Dornier of Germany.

Contents

[edit] Design and development

Although influenced by the Dassault-Breguet/Dornier Alpha Jet design, the Pampa differs in being a smaller aircraft, it is also single-engined and has straight instead of swept wings. Also the avionics systems are simpler than the Franco-German aircraft, which has an important combat second role.

The Pampa prototype first flew on 6 October 1984.

[edit] Variants

[edit] IA 63

Production of the initial series has been delayed and hampered by the state of the Argentinian economy, and as a result only 20 production aircraft have been built for the Argentine Air Force. They are in service with the IV Air Brigade at Mendoza in the advanced training role of Argentine pilots.

[edit] Vought Pampa 2000

In the 1990s, LTV/Vought selected the IA63 as the basis for the Pampa 2000, which Vought entered into the Joint Primary Aircraft Training System. It lost to the Beechcraft/Raytheon entry which became the T-6 Texan II.

[edit] AT-63 Pampa

With the acquisition of FMA by Lockheed-Martin the Pampa went from a MLU (mid life upgrade) with new engine, a more advanced avionics compatible with the A-4AR and weapon system. This new project is called AT-63 Pampa (for attack-trainer) and is commercialized by Lockheed-Martin itself. By now the only client is the Argentinian Air Force who is in the process of modernize its entire fleet and buying six new built units. The AT-63 was also offered to Colombia, Greece and Venezuela.

[edit] Operators

Image:Flag of Argentina.svg Argentina

[edit] Specifications (IA 63)

General characteristics

  • Crew: two
  • Length: 35 ft 10.25 in (10.93 m)
  • Wingspan: 31 ft 9.25 in (9.68 m)
  • Height: 14 ft 1 in (4.29 m)
  • Wing area: 168.2 ft² (15.63 m²)
  • Empty weight: 6,219 lb (2,821 kg)
  • Loaded weight: 8,378 lb (3,800 kg)
  • Max takeoff weight: 11,023 lb (5,000 kg)
  • Powerplant: 1× Garrett TFE731-2-2N turbofan, 3,500 lbf (15.6 kN)

Performance

Armament

  • 2 × 30mm cannon
  • 4 underwing hardpoints, max load 2,557 lb (1,160 kg)

[edit] External links

[edit] Related content

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