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General Info

FAdeA
FMA IA-63 Pampa

Role Trainer aircraft
National origin Argentina
Manufacturer FAdeA
First flight 6 October 1984
Introduction April 1988
Status In service
Primary user Argentine Air Force
Produced 1984-present
Number built 32

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History Fabrica Argentina de Aviones (FAdeA)  
FAdeA FMA IA-63 Pampa

Preliminary design studies for a replacement for the Morane-Saulnier MS-760 of the Argentine Air Force started at the Fábrica Militar de Aviones (FMA) in 1978, with these studies resulting in selection of a proposal powered by a single Garrett TFE731 turbofan with high, unswept wings. At the same time the FMA signed a partnership agreement with Dornier to develop the new aircraft.

Although influenced by the Dassault/Dornier Alpha Jet design, the Pampa differs in being a smaller aircraft, it is also single-engined and has straight supercritical wings rather than the swept ones of the Alpha Jet. It is constructed mainly of aluminium alloy, with carbon-fibre used for components such as the air intakes. The crew of two sit in tandem under a single-piece clamshell canopy. The avionics systems are also simpler than the Franco-German aircraft, which has an important secondary combat role. The Pampa prototype first flew on 6 October 1984

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Fabrica Argentina de Aviones (FAdeA)

FAdeA, a Lockheed Martin Company
FAdeA FMA IA-63 Pampa

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General Info

  • Crew: 2
  • Length: 10.93 m (35 ft 10 in)
  • Wingspan: 9.69 m (31 ft 9 in)
  • Height: 4.29 m (14 ft 1 in)
  • Wing area: 15.63 m2 (168.2 sq ft)
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Powerplant

  • Empty weight: 2,821 kg (6,219 lb)
  • Gross weight: 3,500 kg (7,716 lb)
  • Max takeoff weight: 5,000 kg 
  • Powerplant: 1 × Honeywell TFE731-2-2N turbofan engine, 15.57 kN (3,500 lbf) thrust
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Specifications

  • Maximum speed: 819 km/h (509 mph, 442 kn) at 7,000 m (23,000 ft)
  • Cruise speed: 747 km/h (464 mph, 403 kn) at 4,000 m (13,000 ft)
  • Never exceed speed: M0.81 at 9,500 m
  • Range: 1,500 km (930 mi, 810 nmi)
  • Service ceiling: 12,900 m (42,300 ft)
  • Rate of climb: 30.2 m/s (5,940 ft/min)
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Armament

    • Guns:
      • 1× 30 mm (1.18 in) Defa-Giat 554 with 145 rounds of ammo.
      • 4x 7,62 mm Colibri Pods
    • Hardpoints: 5 with a capacity of
      • 400 kg (880 lb) on inboard 
      • 250 kg (550 lb) on fuselage centerline
    • Missiles:
      • LAU-32/51 rocket pods
      • LAU-10 rocket pods
    • Bombs:
      • Mk81/ Mk82 bombs
     
Special Links FAdeA FMA IA-63 Pampa

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FAdeA FMA IA-63 Pampa

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