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FAdeA
FMA IA-50 Gurani II

General information
Type Multi-purpose aircraft

National origin Argentina
Manufacturer Fabrica Militar de Aviones (FMA)
First flight 26 April 1963
Introduction 1966 Retired 7 January 2007
Status Retired
Primary user Fuerza Aérea Argentina
Number built 3 prototypes + 32 series aircraft
Developed from IAe 35 Huanquero

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History Fabrica Argentina de Aviones (FAdeA)  
FAdeA FMA IA-50 Gurani II
First flight 26 April 1963 Introduction 1966 Retired 7 January 2007

In the early 1960s, the Argentine state aviation conglomerate, DINFIA, realised that its IA 35 Huanquero twin-piston engined light transport was becoming outdated, and it was decided to develop a turboprop-engined derivative. While of similar layout to the Huanquero, with both aircraft being twin-engined low-wing monoplane of all metal construction with a twin tail, the new aircraft, the Guaraní, shared only 20% of the structure of the Huanquero. It was powered by two Turbomeca Bastan III engines each rated at 850 shaft horsepower (630 kW). It first flew on 6 February 1962

The aircraft was further developed as the Guaruani II; the main difference being a single swept fin and a shortened rear fuselage. It also used more powerful (930 shaft horsepower (690 kW)) Bastan VIA engines. The fuselage was semi-monocoque with a squared cross-section, having unswept wings and swept tailplanes. The prototype Guaraní was rebuilt to this standard and flew in this form on 26 April 1963

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Max Crew

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Fabrica Argentina de Aviones (FAdeA)

FAdeA, a Lockheed Martin Company
FAdeA FMA IA-50 Gurani II
First flight 26 April 1963 Introduction 1966

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General Info

  • Crew: 2
  • Capacity: 15 passengers
  • Length: 14.86 m (48 ft 9 in)
  • Wingspan: 19.53 m (64 ft 1 in)
  • Height: 5.81 m (19 ft 1 in)
  • Wing area: 41.81 m2 (450.0 sq ft)
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Powerplant

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Specifications

  • Maximum speed: 500 km/h (310 mph, 270 kn)
  • Cruise speed: 450 km/h (280 mph, 240 kn) (econ cruise)
  • Stall speed: 145 km/h (90 mph, 78 kn)
  • Never exceed speed: 515 km/h (320 mph, 278 kn)
  • Range: 1,995 km (1,240 mi, 1,077 nmi) with max payload
  • Service ceiling: 12,500 m 
  • Rate of climb: 13.4 m/s (2,640 ft/min)
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Comparable aircraft

Special Links FAdeA FAdeA FMA IA-50 Gurani II

Links to Youtube & Others

The Guarani II was developed from it and the prototype flew for the first time on 23 April 1963. It was placed in production for the Argentinian Air Force for communications, photographic (with the Military Geographic Institute) and executive transport duties,

FAdeA FMA IA-50 Gurani II

The Guarani I light transport first flew in prototype form on 6 February 1962

interior

Youtube Link

Navy received one as a staff transport. A total of 41 G.IIs were built.

interior
Aircrafttotal : Fábrica Argentina de Aviones SA (FAdeA)

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