Girish Mahajan (Editor)

FMA IA 50 Guaraní II

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Top speed
  
501 km/h

Length
  
15 m

First flight
  
April 26, 1963

Wingspan
  
20 m

Retired
  
7 January 2007

FMA IA 50 Guaraní II cdnwwwairlinersnetphotosairliners58117451

Manufacturer
  
Fábrica Argentina de Aviones

The I.A. 50 Guaraní II was an Argentine utility aircraft designed at the DINFIA (successor to the "Instituto Aerotecnico" - AeroTechnical Institute) in the early 1960s.

Contents

FMA IA 50 Guaraní II FMA Fabrica Militar de Aviones IA 50 Guarani II Specifications

History

FMA IA 50 Guaraní II Airlinersnet

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state aviation conglomerate, DINFIA, realised that its IA 35 Huanquero twin-piston engined light transport was becoming outdated, and it was decided to develop a turboprop-engined derivative.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.

FMA IA 50 Guaraní II FMA IA50 Guarani II

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.

Operations

FMA IA 50 Guaraní II FMA IA50 Guarani II Argentina Air Force Aviation Photo

In June 1965 the Guarani II prototype (serial number TX-01) was exhibited and flown at the Paris Air Show at Le Bourget Airport, France). TX-01 was later flown to the CEV (“Centre d’Essays en Vol”, Air Test Centre) at Istres, France, for technical evaluation, where it was tested for a total of 200 flying hours. It was flown back to the FMA, Argentina in February 1966, being the first Latin American-built aircraft to fly across the Atlantic Ocean.

FMA IA 50 Guaraní II FMA IA 50 Guaran II Wikipedia

The last flying example, retired in 2006 at the II Brigada Aérea (IInd Air Brigade), at Paraná, Entre Rios, Argentina, is currently preserved at the National Aeronautics Museum ("Museo Nacional de Aeronáutica") of the Argentine Air Force (Fuerza Aérea Argentina), at Morón, Buenos Aires, Argentina.

Users

  • Argentine Air Force
  • Argentine Federal Police
  • Argentine Navy
  • Argentine Naval Aviation
  • Servicio Penitenciario Federal
  • Líneas Aéreas Provinciales de Entre Ríos
  • Government of Córdoba
  • Government of Salta
  • Ministry of National Welfare
  • Specifications (IA 50)

    Data from Jane's All The World's Aircraft 1965-66

    General characteristics

  • Crew: 2
  • Capacity: 15 passengers
  • Payload: 1,810 kg (2,600 lb)
  • Length: 14.86 m (48 ft 9 in)
  • Wingspan: 19.53 m (64 ft 1 in)
  • Height: 5.81 m (19 ft 0¾ in)
  • Wing area: 41.81 m² (450 ft²)
  • Airfoil: NACA 633218
  • Aspect ratio: 9
  • Empty weight: 3,924 kg (8,650 lb)
  • Max. takeoff weight: 7,120 kg (15,700 lb)
  • Powerplant: 2 × Turbomeca Bastan VI-A Turboprop, 694 kW (930 shp) each
  • Performance

  • Never exceed speed: 515 km/h (278 knots, 320 mph)
  • Maximum speed: 500 km/h (270 knots, 311 mph)
  • Cruise speed: 450 km/h (243 knots, 280 mph) (econ. cruise)
  • Stall speed: 145 km/h (78 knots, 90 mph)
  • Range: 1,995 km (1,078 nmi, 1,240 mi)
  • Service ceiling: 12,500 m (41,010 ft)
  • Rate of climb: 13.4 m/s (2,640 ft/min)
  • References

    FMA IA 50 Guaraní II Wikipedia