FMA IA 50 Guaraní II
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IA 50 Guarani II | |
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Type | Multi-purpose aircraft |
Manufacturer | Fabrica Militar de Aviones (FMA) |
Designed by | n/a |
Maiden flight | 26 April 1963 |
Introduced | 1966 |
Retired | 7 January 2007 |
Status | Retired |
Primary user | Fuerza Aérea Argentina |
Number built | 3 prototypes + 32 series aircraft |
Developed from | IAe 35 “Huanquero” |
The I.A. 50 Guarani II was an Argentine Multipurpose aircraft designed at the DINFIA (successor to the "Instituto Aerotecnico" - AeroTechnical Institute) in the early 1960s.
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[edit] History
A twin-engined light transport known as the Guarani I was developed from the Huanquero and first flew on 6 February 1962. The design was a refined version of the Huanquero, keeping 20% of the structure and with an all-metal wing. The aircraft was further developed as the Guaruani II; the main difference was a single swept fin and a shortened rear fuselage. It also used the more powerful Turbomeca Bastan VIA turboprop. The fuselage was semi-monocoque with squared cross-section, and it had unswept wings and swept tailplanes. The prototype flew on 26 April 1963.
In June 1965 the G-II prototype (serial number TX-01) was shown at the Paris Air Show (Le Bourget, 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.
The last flying example, retired in 2006 at the II Brigada Aérea (IInd Air Brigade), at Paraná, Entre Rios, Argentina, is currently at the National Aeronautics Museum ("Museo Nacional de Aeronáutica") of the Argentine Air Force (Fuerza Aérea Argentina), at Morón, Buenos Aires, Argentina.
[edit] Users
- Argentine Air Force
- Argentine Federal Police
- Servicio Penitenciario Federal
- Líneas Aéreas Provinciales de Entre Ríos
- Gobierno de Córdoba
- Gobierno de Salta
- Ministerio de Bienestar Nacional
[edit] Specifications (IA 50)
General characteristics
- Crew: 2
- Capacity: 15 passengers
- Length: 48 ft 9 in (14.86 m)
- Wingspan: 64 ft 1 in (19.53)
- Height: 19 ft 0¾ in (5.81 m)
- Wing area: 449.95 ft² (41.8 m²)
- Empty weight: 8,651 lb (3924 kg)
- Max takeoff weight: 15,697 lb (7120 kg)
- Powerplant: 2× Turbomeca Bastan VIA Turboprop, 930 shp (694 kW) each
Performance
- Maximum speed: 311 mph (500 km/h)
- Cruise speed: 280 mph (450 km/h)
- Range: 1,240 miles (1995 km)
- Service ceiling 41,010 ft (12500 m)
[edit] References
Article on the 50th anniversary of the "Fabrica Militar de Aviones" - listing all the aircraft developed and manufactured there since 1927, Aerospacio, Buenos Aires, 1977. (in Spanish)
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.
[edit] External links
- (Spanish) Development and Specifications
- (Spanish) Individual aircraft histories
- (Spanish) Newspaper article about the G-II
[edit] Related content
Comparable aircraft
- Dassault MD.320, France, circa 1950s
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