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General Info

Embraer EMB 314/A-29 Super Tucano

Role 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 Embraer S.A. aerospace corporation  
Embraer EMB 314/A-29 Super Tucano



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

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aviation conglomerate, DINFIA, realised that its IA 35 Huanquero twin-piston engined light transport was becoming outdated, and it was decided to develop a turboprop-engined derivative.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

Embraer S.A. aerospace corporation
Embraer EMB 314/A-29 Super Tucano

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General Info

  • Crew: 2
  • Length: 9.86 m (32 ft 4 in)
  • Wingspan: 11.14 m (36 ft 7 in)
  • Height: 3.4 m (11 ft 2 in)
  • Wing area: 19.4 m2 (209 sq ft)
  • Airfoil: root: NACA 63A415; tip: NACA 63A212 [
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Powerplant

  • Empty weight: 1,810 kg (3,990 lb)
  • Max takeoff weight: 3,175 kg 
  • Fuel capacity: 694 litres (183 US gal; 153 imp gal)
  • Powerplant: 1 × Pratt & Whitney Canada PT6A-25C turboprop engine, 552 kW (740 hp)
  • Propellers: 4-bladed constant-speed propeller
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Specifications

  • Maximum speed: 458 km/h (285 mph, 247 kn) at 4,115 metres 
  • Stall speed: 124 km/h (77 mph,
  • Never exceed speed: 539 km/h 
  • Range: 1,916 km (1,191 mi, 
  • Service ceiling: 8,750 m 
  • g limits: +6 /-3
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Armament

    • Guns: ** Gun pods:
        • AN/M-B machine gun
        • 12,7 mm machine gun
        • 7,62 mm machine gun (500 rounds)
      • Rocket Machine Gun pod:
        • RMP LC with a 12.7mm M3P and (4x) 70 mm
    • Hardpoints: 4 under-wing pylons with a capacity of 1,000 kg (2,200 lb)
     
Special Links Embraer S.A. aerospace corporation

Links to Youtube & Others

Last operational G-II, retired in 2006, at the Museo Nacional de Aeronáutica de Argentina ("National Aeronautics Museum".

FAdeA FMA IA-50 Gurani II

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