Rahul Sharma (Editor)

IAR 825

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Top speed
  
470 km/h

Length
  
8.99 m

Wingspan
  
10 m

First flight
  
June 12, 1982

Manufacturer
  
Industria Aeronautică Română

The IAR-825 Triumf is a Romanian tandem multirole trainer aircraft based on the IAR-823 built for the Romanian Air Force. The aircraft is roughly in the same class with the Brazilian EMBRAER Tucano. IAR-825 is equipped with the Canadian Pratt & Whitney Canada PT6 turboprop engine. First flight took place on the 12 June 1982. Only one prototype exists, former YR-IGB, sold and registered in the USA in 2006 as N825BA. It was damaged in a forced landing on July 15, 2012.

Contents

Operators

 Romania
  • Romanian Air Force

    • Specifications (IAR-825)

    Data from Jane's All The World's Aircraft 1988-89

    General characteristics

  • Crew: 2
  • Length: 8.99 m (29 ft 6 in)
  • Wingspan: 10.00 m (32 ft 9¾ in)
  • Height: 3.20 m (10 ft 6 in)
  • Wing area: 15.00 m² (151.5 ft²)
  • Airfoil: NACA 23012 (modified)
  • Empty weight: 1,250 kg (2,756 lb)
  • Max. takeoff weight: 2,300 kg (5,070 lb)
  • Powerplant: 1 × Pratt & Whitney PT6A-15AG turboprop, 507 kW (680 hp)

    • Performance

  • Never exceed speed: 550 km/h (296 knots, 341 mph)
  • Maximum speed: 470 km/h (254 knots, 292 mph)
  • Cruise speed: 440 km/h (237 knots, 273 mph)
  • Stall speed: 105 km/h (57 knots, 66 mph)
  • Range: 1,400 km (755 nm, 870 mi)
  • Service ceiling: 9,000 m (29,525 ft)
  • Rate of climb: 16 m/s (3,150 ft/min)

    • References

    IAR 825 Wikipedia
    (Text) CC BY-SA