IAR-827

From Wikipedia, the free encyclopedia
Jump to: navigation, search
IAR-827 and IAR-828
IAR828 2012 4.jpg
Role Agricultural aircraft
National origin Romania
Manufacturer IAR
Designer Radu Manicatide
First flight 22 July 1976

The IAR-827 was an agricultural aircraft built in Romania in the 1970s and 1980s. The penultimate member of the family of designs that began with the IAR-821, it was, like the others, a conventional low-wing monoplane with fixed, tailwheel undercarriage, and shared the all-metal construction of the IAR-826. The prototype flew in 1976, powered by a Lycoming IO-720 engine, but the production examples that followed all had the PZL-3S.

In 1981, the IAR-827 prototype was re-engined with a Pratt & Whitney Canada PT6A turboprop and redesignated first as the IAR-827TP and later as the IAR-828'. Plans to produce the aircraft either with the Pratt & Whitney Canada engine or a Walter 601 never materialised.


Variants[edit]

Specifications (IAR-827A)[edit]

General characteristics

  • Crew: One pilot
  • Capacity: 1,200 L (320 US Gal) of chemicals
  • Length: 8.80 m (28 ft 11 in)
  • Wingspan: 14.00 m (45 ft 11 in)
  • Height: 2.60 m (8 ft 7 in)
  • Wing area: 29.4 m2 (316 ft2)
  • Empty weight: 1,660 kg (3,660 lb)
  • Gross weight: 2,800 kg (6,200 lb)
  • Powerplant: 1 × PZL-3S, 450 kW (600 hp)

Performance

  • Maximum speed: 210 km/h (130 mph)
  • Range: 650 km (400 miles)
  • Service ceiling: 4,500 m (14,800 ft)

References[edit]

  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 527. 
  • Simpson, R. W. (1995). Airlife's General Aviation. Shrewsbury: Airlife Publishing. p. 341. 
  • Уголок неба