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IAR IAR-822 / IAR-826

 

iar822
IAR-822


Designed for agricultural use the first I.A.R. 822 flew in 1970. Series production started in 1971.

 

The IAR-822 was the initial single seat version of mixed wood and metal construction. The tandem two seat IAR-822B was used for training and glider towing.
 
The IAR-826 was as the IAR-822 but of all-metal construction.
 
CNIAR-826-01
IAR-826


Engine: 1 x Lycoming IO-540-G1D5, 215kW
Take-off weight: 1900 kg / 4189 lb
Loaded weight: 1060 kg / 2337 lb
Wingspan: 12.8 m / 41 ft 12 in
Length: 9.4 m / 30 ft 10 in
Height: 2.8 m / 9 ft 2 in
Wing area: 26.0 sq.m / 279.86 sq ft
Max. speed: 195 km/h / 121 mph
Cruise speed: 170 km/h / 106 mph
Ceiling: 4500 m / 14750 ft
Range w/max.fuel: 500 km / 311 miles

 

CNIAR-822-ld

 

CNIAR-822-01
IAR-822 / IAR-822B

 

 

 

 


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