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IAR IAR-823

 

iar823


The piston-engined IAR-823 two/-five-seat training/liaison aircraft first flew in July 1973 and series production started in 1974. The aircraft has a retractable tricycle undercarriage, two underwing hardpoints for fuel tanks or practice weapons, and is aerobatic under certain payload conditions. Power plant is a 216kW Lycoming I0-540.

 CNIAR-823-01
 
 
Engine: 1 x Lycoming IO-540-G1D5, 215kW / 290 hp
Prop: Hartzell
Wingspan: 10.0 m / 32 ft 9.25 in
Wing area: 15.0 sq.m / 161.46 sq ft
Length: 8.24 m / 27 ft 0.25 in
Height: 2.5 m / 8 ft 2 in
Empty weight aerobatic: 880 kg / 1940 lb
Empty weight utility: 900 kg / 1984 lb
MTOW aerobatic: 1186 kg / 2614 lb
MTOW utility: 1380 kg / 3042 lb
Loaded weight: 880 kg / 1940 lb
Usable fuel: 90 USG
Fuel Burn: 15 USG/Hr
Max speed: 300 km/h / 186 mph
Max cruise speed 75%: 280 km/h / 174 mph / 151 kt at 5750 ft / 1750 m
Service ceiling: 5800 m / 19050 ft
ROC: 1378 fpm / 420 m/in
Range w/max.fuel: 1350 km / 839 miles 728 nm
Range w/max.payload: 700 km / 435 miles / 700 km
Seats: 4
Loading: +6/-3
Cabin baggage capacity: 88 lb / 40 kg

 

CNIAR-823-ld

 


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