IAR-824
IS-24, IAR-824 |
Role |
Civil utility aircraft |
National origin |
Romania |
Manufacturer |
IAR |
Designer |
Iosif Silimon |
First flight |
1971 |
The IAR-824 (originally known as the ICA IS-24) was a utility aircraft built in Romania in the 1970s. Developed from the ICA IS-23A, it was a conventional high wing cantilever monoplane with fixed tricycle undercarriage and seating for six people within an enclosed cabin. A small number were built, with five going to Romania's Aeroclub for training and glider towing.
Specifications
General characteristics
- Crew: One pilot
- Capacity: 5 passengers
- Length: 9.20 m (30 ft 2 in)
- Wingspan: 12.40 m (40 ft 8 in)
- Height: 3.30 m (10 ft 10 in)
- Wing area: 23.6 m2 (254 ft2)
- Empty weight: 1,240 kg (2,730 lb)
- Gross weight: 1,900 kg (4,100 lb)
- Powerplant: 1 × Lycoming IO-540-G1D5, 290 kW (215 hp)
Performance
- Maximum speed: 200 km/h (125 mph)
- Range: 800 km (500 miles)
- Service ceiling: 3,000 m (9,800 ft)
References
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. pp. 527.
- Simpson, R. W. (1995). Airlife's General Aviation. Shrewsbury: Airlife Publishing. pp. 341.
- Уголок неба
|
|
Powered aircraft |
|
|
Series ICA (gliders and motor gliders) |
|
|
Under licence |
|
|
Series 300 (helicopters) |
|
|
Series 800 |
|
|
IAR Projects |
|
|
IAR Engines |
|
|
|
|
General |
|
|
Military |
|
|
Accidents/incidents |
|
|
Records |
|
|