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An upgraded version of the I.A.R. 817 which was built in 1955, the I.A.R. 818 first flew in 1960.
 | A three-view drawing (706 x 1018) |
| ENGINE | 1 x M-337, 155kW |
| WEIGHTS |
| Take-off weight | 1300 kg | 2866 lb |
| Operating empty weight | 825 kg | 1819 lb |
| DIMENSIONS |
| Wingspan | 12.1 m | 39 ft 8 in |
| Length | 10.0 m | 32 ft 10 in |
| Wing area | 25.4 m2 | 273.40 sq ft |
| PERFORMANCE |
| Max. speed | 185 km/h | 115 mph |
| Cruise speed | 165 km/h | 103 mph |
| Ceiling | 4000 m | 13100 ft |
| Range w/max.fuel | 900 km | 559 miles |
| Range w/max.payload | 250 km | 155 miles |
Sorin Lupu, sorinlupu67(@)yahoo.ro, 02.03.2008
This is one of the first (if not the first ) series produced airplane to use winglets to reduce wing drag.It,s helycopter - like tail aloud the use of two back fuselage doors, mostly for medical emergencies, being used by Aviasan ( Romanian Air ambulance).
Sorin Lupu, sorinlupu67(@)yahoo.ro, 02.03.2008
This is one of the first (if not the first ) series produced airplane to use winglets to reduce wing drag.It,s helycopter - like tail aloud the use of two back fuselage doors, mostly for medical emergencies, being used by Aviasan ( Romanian Air ambulance).
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Do you have any comments concerning this aircraft ?
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