|
|
Design of the An-10 airliner began in November 1955 and the prototype (named Ukraina) first flew in March 1957. Subsequently more than 500 An-10/10A are believed to have been built. The An-10 was the initial version with accommodation for 84 passengers and a 'play-room' for children at the rear. It entered service in July 1959 on routes from Simferopol to Moscow and Kiev. The An-10A developed version had a 2m longer fuselage and accommodated 100 to 130 passengers. It entered service in February 1960. An-10A also operated on skis in the far north of the Soviet Union. No An-10/10A were exported and Aeroflot withdrew the airliners in 1973. Both versions had the NATO reporting name Cat.
| CREW | 5 |
| PASSENGERS | 100-132 |
| ENGINE | 4 x turbo prop AI-20K, 2940 kW |
| WEIGHTS |
| Take-off weight | 55000 kg | 121255 lb |
| Empty weight | 30500 kg | 67241 lb |
| DIMENSIONS |
| Wingspan | 38.0 m | 124 ft 8 in |
| Length | 37.0 m | 121 ft 5 in |
| Height | 9.8 m | 32 ft 2 in |
| Wing area | 120.0 m2 | 1291.67 sq ft |
| PERFORMANCE |
| Max. speed | 725 km/h | 451 mph |
| Cruise speed | 660 km/h | 410 mph |
| Ceiling | 10000 m | 32800 ft |
| Range w/max.fuel | 4000 km | 2486 miles |
| Range w/max.payload | 1200 km | 746 miles |
|
Do you have any comments about this aircraft ?
|
| |