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In parallel with the I-26 (or Ya-26), the Yakovlev design bureau developed a two-seat version under the designation Yakovlev Ya-27. One pre-production I-26 was completed to this configuration. It was intended to serve not only as a dual-control fighter trainer, but also as a liaison and unit support aircraft. Compared with the I-26, the Ya-27 was simplified and of reduced weight, the tandem cockpits being enclosed by an extended glazed canopy. The resulting Yak-7 aircraft entered production in May 1941 and was soon found to have better flying qualities than those displayed by series Yak-1s. This performance, combined with the urgent need for more fighters, led to production of a single-seat version of which the first was flown in June 1941; in the following month the fighter was officially designated Yak-7A and the two-seater Yak-7V. By the end of 1941 a new single-seater, the Yak-7B, had replaced the Yak-7A . Total delivery of all versions of the Yak-7 was 6,399 aircraft, production terminating in early 1943; of this number, some 1,500 were Yakovlev Yak-7Vs.
| CREW | 1 |
| ENGINE | 1 x VK-105PF, 870kW |
| WEIGHTS |
| Take-off weight | 3050 kg | 6724 lb |
| Empty weight | 2330 kg | 5137 lb |
| DIMENSIONS |
| Wingspan | 10.0 m | 32 ft 10 in |
| Length | 8.5 m | 27 ft 11 in |
| Height | 1.7 m | 5 ft 7 in |
| Wing area | 17.2 m2 | 185.14 sq ft |
| PERFORMANCE |
| Max. speed | 520 km/h | 323 mph |
| Ceiling | 10000 m | 32800 ft |
| Range | 600 km | 373 miles |
| ARMAMENT | 1 x 20mm machine-guns, 2 x 12.7mm machine-guns |
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