Two Seat Tandem Trainer & Liason
Design:Aleksandr Sergeyevich Yakolev
Manufacturer: State Industries
Powerplant: One 1,050 hp (783 kw) M-105P 12-cylinder Vee engine.
Performance: Maximum speed 407 mph (655 km/h) at 10,170 ft (3100 m); service ceiling 35,105 ft (10700 m).
Range: 559 miles (900 km) on internal fuel.
Weight: Empty equipped 4,641 lbs (2105 kg) with a maximum take-off weight of 5,864 lbs (2660 kg).
Dimensions: Span 33 ft 7 1/2 in (10.25 m); length 27 ft 10 1/4 in (8.49 m); height 7 ft 11 1/4 in (2.42 m); wing area 159.53 sq ft (14.83 sq m).
Armament: One engine mounted 20 mm ShVAK cannon with 140 rounds and two synchronised 12.7 mm (0.50 in) UBS machine guns with 348 rounds each.
In parallel with the I-26 (or Y-26), the Yakovlev design bureau developed a two seat version under the designation Y-27. One pre-production I-26 was completed to this configuration. It was intended to not only serve as a dual control fighter trainer but also as a liason and unit support aircraft. Compared with the I-26, the Ya-27 was simplified and reduced in 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 that of the series Yak-1 aircraft. This performance, combined with the urgent need for 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 the 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 with production ending in early 1943. Of this number, some 1,500 were Yakovlev Yak-7Vs.
An excellent link for YAK History
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