Kapten Trumm kirjutas:
Kaks teist lennukit, Jak-1 ja LaGG-1/3 olid aga 20 mm kahuri ja 12,7ga. Esimesel 1 ja teisel 2.
1942 aastaks moodustasid need enamuse hävitajatest rindel (MiG-3 tootmine lõppes 1941 ja rindelt viidi need 1941 lõpus ära) ja mingid seletamatut valgust sovjette kergekuulipilduja sobimatusest õhusõjas 1942 ei tabanud. See "valgus" tabas sovjette juba paar aastat varem ja küllap oleks ka MiG-3 tabanud, kui kahuri panek oleks tehniliselt võimalik olnud. Nimelt ei võimaldanud mootori ehitus sinna paigutada kahurit silindriridade vahele, mujale kahuri panekuks oli lennuk juba liiga raske (nendega eksperimenteeriti, kuid loobuti).
Seega versioon, et 1942 "said venelased aru" 7,62 sobimatusest õhusõjaks ei näi vett pidavat. Venelaseid said sellest aru juba 1939-1940 (osa veelgi varem) ja sellega ma padrunite ülejääke 1942 ei riskeeriks seostada. "Kergekuulipildujarelvastuse näite" MiG-1/3 tootmisarv oli alla 4000 lennuki (mis vene lennukitööstuse tootmisarvude juures oli üks väike rariteet).
Oh sind, uskumatut pärtlit, mat tvoju, on sinuga ikke raske..

Tsiteeri:
In 1939, Alexander Yakovlev designed a tandem-seat advanced trainer, originally designated "I-27" and then "UTI-26", offered along with the original I-26 proposal that became the Yak-1. The "UTI" (Uchebno Trenirovochnyi Istrebitel, translated as: Training Fighter) was intended to give pilots-in-training experience on a high-performance aircraft before transitioning to a fighter. With development work started in 1940, the UTI-26 differed from its predecessor in its larger span wing being placed farther back for balance as well as having two cockpits with dual controls and a rudimentary communication system. It was armed with a single 7.62 mm (0.30 in) ShKAS machine gun in the cowling, mainly for use in training, but Yakovlev envisioned a multi-purpose aircraft that could also undertake courier and light transport duties at the front.
The first production aircraft known as Yak-7UTIs retained a retractable main landing gear, but beginning in the summer of 1941, a fixed landing gear variant, the Yak-7V (Vyvozoni for Familiarization) was substituted. The factory reasoned that production would be simplified and that reduced performance would not be detrimental for a trainer. Yak-7UTIs and Yak-7Vs were also equipped with skis for winter operations.
A factory team from N° 301, headed by K.A. Sinelshchikov, was detached from the Yakovlev OKB to supervise production of Yak-7UTI. One of these aircraft (serial number 04-11) was fitted with an armored backrest plate over the rear position, self-sealing fuel tanks which filled with inert gas as they emptied, three "RO" rocket launchers under each wing for as many RS-82 rockets, an axial motornaya pushka-mount 20 mm (0.79 in) ShVAK cannon firing through the propeller spinner, with 120 rounds, and two 7.62 mm ShKAS machine guns under the cowling, each with 750 rounds.[3] The rear cockpit position was retained, allowing it to accommodate a second seat (without controls) for fast courier and transport duties or a fuel tank for extended range. The additional space could also house bombs or other gear. The engine was an M-105P and the model was designated Yak-7/M-105P.
Tsiteeri:
Armament
1 × 20 mm (0.787 in) ShVAK cannon
2 × 7.62 mm (0.300 in) ShKAS machine guns. Later models like the "B", used x2 12.7mm Berezin UB guns.
Tsiteeri:
Produced 6,399, mat tvoju.