I-16 Type 10
In 1937 the next major version was developed. Initialy it was powered by 1 × Svhetsov M-25A, but soon it was powered by a Shvetsov M-25V for high altitude. Apart from the engine also armament was enhanced. Two 0.3 inch (7,62 mm) ShKAS guns were already in the wings, but two more were additionally placed in the nose above the engine. Some aircraft also received a Cannon in the nose to augment the I-16's armament.
Flaps were added to reduce landing speed and run, and for the first time a retractable landing ski was used as well.
This and the strengthening of the airframe in some places added weight, and it rose to more than 3,747 lb (1.700 kg). Nevertheless performance was more or less equal to the I-16 Type 5.
Number built: unknown out of 7.364+
Caption under this illustration translates: trailing edge

Trailing edge flaps separate of ailerons, inboard and under fuselage.
