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Kazan Aviation Institute KAI-14
The Kazan Aviation Institute at Kazan designed and produced the KAI-14 high performance Standard Class single seater. Designed by a team headed by M. P.Simonov; of all-metal construction it made its first flight in about 1962, and two KAI-14s were entered in the 1965 World Championships held at South Cerney in England.
Two versions of the type have been produced, the first being for competition flying with the pilot seated in a reclining position under a long flush-fitting one-piece transparent canopy; this version has a polished metal finish to reduce drag.
The second version, intended for series production, is similar except that the pilot sits upright in a conventional seat under a raised cockpit canopy, and is unpolished. Both versions are otherwise the same, with cantilever shoulder wings with a forward sweep of 2° at the leading edges and compound taper on the trailing edges; the inset ailerons are each in two sections and small trailing edge air brakes are featured. The wings are metal-covered as is the semi-monocoque fuselage, in which the forward section tapers to a slimmer rear half carrying the all-metal cantilever 'butterfly'-type V-tail. The landing gear consists of a non-retractable monowheel faired into the bottom of the fuselage, with a brake that is linked to the air brakes, and a tail bumper.



Span: 49 ft 2.5 in / 15.0 m
Length: 19 ft 1 in / 5.82 m
Wing area: 107.7 sq.ft / 10.0 sq.m
Aspect ratio: 22.5
Max weight: 573 lb / 260 kg
Water ballast: None
Max wing loading: 26.0 kg/sq.m / 5.32 lb/sq ft
Max permissible diving speed: 155 mph / 135 kt / 250 km/h
Max aero-tow speed: 87 mph
Landing speed: 43.5 kt / 80 km/h
Min sinking speed: 1.90 ft/sec / 0.58 m/sec at 56 mph / 48.5 kt / 90 km/h




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