Эскизный проект самолета Ил-14

ILYUSHIN IL-14 ("CRATE") . Data: Designer : S. Ilyushin. Power: two 2,600-h.p. ASh-82T radial engines. Accommodation: crew of four plus 15-32 passengers. Dimensions: span 104 ft.; length 69 ft. 11 in.; weight (maximum take off) 36,383 lb. Performance figures not available.

AVIA 14. The Avia 14 is the Czech-built Ilyushin IL-14, which is itself a development of the IL-12. The 14 differs externally from the 12 mainly in that it has a revised fin and rudder configuration, square instead of round wingtips and some thrust augmentation to its later series engines, similar to that employed on the Convair-Liner. Short field performance for the Avia 14 is claimed by the manufacturers and take-off and landing figures of less than 2,000 ft. on grass or unimproved fields are quoted. It is claimed to be capable of taking-off and attaining cruising altitude with normal payload on one engine. The aircraft is available in many versions including interior layouts for twenty-four, twenty-eight and thirty-two passengers, as well as a twelve-seat executive and V.I.P. version. A large galley is part of the standard equipment and the cabin is not pressurised but is ventilated and heated in normal fashion. Powerplants are two M-82T 14-cylinder direct-injection radial engines rated at 1,900 h.p. each for take-off. These engines are identical to the ASh-82FNVs used on the Russian IL-14. Propellers are four-bladed AV 50s. Hot-air de-icing is used for wing and tailplane leading edges and cockpit windows, the latter are also electrically heated and fitted with alcohol sprays.
Salient features: Twin-engined low-wing single fin and rudder passenger/freight aircraft with various interior layouts.

Ил-14М