An-12

 

Aircraft description
 The An-12 cargo turboprop aircraft was developed in 1957 by Antonov Design Bureau for medium- and long-haul cargo operations. The An-12 is configured as the cantilever metal monoplane with high-mounted wing, elevated fuselage tail, single-fin tail and retractable three-strut landing gear with steering nose wheel. The landing gear wheels with low-pressure tires permit to operate the aircraft from the unpaved airfields. Four AI-20 turboprops are mounted on the wings furnished with double-slotted
Technical characteristics
 FLIGHT PERFORMANCE:   crew, persons7maximum takeoff weight, t.64,0maximum payload capability, t.20,0maximum flight range, km.4000maximum fuel capacity, kg.22500maximum flight speed, km./h.680cruise speed, km./h.510operational ceiling, m.10200takeoff run, m.1230landing roll (with 58.0t landing weight), m.1125required runway length, m.2200   OVERALL DIMENSIONS: wing span, m.38,015aircraft length, m.33,109height, m.11,44wing area, m2121,70lg base, m.7,85cargo cabin: - width, m.2,89- height, m.2,40