The Short C-23 Sherpa was designed as a twin-engine turboprop strut-braced high-wing aircraft with an H-shaped tail assembly. The aircraft was built on the basis of a fuselage with a length of 17.7 m with a square cross section and characteristic nose and tail contours.
Short C-23 Sherpa is equipped in the center section of two Pratt & Whitney Canada PT6A-45-R turboprop engines with a capacity of 1200 hp each. The motors were equipped with Hartzell five-blade variable-pitch propellers with a diameter of 2.82 m.
Short C-23 Sherpa has a cruise speed of 350 km/h (220 mph), a maximum range of 1,239 km (770 mi) with a payload of 2.2 tonnes. The aircraft was operated by two pilots, the third crew member was responsible for handling cargo.
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