Beechcraft C-12A Huron

Beechcraft · United States · first flew 1974 · transport aircraft

The C-12A Huron is the initial military variant of the Beechcraft King Air A200, adopted by the US Army and US Air Force from 1975 as a utility transport and liaison aircraft.

Recognition (WEFT)

W — Wings	Low-mounted, straight
E — Engines	2 × turboprop, wing-mounted
F — Fuselage	13.34 m fuselage
T — Tail	T-tail

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Initial military King Air A200 variant for US Army and USAF
Twin turboprop low-wing transport with T-tail
Entered service 1975 as utility transport and liaison aircraft

Low-wing twin-turboprop with a circular-section fuselage, T-tail, and winglet-less straight wing; the rounded nose and square cabin windows distinguish it from later Super King Air 350 variants.

Specifications

The Beechcraft C-12A Huron has a length of 13.34 m (44 ft).
It has a wingspan of 16.61 m (54 ft).
Its maximum speed is 536 km/h (333 mph).
Typical crew: 2.

Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.

History

Ordered to replace ageing piston-engined transports, the C-12A entered US Army and USAF service in 1975. Based on the commercial King Air 200, it retained the civil airframe with minimal military modifications, offering proven reliability and commonality with the commercial fleet.

Variants

The C-12A was the baseline of a large family; subsequent variants (C-12C, D, F, and others) introduced improved avionics, cargo doors, and special-mission equipment.

Where you'll see it

The C-12A served widely with US Army and USAF units worldwide in the utility and staff transport role, and continues to serve in various guises with allied nations.

Related aircraft

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