The PA-42 Cheyenne III was announced in September 1977. The first production Cheyenne III flew for the first time on May 18 1979 and FAA certification was granted in early 1980. Powered by 537kW (720shp) PT6A-41 turboshafts and new style a T-tail. Deliveries of production Cheyenne IIIs began on June 30 1980. 

Development and improvement of the III led to the PA-42-720 Cheyenne IIIA, with PT6A-61 engines, a higher service ceiling and revised systems and interior. Production of the PA-42 ended in February 1993.

 
 
Country of Origin
United States of America
 
Powerplants
PA-42-720 - Cheyenne III - Two 535kW (720shp) Pratt & Whitney Canada PT6A-41 turboprops driving three blade constant speed Hartzell propellers.
 
Performances
PA-42-720 - Max speed 537km/h (290kt), max cruising speed 461km/h (250kt), economical cruising speed 413km/h (223kt). Initial rate of climb 2.235ft/min. Service ceiling 33,000ft. Range at max cruising speed 3.100km (1.675nm). 
 
Weight
PA-42-720 - Empty 2.900kg (6.389lb), max ramp weight 5.125kg (11.285lb). 
 
Dimensions
PA-42-720 - Wing span (over tip tanks) 14.53m, length 13.23m, height 4.50m. Wing area 27.2mq.
 
Capacity
Two pilots on flight deck. Typical seating for six in main cabin in corporate configuration. Can be configured as an AIR AMBULANCE with one or two stretchers and two medical attendants.
 
Production
Total manufactured 149 III/IIIAs.
 
Type
Twin turboprop corporate transport
 
   
   
   
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