Piper PA-42 Cheyenne III Civil Aircraft Model Details

If you are looking for Piper PA-42 Cheyenne III parts and other civil aircraft components, look no further. ASAP Aerospace is an ASAP Semiconductor subsidiary with access to an inventory of over six billion new, used, and obsolete parts. We operate as an FAA AC 00-56B accredited and ISO 9001:2015 certified enterprise and adhere to a strict no China sourcing policy.

Our dedication to quality does not end there, as every part of civil aircraft model Piper PA-42 Cheyenne III is subjected to rigorous quality assurance testing by our expert team to ensure our customers only receive the best. If you are ready for a competitive quote, submit an RFQ today and a dedicated account manager will be in touch.

General Information of Piper PA-42 Cheyenne III

Developed From : Piper PA-31T Cheyenne

First Flight : May 18, 1979

Manufacturer : Piper Aircraft

Number Built : 192; 149 IIIAs and 43 400s

Role : Turboprop

Unit_Cost : $429,000 base in 1975[1]; $1,830,000 in 2012 USD

General characteristics of Piper PA-42 Cheyenne III

Capacity : 1 to 9 passengers

Crew : One or two

Empty Weight : 6,837 lb (3,101 kg)

Height : 14 ft 9 in (4.50 m)

Length : 43 ft 4¾ in (13.23 m)

Max Takeoff Weight : 11,200 lb (5,080 kg)

Powerplant : 2 × Pratt & Whitney Canada PT6A-41 turboprop, 720 shp (537 kW) each

Wing Area : 293.0 ft² (27.22 m²)

Wingspan : 47 ft 8 in (14.53 m)

Performance of Piper PA-42 Cheyenne III

Cruise Speed : 282 knots (523 km/h, 325 mph) at 35,000 ft (10,700 m)

Maximum Speed : 314 knots (582 km/h, 362 mph)

Power/Mass : 0.13 hp/lb (0.21 kW/kg)

Range : 2,270 nmi (4,207 km, 2,614 mi)

Rate Of Climb : 2,380 ft/min (12.1 m/s)

Service Ceiling : 35,840 ft (10,925 m)

Stall Speed : 89 knots (165 km/5, 103 mph) (flaps and undercarriage down)

Wing Loading : 38.2 lb/ft² (186.7 kg/m²)

If you have any parts requirement for this model then simply request a quote here!