Overview

The Cheyenne II is normally configured to seat seven in addition to the pilot, including one occupant in the right seat on the flight deck. Main cabin seating is commonly arranged in a four-seat club plus two individual seats. The Cheyenne II is powered by a pair of Pratt & Whitney Canada PT6A-28 turboprop engines rated at 620 shp each, driving three-bladed, constant speed, full feathering Hartzell propellers. Engine inspection interval is 3,600 hours.


Aircraft Specifications


Certified Crew

1

Typical / Maximum Cabin Passenger Capacity

6/7

Balanced Field Length [SL/ISA TMP] (FT)

1980

Length (FT)

34.7

Wingspan (FT)

42.7

Height (FT)

12.8

Cabin Height (FT)

4.3

Cabin Width (FT)

4.2

Cabin Length (FT)

8.4

Baggage Capacity Internal / External (CFT)

0/42

Powerplant

2 P&WC PT6A-28

Years Aircraft Manufactured

1974-1983

Estimated Retail Price Low

309,000

Estimated Retail Price High

550,000

Aircraft Category

ME TP < 12,500 LBS



Operating Cost Overview

Aircraft variable and fixed costs are important to determine before making a purchase decisions or planning annual budgets. Our interactive graphs demonstrate the relationships between fuel cost and annual flight hour utilization.



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If you are further along in the aircraft buying process, our comprehensive aircraft operating cost reports are the perfect companion in your decision making process. View a sample or buy a report and have it available in minutes.




Range Map

The Piper Cheyenne II has a range of 1,219 nautical miles. Type in your city or airport identifier for a visual representation of the NBAA IFR Range (NM) for this aircraft.


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