Piper Cheyenne II

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 Characteristics


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

General Information


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

Welcome to PlaneFastFacts©. 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.


$
hrs

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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