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 Specifications

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Aircraft Characteristics


Certified Crew
1
Typical / Maximum Cabin Passenger Capacity
6/7
Take Off Ground Roll (FT)
0
Landing Ground Roll (FT)
0
Balanced Field Length [SL/ISA TMP] (FT)
1,980
Maximum Fuel (GL)
0
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

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Range Map

The Piper Cheyenne II has a range of 1,282 nautical miles. You can use the map below to visual this range from a particular airport...


Legend


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