Piper Cheyenne I

Overview

The Cheyenne I is normally configured to seat six passengers in addition to the pilot, including one occupant in the right seat on the flight deck. The cabin seating is commonly arranged in a four-seat club, with an individual fifth seat aft, opposite the airstair door. The Cheyenne I is powered by a pair of Pratt & Whitney of Canada PT6A-11 turboprop engines rated at 500 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)
2444
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-11

General Information


Years Aircraft Manufactured
1978-1984
Estimated Retail Price Low
275,000
Estimated Retail Price High
489,000
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.


$
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Range Map

The Piper Cheyenne I has a range of 1,171 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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