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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 Specifications


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)

Powerplant

2 P&WC PT6A-11

Years Aircraft Manufactured

1978-1984

Estimated Retail Price Low

320000

Estimated Retail Price High

460000

Aircraft Category

ME Turboprop



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 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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