Piper Cheyenne 400 LS

Overview

The Cheyenne 400LS is usually configured to seat a pilot and seven passengers with an additional passenger occupying the right seat on the flight deck, if desired. Cabin seating is commonly arranged in a four-seat club with three additional seats available. The Cheyenne 400LS is powered by a pair of Honeywell/Allied Signal TPE331-14-801 turboprop engines derated to 1000 shp and turning four-blade, counter-rotating, constant speed Hartzell propellers. The inspection interval on the engines is 3,000 hours.


Aircraft Specifications

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Aircraft Characteristics


Certified Crew
1
Typical / Maximum Cabin Passenger Capacity
8/8
Take Off Ground Roll (FT)
0
Landing Ground Roll (FT)
0
Balanced Field Length [SL/ISA TMP] (FT)
2,325
Maximum Fuel (GL)
0
Length (FT)
43.4
Wingspan (FT)
47.7
Height (FT)
17
Cabin Height (FT)
4.7
Cabin Width (FT)
4.3
Cabin Length (FT)
17.7
Baggage Capacity Internal / External (CFT)
0/42
Powerplant
2 HON TPE331-14

General Information


Years Aircraft Manufactured
1984-1991
Estimated Retail Price Low
895,000
Estimated Retail Price High
1,350,000
Aircraft Category
ME TP < 12,500 LBS

Operating Cost Overview

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Range Map

The Piper Cheyenne 400 LS has a range of 727 nautical miles. You can use the map below to visual this range from a particular airport...


Legend


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