Cookie Consent by TermsFeed 1974 - 1983 PIPER PA-31T-620 Cheyenne II - Specifications, Performance, Operating cost, Valuation, Brokers - planephd.com

1974 - 1983 PIPER PA-31T-620 Cheyenne II

Twin engine turboprop aircraft with retractable landing gear. The PA-31T-620 Cheyenne II seats up to 7 passengers plus 1 pilot.


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Performance specifications


Horsepower:

2 x 620 HP

Best Cruise Speed:

269 KIAS

Best Range (i):

1,444 NM

Fuel Burn:

72.2 GPH

Stall Speed:

75 KIAS

Rate of climb:

2,710 FPM

Rate of climb (1 engine out):

660 FPM

Ceiling:

31,600 FT

Ceiling (1 engine out):

14,600 FT

Takeoff distance:

1,410 FT

Landing distance:

1,430 FT

Takeoff distance over 50ft obstacle:

1,980 FT

Landing distance over 50ft obstacle:

2,480 FT


Weights


Gross Weight:

9,000 LBS

Empty Weight:

5,018 LBS

Maximum Payload:

1,102 LBS

Fuel capacity:

382 GAL


Engine (x2)


Manufacturer:

Pratt & Whitney

Model:

PT6A-28

Horsepower:

620 HP

Overhaul (HT):

3,600 Hrs

Also Consider


PIPER PA-31T-620 Cheyenne II XL (1981 - 1984)

Image description

Best Cruise: 270 KIAS ( 1 )
Best Range: 1336 NM ( 108 )
Fuelburn: 75.5 GPH ( 3.3 )

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