Piper Turbo Dakota
Piston • single engine • Low Wing • Fixed gear
Range Visualization
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Payload vs. Range
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Default: 190 lbs (FAA standard)
Default: 30 lbs
Passengers
lbs
@ lbs / pax
0 lbs
Fuel on board
gal
+ Weight
Range
Available Range
/ nm
Mission capable —
Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required —
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( gal usable for nm range).
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Mission Profile
154
KTAS
Cruise Speed
4
Occupants
729
nm
Max Range
889
lbs
Wet Payload
About the Piper Turbo Dakota
The Piper PA-28-201T Turbo Dakota is a four-seat, fixed-gear, turbocharged variant of the Cherokee family produced for the 1979-1980 model years. Powered by a 200 hp Continental TSIO-360-FB engine, it offers improved high-altitude performance (service ceiling 20,000 ft) with a best cruise speed of 154 kt. Only produced for one year due to limited sales.
Technical Specifications
Dimensions
- Wingspan
- 35.417 ft
- Length
- 25.0 ft
- Height
- 7.583 ft
Weights
- Max Takeoff Weight
- 2,900 lbs
- Max Landing Weight
- 2,900 lbs
- Useful Load
- 1,321 lbs
- Fuel Capacity
- 72 gal
Performance
- Cruise Speed
- 154 KTAS
- Range
- 729 NM
- Service Ceiling
- 20,000 ft
- Rate of Climb
- 902 fpm
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