Piper 22 Tri-Pacer
Piston • single engine • High Wing • Fixed gear
Range Visualization
Origin: · click map to move · nm at current load
Payload vs. Range
Customize assumptions
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 —
You'll need to leave gallons of fuel behind
( gal usable for nm range).
Over max gross weight —
Reduce payload by lbs
to safely operate this aircraft.
Mission Profile
116
KTAS
Cruise Speed
4
Occupants
430
nm
Max Range
-
lbs
Wet Payload
About the Piper 22 Tri-Pacer
Introduced in 1951. Piper PA-22 succeeded the Piper PA-20; added a nosewheel (as opposed to predecessor tailwheel). Culled from manufacturer site.
Technical Specifications
Dimensions
- Wingspan
- 29.3 ft
- Length
- 20.5 ft
- Height
- 8.3 ft
Weights
- Max Takeoff Weight
- 2,000 lbs
- Max Landing Weight
- 2,000 lbs
- Fuel Capacity
- 36 gal
Performance
- Cruise Speed
- 116 KTAS
- Range
- 430 NM
- Service Ceiling
- 16,500 ft
- Rate of Climb
- 800 fpm
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