Piper PA-28-161 Warrior II Weight and Balance Calculator
Use this calculator to check loaded weight and center of gravity for the Piper PA-28-161 Warrior II. Enter the current empty weight and empty arm from the aircraft weight and balance record for the individual aircraft.
Maximum takeoff weight: 2,325 lbs. Maximum landing weight: 2,325 lbs. Usable fuel: 48 US gal.
Data source: FAA Type Certificate Data Sheet 2A13, PA-28-161. How WBcalc sources aircraft data
Enter the aircraft loading and fuel plan to check takeoff and expected landing conditions. After calculating, you can print or save the completed weight and balance worksheet as a PDF.
Piper PA-28-161 Warrior II specifications
| Specification | Value |
|---|---|
| Maximum takeoff weight | 2,325 lbs |
| Maximum landing weight | 2,325 lbs |
| Forward CG at 1,950 lbs or less | 83 in |
| Forward CG at 2,325 lbs | 87 in |
| Aft CG limit | 93 in |
| Usable fuel | 48 US gal |
| Fuel arm | 95 in |
Source: FAA Type Certificate Data Sheet 2A13, PA-28-161.
Piper PA-28-161 Warrior II CG limits
| Aircraft weight | Forward CG limit | Aft CG limit |
|---|---|---|
| 1,950 lbs | 83 in | 93 in |
| 2,325 lbs | 87 in | 93 in |
The calculator uses the published CG envelope points and linear interpolation between forward-limit breakpoints where applicable.
Piper PA-28-161 Warrior II loading stations
| Station | Arm | Limit |
|---|---|---|
| Pilot and front passenger | 80.5 in | 400 lbs |
| Rear passengers | 118.1 in | 400 lbs |
| Baggage | 142.8 in | 200 lbs |
PA-28-161 Warrior II fuel capacity
This calculator uses 48 US gallons of usable fuel at an arm of 95 inches.
PA-28-161 Warrior II baggage limits
Baggage is limited to 200 lbs
Normal category limits
The CG envelope on this page is for the normal category.
About this Piper PA-28-161 Warrior II configuration
This page represents the normal-category Piper PA-28-161 Warrior II configuration identified in FAA Type Certificate Data Sheet 2A13, PA-28-161. The calculator uses a maximum takeoff weight of 2,325 lb and 48 US gal of usable fuel.
The reference datum for the loading arms on this page is See applicable Piper POH and weight and balance record.
Need help with the terminology? Read the aircraft weight and balance guide or the CG envelope guide.
Related aircraft
Piper PA-28R-180 Arrow, Piper PA-28RT-201 Arrow IV, Piper PA-28R-201 Arrow III, Piper PA-28-151 Cherokee Warrior, Piper PA-28-181 Archer III, Piper PA-28R-200 Arrow II, Piper PA-28-181 Archer II
Piper PA-28-161 Warrior II FAQ
What maximum takeoff weight does this Piper PA-28-161 Warrior II calculator use?
This calculator uses a maximum takeoff weight of 2,325 lb for the configuration identified on this page.
How much usable fuel is represented for the Piper PA-28-161 Warrior II?
This page uses up to 48 US gal of usable fuel at an arm of 95 in.
What baggage limit is represented for the Piper PA-28-161 Warrior II?
Baggage is limited to 200 lb on this page.
Source and applicability
Source: FAA Type Certificate Data Sheet 2A13, PA-28-161. Check the current POH or AFM, aircraft weight and balance record, equipment list and applicable supplements for the individual aircraft.
WBcalc is a planning aid. Check the current POH or AFM, aircraft weight and balance record, equipment list and applicable supplements before flight.
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