Piper PA-28R-180 Arrow Weight and Balance Calculator
This page represents the FAA TCDS 2A13 PA-28R-180 normal-category configuration. Enter the current basic empty weight and arm from the certified weight and balance record for the individual aircraft.
Maximum weight: 2,500 lbs. Usable fuel: 48 US gal. Fuel arm: 95 in.
Data source: FAA Type Certificate Data Sheet 2A13 and applicable Piper POH/AFM. 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-28R-180 Arrow specifications
| Specification | Value |
|---|---|
| Maximum takeoff weight | 2,500 lbs |
| Maximum landing weight | 2,500 lbs |
| Forward CG at 1,925 lbs or less | 81 in |
| Forward CG at 2,500 lbs | 91 in |
| Aft CG limit | 95.9 in |
| Usable fuel | 48 US gal |
| Fuel arm | 95 in |
Source: FAA Type Certificate Data Sheet 2A13 and applicable Piper POH/AFM.
Piper PA-28R-180 Arrow CG limits
| Aircraft weight | Forward CG limit | Aft CG limit |
|---|---|---|
| 1,925 lbs | 81 in | 95.9 in |
| 2,500 lbs | 91 in | 95.9 in |
The calculator uses the published CG envelope points and linear interpolation between forward-limit breakpoints where applicable.
Piper PA-28R-180 Arrow loading stations
| Station | Arm | Limit |
|---|---|---|
| Pilot and front passenger | 85.5 in | |
| Rear passengers | 118.1 in | |
| Baggage | 142.8 in | 200 lbs |
PA-28R-180 Arrow fuel capacity
This calculator uses 48 US gallons of usable fuel at an arm of 95 inches.
PA-28R-180 Arrow 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-28R-180 Arrow configuration
This page represents the normal-category Piper PA-28R-180 Arrow configuration identified in FAA Type Certificate Data Sheet 2A13 and applicable Piper POH/AFM. The calculator uses a maximum takeoff weight of 2,500 lb and 48 US gal of usable fuel.
The reference datum for the loading arms on this page is Piper PA-28 datum; see applicable POH/AFM.
Need help with the terminology? Read the aircraft weight and balance guide or the CG envelope guide.
Related aircraft
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
Piper PA-28R-180 Arrow FAQ
What maximum takeoff weight does this Piper PA-28R-180 Arrow calculator use?
This calculator uses a maximum takeoff weight of 2,500 lb for the configuration identified on this page.
How much usable fuel is represented for the Piper PA-28R-180 Arrow?
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-28R-180 Arrow?
Baggage is limited to 200 lb on this page.
Source and applicability
Source: FAA Type Certificate Data Sheet 2A13 and applicable Piper POH/AFM. 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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