Piper PA-28RT-201 Arrow IV Weight and Balance Calculator
This page represents the FAA TCDS 2A13 PA-28RT-201 Arrow IV normal-category configuration. Enter the current basic empty weight and arm from the certified weight and balance record for the individual aircraft.
Maximum weight: 2,750 lbs. Usable fuel: 72 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-28RT-201 Arrow IV specifications
| Specification | Value |
|---|---|
| Maximum takeoff weight | 2,750 lbs |
| Maximum landing weight | 2,750 lbs |
| Forward CG at 2,400 lbs or less | 85.5 in |
| Forward CG at 2,750 lbs | 90 in |
| Aft CG limit | 93 in |
| Usable fuel | 72 US gal |
| Fuel arm | 95 in |
Source: FAA Type Certificate Data Sheet 2A13 and applicable Piper POH/AFM.
Piper PA-28RT-201 Arrow IV CG limits
| Aircraft weight | Forward CG limit | Aft CG limit |
|---|---|---|
| 2,400 lbs | 85.5 in | 93 in |
| 2,750 lbs | 90 in | 93 in |
The calculator uses the published CG envelope points and linear interpolation between forward-limit breakpoints where applicable.
Piper PA-28RT-201 Arrow IV loading stations
| Station | Arm | Limit |
|---|---|---|
| Pilot and front passenger | 80.5 in | |
| Rear passengers | 118.1 in | |
| Baggage | 142.8 in | 200 lbs |
PA-28RT-201 Arrow IV fuel capacity
This calculator uses 72 US gallons of usable fuel at an arm of 95 inches.
PA-28RT-201 Arrow IV 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-28RT-201 Arrow IV configuration
This page represents the normal-category Piper PA-28RT-201 Arrow IV configuration identified in FAA Type Certificate Data Sheet 2A13 and applicable Piper POH/AFM. The calculator uses a maximum takeoff weight of 2,750 lb and 72 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-28R-180 Arrow, 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-28RT-201 Arrow IV FAQ
What maximum takeoff weight does this Piper PA-28RT-201 Arrow IV calculator use?
This calculator uses a maximum takeoff weight of 2,750 lb for the configuration identified on this page.
How much usable fuel is represented for the Piper PA-28RT-201 Arrow IV?
This page uses up to 72 US gal of usable fuel at an arm of 95 in.
What baggage limit is represented for the Piper PA-28RT-201 Arrow IV?
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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