Piper PA-28R-200 Arrow II Weight and Balance Calculator

Aircraft reference: Piper PA-28R-200 Arrow II production years, model information and certification

This page represents the FAA TCDS 2A13 PA-28R-200 normal-category configuration. Enter the current basic empty weight and arm from the certified weight and balance record for the individual aircraft.

Maximum weight: 2,650 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-200 Arrow II specifications

Specification	Value
Maximum takeoff weight	2,650 lbs
Maximum landing weight	2,650 lbs
Forward CG at 1,800 lbs or less	80 in
Forward CG at 2,300 lbs	82 in
Forward CG at 2,650 lbs	87.3 in
Aft CG limit	93 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-200 Arrow II CG limits

Aircraft weight	Forward CG limit	Aft CG limit
1,800 lbs	80 in	93 in
2,300 lbs	82 in	93 in
2,650 lbs	87.3 in	93 in

The calculator uses the published CG envelope points and linear interpolation between forward-limit breakpoints where applicable.

Piper PA-28R-200 Arrow II loading stations

Station	Arm	Limit
Pilot and front passenger	80.5 in
Rear passengers	118.1 in
Baggage	142.8 in	200 lbs

PA-28R-200 Arrow II fuel capacity

This calculator uses 48 US gallons of usable fuel at an arm of 95 inches.

PA-28R-200 Arrow 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-28R-200 Arrow II configuration

This page represents the normal-category Piper PA-28R-200 Arrow II configuration identified in FAA Type Certificate Data Sheet 2A13 and applicable Piper POH/AFM. The calculator uses a maximum takeoff weight of 2,650 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-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-28-181 Archer II, Piper PA-28-161 Warrior II

Piper PA-28R-200 Arrow II FAQ

What maximum takeoff weight does this Piper PA-28R-200 Arrow II calculator use?

This calculator uses a maximum takeoff weight of 2,650 lb for the configuration identified on this page.

How much usable fuel is represented for the Piper PA-28R-200 Arrow 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-28R-200 Arrow II?

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.

Need model context? View the Piper PA-28R-200 Arrow II Aircraft Reference page for production years, family information and certification details.

Weight and balance guides: Weight and balance · Center of gravity · CG envelope · Moment · Basic empty weight · Fuel weight

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