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Piper PA-28-181 Archer II Weight and Balance Calculator

Aircraft reference: Piper PA-28-181 Archer II production years, model information and certification

Use this calculator to check loaded weight and center of gravity for the Piper PA-28-181 Archer II. Enter the current empty weight and empty arm from the aircraft weight and balance record for the individual aircraft.

Maximum takeoff weight: 2,550 lbs. Maximum landing weight: 2,550 lbs. Usable fuel: 48 US gal.

Data source: Piper PA-28-181 Archer II Pilot's Operating Handbook, normal category. 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-28-181 Archer II specifications

SpecificationValue
Maximum takeoff weight2,550 lbs
Maximum landing weight2,550 lbs
Forward CG at 2,050 lbs or less82 in
Forward CG at 2,550 lbs88.6 in
Aft CG limit93 in
Usable fuel48 US gal
Fuel arm95 in

Source: Piper PA-28-181 Archer II Pilot's Operating Handbook, normal category.

Piper PA-28-181 Archer II CG limits

Aircraft weightForward CG limitAft CG limit
2,050 lbs82 in93 in
2,550 lbs88.6 in93 in

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

Piper PA-28-181 Archer II loading stations

StationArmLimit
Pilot and front passenger80.5 in
Rear passengers118.1 in
Baggage142.8 in200 lbs

PA-28-181 Archer II fuel capacity

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

PA-28-181 Archer 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-28-181 Archer II configuration

This page represents the normal-category Piper PA-28-181 Archer II configuration identified in Piper PA-28-181 Archer II Pilot's Operating Handbook, normal category. The calculator uses a maximum takeoff weight of 2,550 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-28-161 Warrior II

Piper PA-28-181 Archer II FAQ

What maximum takeoff weight does this Piper PA-28-181 Archer II calculator use?

This calculator uses a maximum takeoff weight of 2,550 lb for the configuration identified on this page.

How much usable fuel is represented for the Piper PA-28-181 Archer 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-28-181 Archer II?

Baggage is limited to 200 lb on this page.

Source and applicability

Source: Piper PA-28-181 Archer II Pilot's Operating Handbook, normal category. 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-28-181 Archer 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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