Piper Arrow PA-28-200R N33151
Weight and Balance Calculator

This calculator is presented for educational or amusement purposes only.
You, as pilot in command, are solely responsible for assuring proper loading of your aircraft prior to flight.

This page is a derivation of R. A. Booty's original javascript powered Weight & Balance calculator.

Form default data specific to PA-28-200R, N33151	Weight (lbs)	Arm (inches)	Moment (in-lb)
Basic Empty Weight (includes undrainable engine oil and hydrolic fluid)
Oil (8 Quarts)
Pilot and Front Passenger
Rear Passengers
Baggage (200lb.max.)
Moment due to Gear Retraction
I. Sub Total Zero Fuel Weight: (no fuel, gear down)
Center of Gravity:
Useable Fuel (max.50 gal. useable 48 gal. @ 6 lbs./gal)
II. Sub Total Ramp Condition: (includes fuel, gear down)
Center of Gravity:
Taxi Fuel Burn (Start, Taxi, Run Up, Take Off; normally 10 lbs.)
III. Departure Condition: (max 2650lbs, gear retracted)
Center of Gravity:
Fuel Burn To Destination (6 lbs. per gallon)
IV. Landing Condition:
Center of Gravity:

Calculated Gross Weight and C.G. point must lie within the normal category envelope limits per this specific aircraft's Airplane Flight Manual.
YOU MUST ENTER DATA SPECIFIC TO YOUR AIRPLANE.  DEFAULT DATA FOR N33151 WILL NOT WORK FOR YOUR PA-28-200R OR ANY OTHER AIRCRAFT.

I am working on a C.G. graph, if you know how to do it please contact me.

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Sean Cooksy
scooksy@yahoo.com

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