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Weight & Balance Cessna-182 N1732A

Max T/O Weight 3,100 (lbs.) Weight (lbs.) Arm (in.) Moment (lb-in)
Empty Weight   2037.1 39.45 80,363.60
Usable Fuel 87 gal. 0 46.6 0
Pilot   37 0
Co-Pilot   37 0
Mid Island Aviation:
Station 37 is used for caclulations assuming and average weight occupant as per the POH. Pilot or passenger center-of-gravity on adjustable seats positioned for average occupant. Numbers in parentheses indicate forward and aft limits of occupant center-of-gravity range.
Rear Passenger #1   74 0
Rear Passenger #2   74 0
Baggage Area 1 (97 lbs.max.)   97 0
Baggage Area 2 (116 lbs.max.)   116 0
Baggage Area 3 (129 lbs.max.)   129 0
Estimated Fuel Burned (gal.) Estimated Landing Fuel (gal.) 0
Total Ramp Weight (3110 max) 2037.1 80,363.60
Start, Taxi, Takeoff -10.2 46.6 -475.32
Take Off Weight (3,100 max) 2026.9 79,888.28
Useful Load Remaining 1073.1    
Take Off CG 39.41    
Landing CG 39.41    
Va (knots) 90.68    
Landing Weight (2950 max) 2026.9
Va Range (knots @lbs.) 110 3100 101 2600 91 2100    

      NOT ENOUGH FUEL!   

No Pilot or Fuel

Weight FWD Limit 33 AFT Limit 46 CG Location (Inches Aft of Datum) 1800 2100 2000 1900 2600 2700 2800 2900 3000 3100 2500 2400 2300 2200 2950 lbs Max Landing Weight 3100 lbs Max Take Off Weight

Calculate Weight First, Fill the Form Below and Submit

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You, as pilot in command, are solely responsible for assuring correct data and proper loading of your aircraft prior to flight.

The Mid Island Weight and Balance Program is intended for planning purposes only and should NOT be used as the sole determiner for a safe flight. All numbers should be verified using the planes POH, especially if the calculations approach the maximum limits for weight and CG. This calculator is intended to give you a quick estimate as to your weight and CG load being within each plane's limits. You, as pilot in command, are solely responsible for assuring correct data and proper loading of your aircraft prior to flight.

MID ISLAND MAKES NO GUARANTEE AS TO THIS CALCULATOR'S ACCURACY.

 

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