Cessna 182 N3537C

N3537C Weight and Balance Computations
Based on N3537C Owner's Manual
Information as of May 5, 2007

Weight and Balance Weight (lbs) CG Arm (inches) Moment (lb*ins/1000)
Basic Empty Weight (including unusable fuel and full oil) 1968.48 37.18 73.20604
Usable fuel: Max 87 gal (64 to tabs):. . . . . . . . . . . . . .
Pilot and front passenger (station 37 in)
Rear passengers (station 74 in)
Baggage area 1 (max 120 lbs) (station 97 in)
Baggage area 2 (max 80 lbs) (station 116.0 in)
RAMP WEIGHT AND MOMENT
Fuel allowance for engine start, taxi, and run-up -10.0 46.5 -0.50
TAKEOFF WEIGHT AND MOMENT (max 3100 lbs)
Center of Gravity Moment Envelope Min. CG
Max. CG
Start by entering the number of gallons of fuel. Then tab through the fields entering the weight for each remaining item.  The arms will automatically be entered and the individual moments computed. The totals and C.G. will be calculated and analyzed for out-of-range conditions.

The PIC is responsible for performing Weight & Balance
using current Aircraft and POH information, as well as proper loading of the aircraft.
This reference tool is not warranted by the author or Flying Neutrons LLC