Cessna Stationair N206FN

N3FN Weight and Balance Computations
Based on N3FN 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) 1958.63 78.61 153.967904
Usable fuel: Max 84 gal: . . . . . . . . . . . . . . . . . . . .
Pilot and front passenger (station 85.5 in)
Center passengers (station 118.1 in)
Rear passengers (station 155.7 in)
Baggage area-forward (max 100 lbs) (station 42.0 in)
Baggage area-aft (max 100 lbs) (station 178.7 in)
RAMP WEIGHT AND MOMENT
Fuel allowance for engine start, taxi, and run-up -6.0 95.0 -0.570
TAKEOFF WEIGHT AND MOMENT (max 3400 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