Cessna Stationair N206FN

N206FN Weight and Balance Computations
Based on N206FN Owner's Manual
Information as of September 20, 2016

Weight and Balance Weight (lbs) CG Arm (inches) Moment (lb*ins/1000)
Basic Empty Weight (including unusable fuel and full oil) 2258 40.54 91.543
Usable fuel: Max 88 gal (64 to tabs):. . . . . . . . . . . . . .
Pilot and front passenger (station 37 in)
Center passengers (station 70 in)
Rear passengers (station 100 in)
Baggage area-aft (max 180 lbs) (station 127.0 in)
RAMP WEIGHT AND MOMENT
Fuel allowance for engine start, taxi, and run-up -15.6 46.6 -0.726
TAKEOFF WEIGHT AND MOMENT (max 3600 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