Arrow N8FN

N8FN Weight and Balance Computations
Based on N8FN Owner's Manual
Information as of May 6, 2010

Weight and Balance Weight (lbs) CG Arm (inches) Moment (lb*ins/1000)
Basic Empty Weight (including unusable fuel and full oil) 1784.0 84.99 151.61760
Usable fuel: Max 72 gal: . . . . . . . . . . . . . . . . . . . .
Pilot and front passenger (station 80.5 in)
Rear passengers (station 118.1 in)
Baggage area 1 (max 200 lbs) (station 142.8 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 2750 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