Specifications

SECTION VII
FLIGHT PLANNING AND PERFORMANCE
MODEL 560
10. Subtract the fuel and moment used for taxi. A standard 200-pound burnoff is assumed. The
moment for the taxi fuel is determined by the difference in moments of the fuel loaded and the
fuel remaining on board after taxi. Check takeoff weight and moment for approved limits.
NOTE
To check approved limits, divide moment by weight and multiply by 100 and obtain
center-of-gravity. Locate the weight versus center-of-gravity point on the
Center-of-Gravity Limits Envelope Graph (refer to Figure 7-5). Approved points are
points located inside the shaded area.
11. Determine the estimated weight of the fuel to be used to arrive at the destination. The
moment is determined by the difference in moments of the fuel remaining after taxi and the
fuel remaining after reaching destination. Enter the weight of the fuel burned and the
moment in the Weight and Balance Computation Form.
I 7-6 Configuration AA 56OMB-01