Beechcraft Baron G58 Pilot Operating Handbook page 294

Section 6
Wt and Bal/Equip List
6. Copy the fuel load weight only from Line 11. to Line 15.
7. Off to the side, add the calculated fuel to destination to
the Start, Taxi and Run-Up fuel. Record the total weight
only on line 16.
8. Subtract the Line 16. weight from the Line 15 weight and
record the results on Line 17. Obtain the corresponding
moment/100 from the Usable Fuel Table. Interpolation
may be necessary.
9. Copy the Zero Fuel Weight from Line 10. to Line 18.
and the fuel remaining from Line 17. to Line 19. Add the
Line 19. weight and moment/100 to the Line 18. values
to determine the Landing Weight on Line 20. Calculate
the arm.
10. Refer to the Moment Limits vs. Weight Table or the
Weight and Balance Diagram and ensure that the Zero
Fuel Weight, Take-Off Weight and Landing Weight
are all within the Weight and Center of Gravity or
Moment/100 Limits. If not, rearrange or remove Useful
Load Item(s) to stay within the limits.
6-16
Model G58
December, 2009