WEIGHT AND
BALANCE
AIRPLANE
OPERATIONS
MANUAL
1-06-50
Page
2
Code
01
SEPTEMBER 20, 1999
6. Enter the Fuel Index table with the fuel weight and read the fuel
index.
7. Enter the Fuel box with the fuel weight and index and draw the CG
shift from the last position determined in step 3.
8. From the position determined in step 7, draw a vertical line into the
CG envelope until it crosses a horizontal line at the TOW. The
crossing point determines the TOW-CG, and if it is located outside
of the TOW envelope, a new loading distribution must be made.
9. Enter the Stab Trim table with the TOW-CG and read the stab trim
setting (pitch trim).
10.Complete the flight identification box with Flight Number, Date,
Origin airport, Destination airport, Aircraft Registration and Crew
Configuration.
11.Complete the results box with the ZFW, ZFW-CG, TOW, TOW-CG
and Stab Trim setting and sign the load sheet in the Prepared By
box.
To Next Page
Loading...
