Refer to figures. 
Step 1:

• From the load sheet we can find the take-off fuel mass as 11 520 kg.
• From the load sheet we can also find the trip fuel mass as 8810 kg.
• 11 520 kg - 8810 kg = 2710 kg fuel on board at landing
• Using the fuel index table: there is no index for 2710 kg, so the next highest mass is used, which is 3000 kg. This equates to an index of -4.3

Step 2:

Using the trim sheet:

• The red line, filled in by the examiner, ends at the rear passenger section.
• Continue the line (in green in the attachment) vertically into the fuel index row.
• Plot -4.3 units to the left to include the landing fuel index.
• Drop the line vertically into the trim envelope.

Step 3:

• From the load sheet we can find the landing mass as 47 770 kg.
• Draw a line (in blue in the attachment) horizontally across the trim envelope from this mass on the left hand side scale.
• Where the two lines cross = Landing CG.
• The Landing CG can be read from the fan lines and is between the 21% and 22% fans at 21.6% MAC.