Maintenance Manual LS8-st
Weight and Balance
Edition: June 2016
Rev. 6 TN 8024
5-3
5.2 Calculation of Loading Limits
1.
Determine Minimum Cockpit Load for 15 m wingspan and full and empty
tail fin tank version following procedure given in section 5.1 from table
“Empty Weight C.G. Position”, section 5.4 in <kg/mm> or <in/lbs>.
Minimum Cockpit Load for
tail fin battery (3BR-199) removed
(and
installed in baggage compartment, when required) decreases
by 10 kg
<22 lbs>
.
Finally resulting 4 different cockpit loads should be entered in the
following places:
a. in weighing report of inspection
b. in Flight Manual section 6.2
c. in cockpit placard under instrument panel cover
d. in cockpit on data placard
1. Minimum Cockpit Load for full tail fin tank with tail fin battery
2. Minimum Cockpit Load for empty tail fin tank with tail fin battery
3. Minimum Cockpit Load for full tail fin tank without tail fin battery
4. Minimum Cockpit Load for empty tail fin tank without tail fin battery