DG Flugzeugbau LS8-st 유지 관리 매뉴얼 - 페이지 9

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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

Edition: June 2016

Maintenance Manual LS8-st

Rev. 6 TN 8024

Weight and Balance

5-3