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Maintenance Manual LS8-s and LS8-sb

5.2 Calculation of Loading Limits (continued)

2. Maximum approved Weight of Non-lifting Parts may vary, depending on

empty weight and empty weight C.G. position:

LS8-s:

LS8-sb:

In contrast to methods used up to now, maximum weight of non-lifting

parts can be determined in relation to empty weight and empty weight

C.G. position according to table in section 5.3. See also examples on end

of this section.

Maximum weight of Non-lifting Parts should be entered into weighing

report.

3. Determine Maximum approved Cockpit Load from table "Empty Weight

C.G. Position", section 5.4 in <kg/mm> or <in/lbs>. Maximum Cockpit

Load normally should be 110 kg <242 lbs>, as given in empty weight

C.G. table. It may be lower due to trim conditions, excessive equipment or

repairs.

Calculate Maximum Cockpit Load on weighing report, see also examples

at end of this section.

Resulting Maximum Cockpit Load should be entered in the following

places:

a. in weighing report of inspection

b. in Flight Manual, section 6.2

c. on Data Placard in cockpit

4. Empty Weight (perhaps increased by weight of permanently fitted trim

ballast) should be entered in the following places:

a. in weighing report of inspection

b. in Flight Manual section 6.2 for calculation of maximum

permissible water ballast weight

5. Battery position during weighing should be entered in the following

places:

a. in weighing report and equipment list of inspection

b. in section 6.2 of Flight Manual

For permanent installation of trim ballast weights, see Maintenance

Manual section 4.15.

Form for Weighing Report, see Maintenance Manual section 11.

Edition: June 2016

between 255 and 263 kg <562 to 580 lbs>

between 280 and 288 kg <617 to 635 lbs>

Rev. 6 TN 8024

Weight and Balance

5-4