XtremeAIR XA41, Руководство по обслуживанию

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Maintenance Manual XA41/XA42
AMM-XA42-0040-001 C.00
Page date: Page 13
25.09.2018 Chapter 05
05-20-04 100 Hour Inspection
Do all steps of the 50h inspection plus these steps:
Description Action Signature
Electrical system
Alternator maintenance iaw ICA-BC410 or ICA-BC462-H. PERFORM
Regulator maintenance iaw ICA-LR3C PERFORM
Fuel selector switch
The aft universal joint and the mounting bracket are correctly
installed CHECK
The mounting bracket is correctly installed CHECK
The fuel selector valve is correctly installed CHECK
The fuel hoses are correctly connected to the fuel selector
valve CHECK
The bushing is correctly installed in the carry-through bridge
of the spar CHECK
The front universal joint and the mounting bracket are
correctly installed CHECK
Structure
The firewall and the adjacent structure are not damaged and
have no cracks CHECK
Visual inspection: The composite structure is not damaged
and has no cracks CHECK
The torque of the fuselage longeron connection bolt is 42 Nm
(31 ft.lbs.) CHECK
The control surface deflections are correct, refer to the form
(Appendix 7) CHECK
If
necessary
ADJUST
The maximum permitted play in a control bearing is 0.6 (mm). If the value
is higher, replace the bearing.
The condition of the magneto is satisfactory and its timing is
correct CHECK
For the step above, refer to
“Lycoming Maintenance and Overhaul Manual
LMO-AEIO-580
”
NOTE
NOTE