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Maintenance Manual XA41/XA42
AMM-XA42-0040-001 C.00
Page
14
Page date:
Chapter 05
25.09.2018
05-20-05 1000 Hour Inspection
Disassemble the aircraft and do a full inspection of all components.
Description
Action
Signature
Remove the wings
CHECK
Remove the ailerons
CHECK
Remove the elevator
CHECK
Remove the rudder
CHECK
Remove the stabilizer
CHECK
Do the NDI on all composite structure bond lines, for example
the tap test, refer to FAA AC43.13-1B section 8*
EXAMINE
Remove the tailwheel strut. Disassemble the tailwheel
CLEAN.
If
necessary
REPLACE
Disassemble the controls and the control rods
CLEAN
and
EXAMINE
05-20-06 Engine change
Install the engine, refer to 72-10-00 and Lycoming. AEIO-580-B1A Operation and Installation
Manual. P/N 60297-32, Section II.
Summary of Contents for XA41
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