14-10 LANDING GEAR / TROUBLESHOOTING
ICON A5 / MAINTENANCE MANUAL CHANGE C2
circumference of each joint. Any areas where the bonded flanges of the boot can be easily lifted
by hand should be corrected. (See “Re-Bond Main Landing Gear (MLG) Boot” on page 14-44.)
9. With the inspector viewing the main landing gear control system located behind the aft baggage
panel, actuate the landing gear and verify that nothing unusual occurs.
VERIFICATION METHOD:
Verify that each check is passed successfully.
RELATED INFORMATION:
"Condition and 100-Hour Inspection—Landing Gear" on page 3-14
"Removal and Installation of Inspection Panels and Fairings" on page 3-34
"Empty Weight and CG Measurement While on Jackpoint Scales" on page 3-32
"Re-Bond Main Landing Gear (MLG) Boot" on page 14-44
14.3.4 Landing Gear Indicator Lights
The following should be used to test and check the landing gear indicator lights.
TASK INFORMATION:
Type of Maintenance
Line
Level of Certification
LSA-RM
Task Specific Training Required
No
Special Tools Required
Wing Jack Point Adapter—ICA009750
Parts Required
None
Aircraft System and Number
11—Landing Gear
Consumables
None
This task can be readily combined with the Landing Gear Retraction and Extension Time task. (See
“Retraction and Extension Time” on page 14-12.)
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