14-44 LANDING GEAR / MAIN LANDING GEAR
ICON A5 / MAINTENANCE MANUAL CHANGE C2
until the verification checks are complete. Allow the boot cuff and boot flange joints to fully cure
(24 hours) before conducting the verification checks.
VERIFICATION METHOD:
Retract and extend the landing gear to verify system function. Repeat until 10 up/down cycles have
been completed, with a 30 second dwell between each up or down actuation. The verification check
shall be considered complete only if the system actuates without fuse failure. If fuse failure occurs,
contact ICON Owner Support for further instructions.
RELATED INFORMATION:
"Re-Bond Main Landing Gear (MLG) Boot" on page 14-44
"Main Landing Gear (MLG) Wheel and Axle Installation" on page 14-48
"Main Landing Gear (MLG) Removal" on page 14-37
"Main Landing Gear (MLG) Installation" on page 14-38
14.6.1.5 Re-Bond Main Landing Gear (MLG) Boot
Perform this procedure if there are any areas where the MLG boot has become disbonded, delami-
nated, or is lifting from the MLG leg or Seawings™.
TASK INFORMATION:
Type of Maintenance
Line
Level of Certification
LSA-RM
Task Specific Training Required
No
Special Tools Required
None
Parts Required
None
Aircraft System and Number
11—Landing Gear
Consumables
Sil-Poxy
®
1. Inspect the boot for any damage such as holes, tears, or excessively worn spots. If damage is
unacceptable, replace the boot using the MLG Boot Replacement Procedure. (See “Main
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