ICON A5 - Page 783

WING FOLD MECHANISM / WING FOLD MECHANISM GENERAL MAINTENANCE 18-13
CHANGE C0 ICON A5 / MAINTENANCE MANUAL
CHAPTER 18
Line
Level of Certification
LSA-RM
Task Specific Training Required
No
Special Tools Required
None
Parts Required
None
Aircraft System and Number
15—Wing Fold Mechanism
Consumables
None
FIGURE 18-5
INTERIOR WING ACCESS PANEL
TASK INSTRUCTIONS:
1. Test the socket assembly in the wing by carefully rotating the wing tip to ensure proper engage-
ment and retention of the pin.
CAUTION: Be sure to support the wing in case of failure. The wing should
move slightly but should not contact the Seawing.
2. Looking at the wing fold mechanism, ensure that all circlips and visible attachment points are fully
secured. Evaluate the U-point pins and circlips.
3. With the wing fold mechanism exposed, actuate the wing fold handle to validate that there is full
positive detent at the end of the handle rotation while also exhibiting smooth motion throughout
the range. With the handle unlatched, check for excessive freeplay of the handle.