Wing Skins Delaminate/Voids
100321-00
Use the following steps in conjunction with tap tests to inspect wing skins for voids.
Applicable Aircraft Serial Numbers
All
Type of Maintenance
Line
Level of Certification
LSA-RM
Task Specific Training Required
No
Special Tools Required
See Manual Tap Test
Parts Required
None
Aircraft System and Number
14—Wing
Safety Equipment
As Needed
Consumables
None
Figure 446. Internal Structural Layout of Wing
Task Instructions
1. Conduct a tap test on right hand wing skins in the vicinity of upper and lower bond lines for the main spar. (Manual Tap Test)
2. Conduct a tap test on right hand wing skins in the vicinity of upper and lower bond lines for the aft spar.
3. Conduct a tap test on right hand wing skins in the vicinity of upper and lower lines for all internal ribs.
4. Conduct a tap test on left hand wing skins in the vicinity of upper and lower bond lines for the main spar.
5. Conduct a tap test on left hand wing skins in the vicinity of upper and lower bond lines for the aft spar.
6. Conduct a tap test on left hand wing skins in the vicinity of upper and lower bond lines for all internal ribs.
Verification Method
Confirm results are within acceptable limits.
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