What was found
C4 CHECK. LT LEADING EDGE PANEL 511AL HAS FRETTING AT LOWER INBD END. REMOVED DAMAGE AS REQUIRED IAW SRM 51-14-00-02-04. REMAINING THICKNESS .206. NO CRACKS. WITHIN LIMITS. ALODINED AND PRIMED AREA. APPLIED TEFLON TAPE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C4 CHECK. LT LEADING EDGE PANEL 511AL HAS FRETTING AT LOWER INBD END. REMOVED DAMAGE AS REQUIRED IAW SRM 51-14-00-02-04. REMAINING THICKNESS .206. NO CRACKS. WITHIN LIMITS. ALODINED AND PRIMED AREA. APPLIED TEFLON TAPE.