What was found
UPPER WING TO FUSELAGE FAIRING PANEL 261HT IS CHAFED ON MATING SURFACE. REMOVED FASTENERS AS REQUIRED IAW SRM 51-44-30-02-01, REV 12. REMOVED DAMAGE IAW SRM 53-75-06-02-01 REV 12. MECHANICALLY MEASURED, MIN REMAINING THICKNESS IS 0.099". DAMAGE IS IN LIMITS IAW SRM 53-75-06-02-01, REV 12. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801, PT 1, REV 7. ALODINED AND PRIMED IAW SRM 51-21-10-02-01 AND 51-25-10-02-01, REV 12. CAMLOC GRIP GOOD, MIN POSSIBLE COMBINED THICKNESS .191 SRM 53-75-06-02-01, REV 12. INSTALLED FASTENERS IAW SRM REV 12 53-75-06-02-01.