What was found
UPPER WING TO FUSELAGE FAIRING PANEL 261LT IS CHAFED ON MATING SURFACE. REMOVED FASTENERS AS REQUIRED IAW SRM 51-44-30-02-01, REV 12. REMOVED DAMAGE SRM 53-75-06-02-01 REV 12. CONFIRMED CRACK FREE IN AFFECTED AREA REF NTM 51-00-06-910-801, PT 1, REV 7. MECHANICALLY MEASURED MIN REMAINING THICKNESS IS 0.089". IN LIMITS IAW SRM 53-75-06-02-01 REV 12. ALODINED AND PRIMED IAW SRM 51-21-10-02-01 AND 51-25-10-02-01, REV 12. CAMLOC GRIP LENGTH GOOD, MIN POSSIBLE COMBINED THICKNESS .181" SRM 53-75-06-02-01, REV 12. INSTALLED FASTENERS IAW SRM REV 12 53-75-06-02-01.