What was found
UPPER WING TO FUSELAGE FAIRING PANEL 262HT IS CHAFED ON MATING SURFACE. REMOVED FASTENERS AS REQUIRED IAW SRM 51-44-30-02-01, REV 12. REMOVED DAMAGE IAW SRM 51-14-00-02-03, REV 12. MECHANICALLY MEASURED, MIN REMAINING THICKNESS IS 0.088" IN LIMITS IAW SRM 53-75-06-02-01. CONFRMED 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. INSTALLED FASTENERS SRM 51-44-30-02-01, REV 12. VERIFIED SATISFACTORY GRIP LENGTH IAW SRM 53-75-06-02-01, REV 12.