As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AT C-CHECK, WING TO FUSELAGE FAIRING HOUSING REINFORCING STRIP CRACKED 1/2 INCH AT XWG 69.500 CLOSE TO FS 970.00. REMOVED DAMAGE AREA AND PERFORMED ANTI-CORROSIVE TREATMENT IAW SRM 51-1-8 PAGE 11. FABRICATED DOUBLER PLATE IAW SRM 53-2-0 PAGE 2E-2F. PRIMED PER SRM 51-1-8 PAGE 12. INSTALLED DOUBLER WITH SOLID RIVETS IAW SRM 51-1-21 PG 6.