As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND NICKS ON CENTER SECTION REAR SPAR UPPER FORWARD SIDE FITTING. REMOVED NICKS/DAMAGED MATERIAL TO A MAXIMUM OF .01 INCH AND TAPERED. APPLIED A CHEMICAL CONVERSION COATING AND REFINISHED THE REWORKED SURFACE IAW SRM 55-10-1 FIGURE 6, DETAIL IX. AIRCRAFT RETURNED TO SERVICE. (M)