What was found
DURING INSPECTION, FOUND CORROSION ON EXTERNAL FUSELAGE SKIN FRAME 69+12 AND STRINGERS 29 - 30R. REPAIRED IAW SRM 53-41-11, PARA 5.D, FIGURE 205, PAGES 255 TO 260.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, FOUND CORROSION ON EXTERNAL FUSELAGE SKIN FRAME 69+12 AND STRINGERS 29 - 30R. REPAIRED IAW SRM 53-41-11, PARA 5.D, FIGURE 205, PAGES 255 TO 260.