As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT PIT LH Z ANGLE BETWEEN STA 767-787 CORROSION AROUND NUTPLATE HOLES / REMOVED AND EVALUATED CORROSION; ORIGINAL THICKNESS .040' LOSS OF .006' WITH .034' REMAINING. BLEEND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AND REPLACED Z-ANGLE SECTION STA 757 TO 847 LH AND ACCOMPLISHED REPAIR SPLICE AT STA 757 PER SRM 53-00-53-2R-5 AND DWG 146A7500 REV-