As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON UPPER CENTER TANK SKIN AT PULLEY SUPPORT ANGLE AT STA. 745 LBL 25-34. BLENDED AND REMOVED ALL CORROSION REF B717 SRM 57-10-01-1A. UT THICKNESS INSPECTED AND MAPPED ON 1/2" GRID PER NDTSPM PART 04-00-00 TO 04-00-09. ORIGINAL THICKNESS IS .252. LOWEST BLENDED AREA MEASURES .190. FOUND TO BE OUT OF LIMITS PER B717 SRM 57-10-01-1A. REPAIRED PER ERA 592454-14 REV. ORIG. (LP #1863538)