As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C5 CHECK - FLOORBEAM 698.000 IS CORRODED ABOVE THE CTR SPLICE ON THE LT HALF. REMOVED CORROSION IAW SRM 51-21-00 ORIGINAL THICKNESS .063, REMAINING THICKNESS AFTER CORROSION REMOVAL .058". FLOORBEAM WITHIN LIMITS IAW SRM 51-14-00-02-03. ALODINED AND PRIMED IAW SRM 51-21-10-02-01 AND 51-25-10-02-01.