As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON MATING SURFACE OF PANEL 541BB. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL II. ORIGINAL THICKNESS .032 INCHES, 7075-T6 IAW DRW NR ARC0267. MATERIAL THICKNESS AFTER BLEND OUT .020 INCHES, PART OUT OF LIMITS IAW DC10 SRM 57- 00-01 VOL I. RECIEVED NEW PANEL P/N ARC0267-503 IAW DAC DWG. DRW NR ARC0267. LOCATED, DRILL AND COUNTERSUNK FASTENER HOLES IAW SRM 51-31-01 VOL II. REF N/R N00123.