As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FWD CARGO DOOR CUT OUT UNDER MAIN SCUFF PLATE CORRODED @STA. 440+5 AND 440+15 MARKED / REMOVED AND EVALUATED CORROSION IN FWD CARGO DOOR WEB UNDER MAIN SCUFF PLATE STA 440+5 AND 440+15 ORIGINAL THICKNESS .045 MAT LOSS .001' MAT REMAINING .044' IN LIMITS IAW SRM 53-30-15-1A-1