What was found
AFTER BLEND OUT OF HEAVY CORROSION ON FOLLOWING PART AT 69 BULK CARGO DOOR CUT OUT, REMAINING THICKNESS IS UP TO 50 PERCENT. REPAIR PERFORMED BY REPLACEMENT OFF MENTIONED PART IAW SRM 51-72-10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER BLEND OUT OF HEAVY CORROSION ON FOLLOWING PART AT 69 BULK CARGO DOOR CUT OUT, REMAINING THICKNESS IS UP TO 50 PERCENT. REPAIR PERFORMED BY REPLACEMENT OFF MENTIONED PART IAW SRM 51-72-10.