What was found
DURING ROUTINE INSPECTION UPPER FUSELAGE SKIN FOUND CORRODED AND POPPED RIVETS FROM BS 430 - 440 AT STR 5L. REMOVED RIVET AND TRIMMED OUT DAMAGED AREA IAW SRM 53-30-3. FAB REPAIR PARTS PER IAW SRM 53-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE INSPECTION UPPER FUSELAGE SKIN FOUND CORRODED AND POPPED RIVETS FROM BS 430 - 440 AT STR 5L. REMOVED RIVET AND TRIMMED OUT DAMAGED AREA IAW SRM 53-30-3. FAB REPAIR PARTS PER IAW SRM 53-30-3.