What was found
DURING D-CHECK, FUS EXTERIOR HOLE CORRODED IN FUS SKIN AT FS STR 30. CUT OUT DAMAGED AREA PER SRM 53-30-3 AND INSTALLED REPAIR .71 7075-T6 6 INCHES BY 8 INCHES. TOTAL CYCLES 29577.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING D-CHECK, FUS EXTERIOR HOLE CORRODED IN FUS SKIN AT FS STR 30. CUT OUT DAMAGED AREA PER SRM 53-30-3 AND INSTALLED REPAIR .71 7075-T6 6 INCHES BY 8 INCHES. TOTAL CYCLES 29577.