What was found
FUSELAGE STRUCTURE INTERNAL WEB CRACKED AT STA 208 LONG 11L. TRIM OUT DAMAGED AREA AND INSTALLED TYPICAL WEB REPAIR PER SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE STRUCTURE INTERNAL WEB CRACKED AT STA 208 LONG 11L. TRIM OUT DAMAGED AREA AND INSTALLED TYPICAL WEB REPAIR PER SRM 51-40-02.