What was found
AFT FUSELAGE FAIRING, INTERNAL SUPPORT WEB STRUCTURE SPLICE AT BL0, FS 939 IS CORRODED. R & R WITH NEW ANGLE IAW SRM 51-42-06.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT FUSELAGE FAIRING, INTERNAL SUPPORT WEB STRUCTURE SPLICE AT BL0, FS 939 IS CORRODED. R & R WITH NEW ANGLE IAW SRM 51-42-06.