What was found
INSPECTION FOUND A 6 INCH CRACK IN EXTERNAL FUSELAGE LOWER FILLET FAIRING T-FITTING AT FS 880. THE T-FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 6 INCH CRACK IN EXTERNAL FUSELAGE LOWER FILLET FAIRING T-FITTING AT FS 880. THE T-FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-5.