What was found
INSPECTION FOUND A .5 INCH CRACK IN EXTERNAL FUSELAGE LOWER SURFACE WING TO BODY FAIRING SUPPORT TEE AT FS 916. THE SUPPORT WAS REMOVED AND A REPLACEMENT SUPPORT ANGLE WAS INSTALLED 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 .5 INCH CRACK IN EXTERNAL FUSELAGE LOWER SURFACE WING TO BODY FAIRING SUPPORT TEE AT FS 916. THE SUPPORT WAS REMOVED AND A REPLACEMENT SUPPORT ANGLE WAS INSTALLED IAW SRM 51-30-5.