What was found
T ANGLE ON FUSELAGE FORWARD END AT FILLET FAIRING SUPPORT ANGLE THAT ATTACHES TO UPPER WING TRAILING EDGE WORN. REMOVED AND REPLACED ANGLE PER SRM 51-10-2 AND 51-40-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
T ANGLE ON FUSELAGE FORWARD END AT FILLET FAIRING SUPPORT ANGLE THAT ATTACHES TO UPPER WING TRAILING EDGE WORN. REMOVED AND REPLACED ANGLE PER SRM 51-10-2 AND 51-40-00.