What was found
INSPECTION FOUND ANGLE CORRODED AT RT SIDE OF FUSELAGE, BS 251.6, BL 0. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND ANGLE CORRODED AT RT SIDE OF FUSELAGE, BS 251.6, BL 0. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-00.