What was found
CRACK ON LT C12A STIFFENER FITTING, CRACK LENGTH 4MM. REPAIR PERFORMED BY INCORPORATION OF SB A300-53-6137, APPROVED BY EO 6-5340-7-5003.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON LT C12A STIFFENER FITTING, CRACK LENGTH 4MM. REPAIR PERFORMED BY INCORPORATION OF SB A300-53-6137, APPROVED BY EO 6-5340-7-5003.