What was found
INSPECTION FOUND A 2 INCH CRACK ON LT MLG WHEEL WELL AFT WEB VERTICAL STIFFENER. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 53-53-01, 51-21-01, AND 51-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK ON LT MLG WHEEL WELL AFT WEB VERTICAL STIFFENER. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 53-53-01, 51-21-01, AND 51-31-01.