What was found
INSPECTION FOUND A 2 CRACK ON VERTICAL STIFFENER IN AFT WEB OF LEFT MLG WHEEL WELL. THE STIFFENER WAS REMOVED. A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 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 CRACK ON VERTICAL STIFFENER IN AFT WEB OF LEFT MLG WHEEL WELL. THE STIFFENER WAS REMOVED. A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 51-31-01.