What was found
INSPECTION FOUND A 1 INCH CRACK IN RT WHEEL WELL ANGLE BELOW LOAD CONTROL VALVE. THE ANGLE WAS REMOVED, A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN RT WHEEL WELL ANGLE BELOW LOAD CONTROL VALVE. THE ANGLE WAS REMOVED, A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-4.