What was found
INSPECTION FOUND A 2 INCH CRACK IN RT WHEEL WELL ANGLE FORWARD OF APU LOAD CONTROL VALVE DUCT AT KEEL BEAM. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-1 AND 51-10-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN RT WHEEL WELL ANGLE FORWARD OF APU LOAD CONTROL VALVE DUCT AT KEEL BEAM. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-1 AND 51-10-2.