What was found
INSPECTION FOUND A 1.5 INCH CRACK IN RT WHEEL WELL CEILING PRESSURE DECK ABOVE O/B END OF GROUND SPOILER CONTROL VALVE, STA 664, RBL 40. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-60-51 AND 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.5 INCH CRACK IN RT WHEEL WELL CEILING PRESSURE DECK ABOVE O/B END OF GROUND SPOILER CONTROL VALVE, STA 664, RBL 40. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-60-51 AND 51-40-02.