What was found
DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 69 PRESSURE PANEL TO WHEEL WELL WEB ATTACH FITTING, RIGHT SIDE. REPLACED FITTING PER SRM 51-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 69 PRESSURE PANEL TO WHEEL WELL WEB ATTACH FITTING, RIGHT SIDE. REPLACED FITTING PER SRM 51-01.