What was found
DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS IN BOTH FS 69 PRESSURE PANEL TO WHEEL WELL WEB ATTACH FITTINGS. REPLACED FITTINGS 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 CRACKS IN BOTH FS 69 PRESSURE PANEL TO WHEEL WELL WEB ATTACH FITTINGS. REPLACED FITTINGS PER SRM 51-01.