What was found
UPON INSTALLATION OF CARGO DOOR SILL PLATE, FOUND ANGLE AT FS 589.00 TO BE CRACKED. REMOVED CRACKED ANGLE IAW SRM 51-42-21. INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPON INSTALLATION OF CARGO DOOR SILL PLATE, FOUND ANGLE AT FS 589.00 TO BE CRACKED. REMOVED CRACKED ANGLE IAW SRM 51-42-21. INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-21.