What was found
CRACKED ANGLE ON LINING ACCESS PANEL 844AW ON THE AFT SERVICE DOOR. REPLACED THE ANGLE IAW SOPM-20-50-12, REV 58, & DWG-411A2114-43B, SHEET 26, REV C.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED ANGLE ON LINING ACCESS PANEL 844AW ON THE AFT SERVICE DOOR. REPLACED THE ANGLE IAW SOPM-20-50-12, REV 58, & DWG-411A2114-43B, SHEET 26, REV C.