What was found
CRACKED ANGLE ON LINING ACCESS PANEL 831AW. REPLACED THE ANGLE IAW SOPM 20-50-12, REV 58, AND DWG 411A2111, SHEET 35, REV B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED ANGLE ON LINING ACCESS PANEL 831AW. REPLACED THE ANGLE IAW SOPM 20-50-12, REV 58, AND DWG 411A2111, SHEET 35, REV B.