What was found
RIGHT WING T/E CAVITY INTERIOR HAS CRACKED (APPROXIMATELY 1 INCH LONG) SUPPORT ANGLE FOR ACCESS PANEL NR 8611 (WS 383.5). REMOVED AND FABBED NEW SUPPORT ANGLE AND INSTALLED NEW ANGLE IAW SRM 51-10-01 AND SRM 51-20-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING T/E CAVITY INTERIOR HAS CRACKED (APPROXIMATELY 1 INCH LONG) SUPPORT ANGLE FOR ACCESS PANEL NR 8611 (WS 383.5). REMOVED AND FABBED NEW SUPPORT ANGLE AND INSTALLED NEW ANGLE IAW SRM 51-10-01 AND SRM 51-20-01.