What was found
CRACKED SUPPORT ANGLE OF ACCESS PANEL 433BT AT LH INTERNAL PYLON STRUCTURE. SUPPORT ANGLE OF ACCESS PANEL 433BT AT LH INTERNAL PYLON STRUCTURE WAS REPLACED PER SRM 51-42-06-001-001-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED SUPPORT ANGLE OF ACCESS PANEL 433BT AT LH INTERNAL PYLON STRUCTURE. SUPPORT ANGLE OF ACCESS PANEL 433BT AT LH INTERNAL PYLON STRUCTURE WAS REPLACED PER SRM 51-42-06-001-001-A01.