What was found
CRACK ANGLE OF ACCESS PANEL 333AT ON THE LT HORIZONTAL STAB. REPLACED THE ACCESS PANEL IAW SRM-51-40-02-0G-0, & SRM-51-10-02-0G-0, ITEM 9.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ANGLE OF ACCESS PANEL 333AT ON THE LT HORIZONTAL STAB. REPLACED THE ACCESS PANEL IAW SRM-51-40-02-0G-0, & SRM-51-10-02-0G-0, ITEM 9.