What was found
PRESSURE PANEL DOUBLER WAS BULGING LEFT BUTT LINE 8 TO LEFT BUTT LINE 16, FS 756. REPLACED LOWER T-ANGLE OF FLOORBEAM FS 756, BUTT LINE 56 RIGHT TO BUTT LINE 54 IAW DC-9 SRM 51-30-2, 51-30-5 AND REA D953-48132.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PRESSURE PANEL DOUBLER WAS BULGING LEFT BUTT LINE 8 TO LEFT BUTT LINE 16, FS 756. REPLACED LOWER T-ANGLE OF FLOORBEAM FS 756, BUTT LINE 56 RIGHT TO BUTT LINE 54 IAW DC-9 SRM 51-30-2, 51-30-5 AND REA D953-48132.