What was found
CRACK ON ANGLE OF PAX DOOR AFT SIDE PANEL. SECTIONAL REPAIR INSTALLED OF ANGLE WAS PERFORMED IAW SRM 52-11-04, FIGURE 52-11-04-991-814, SHEET 1-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON ANGLE OF PAX DOOR AFT SIDE PANEL. SECTIONAL REPAIR INSTALLED OF ANGLE WAS PERFORMED IAW SRM 52-11-04, FIGURE 52-11-04-991-814, SHEET 1-2.