What was found
LEFT STABLIZER I/B LEADING EDGE PANEL IS CREASED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED PLATE AND FILLER IAW SRM 55-10-01 FIGURE 201 REPAIR 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT STABLIZER I/B LEADING EDGE PANEL IS CREASED. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED PLATE AND FILLER IAW SRM 55-10-01 FIGURE 201 REPAIR 2.