What was found
INSPECTION FOUND STRINGER GOUGED AT LT FUSELAGE STA 1213 ABOVE PANEL NR 3901. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, FIGURE 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND STRINGER GOUGED AT LT FUSELAGE STA 1213 ABOVE PANEL NR 3901. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, FIGURE 2.