What was found
INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 515 TO 535, S28L. THE DENTED AREA WAS TRIMMED OUT AND REINFORCED WITH DOUBLER AND FINGER DOUBLER IAW SRM 53-20-00, FIGURE 6, 51-21-01, AND 51-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 515 TO 535, S28L. THE DENTED AREA WAS TRIMMED OUT AND REINFORCED WITH DOUBLER AND FINGER DOUBLER IAW SRM 53-20-00, FIGURE 6, 51-21-01, AND 51-31-01.