What was found
DURING NON ROUTINE CHECK, FWD FUSELAGE LWR SKIN BENT FROM Y-330 TO 22.50 INCHES RT OF CENTER AT FR 1 MARKED IN RED. TRIMMED OUT DAMAGED AREA 3" BY 12". FABRICATED AND INSTALLED.09 0" 2024-T3 DOUBLER PER SRM 53-11-11 FIG 221.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING NON ROUTINE CHECK, FWD FUSELAGE LWR SKIN BENT FROM Y-330 TO 22.50 INCHES RT OF CENTER AT FR 1 MARKED IN RED. TRIMMED OUT DAMAGED AREA 3" BY 12". FABRICATED AND INSTALLED.09 0" 2024-T3 DOUBLER PER SRM 53-11-11 FIG 221.