What was found
TUL - FUSELAGE SKIN HAD DENTED AREA STA 229 TO STA 239, LONGERON 18L TO LONGERON 17L (ADL DOT IN AREA). INSTALLED DOUBLER PER SRM 53-04 FIG 38 SHEETS 21, 36, 37, 38. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TUL - FUSELAGE SKIN HAD DENTED AREA STA 229 TO STA 239, LONGERON 18L TO LONGERON 17L (ADL DOT IN AREA). INSTALLED DOUBLER PER SRM 53-04 FIG 38 SHEETS 21, 36, 37, 38. (X)