What was found
FUSELAGE SKIN HAS 2 ADJACENT DENTS, JUST AFT OF FRAME STA 23 AT STR 22L. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED PER SRM 53-21-11 FIG 215 AT SMB C CHECK WRITE-UP E3138F.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN HAS 2 ADJACENT DENTS, JUST AFT OF FRAME STA 23 AT STR 22L. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED PER SRM 53-21-11 FIG 215 AT SMB C CHECK WRITE-UP E3138F.