What was found
RT AFT FUSELAGE SKIN CRACKED 11 INCHES AFT OF FAIRING AND 11 INCHES ABOVE LAP JOINT. FABRICATED AND INSTALLED REPAIR PER SRM 53-00-01 FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT AFT FUSELAGE SKIN CRACKED 11 INCHES AFT OF FAIRING AND 11 INCHES ABOVE LAP JOINT. FABRICATED AND INSTALLED REPAIR PER SRM 53-00-01 FIG 201.