What was found
FUSELAGE SKIN HAS A CRACK INDICATION .125 INCHES IN LENGTH 1 RIVET BELOW STRINGER 6L AT FRAME 77 -C/A-EVALUATED WITH HFEC FOUND NO CRACK. RESTORED SURFACE PROTECTION IAW CPM 51-25-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN HAS A CRACK INDICATION .125 INCHES IN LENGTH 1 RIVET BELOW STRINGER 6L AT FRAME 77 -C/A-EVALUATED WITH HFEC FOUND NO CRACK. RESTORED SURFACE PROTECTION IAW CPM 51-25-01.