What was found
FUSELAGE SKIN HAS A CRACK INDICATION .250 INCHES IN LENGTH 1 RIVET ABOVE STRINGER 6L AT FRAME 77. -C/A-REPAIRED FUSELAGE SKIN AT FRAME 77 IAW SRM 53-32-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN HAS A CRACK INDICATION .250 INCHES IN LENGTH 1 RIVET ABOVE STRINGER 6L AT FRAME 77. -C/A-REPAIRED FUSELAGE SKIN AT FRAME 77 IAW SRM 53-32-01.