What was found
S2 CHECK, CRACK ON FUSELAGE FRAME AT FRAME 68, STRINGER 23L. REPAIRED FUSELAGE FRAME AT FRAME 68, STRINGER 23L IAW SRM 53-41-12-201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
S2 CHECK, CRACK ON FUSELAGE FRAME AT FRAME 68, STRINGER 23L. REPAIRED FUSELAGE FRAME AT FRAME 68, STRINGER 23L IAW SRM 53-41-12-201.