What was found
SYS 6, FUSELAGE FRAME 68, CORRODED AT STRINGER 23R. REPAIRED FRAME IAW SRM 53-41-14-201 PRINCIPLE 5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SYS 6, FUSELAGE FRAME 68, CORRODED AT STRINGER 23R. REPAIRED FRAME IAW SRM 53-41-14-201 PRINCIPLE 5.