What was found
SY6 CHECK, FUSELAGE STRINGER 23L, CORRODED 4 INCHES FWD OF FRAME 68. REPAIRED 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.
SY6 CHECK, FUSELAGE STRINGER 23L, CORRODED 4 INCHES FWD OF FRAME 68. REPAIRED IAW SRM 53-41-14-201 PRINCIPLE 5.