What was found
CORROSION AT L2 DOOR SILL AFT END AT FRAME 68, STRINGER 23L, Y1172.66. REPAIRED L2 DOOR SILL AFT END IAW SRM 53-41-14-201, REPAIR PRINCIPLE 5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION AT L2 DOOR SILL AFT END AT FRAME 68, STRINGER 23L, Y1172.66. REPAIRED L2 DOOR SILL AFT END IAW SRM 53-41-14-201, REPAIR PRINCIPLE 5.