What was found
1S CHECK, CORROSION ON FLOORBEAM AT FRAME 68 & STRINGER 23R. REPAIRED IAW SRM 53-41-14-201 FIGURE 201 PRINCIPLE 5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
1S CHECK, CORROSION ON FLOORBEAM AT FRAME 68 & STRINGER 23R. REPAIRED IAW SRM 53-41-14-201 FIGURE 201 PRINCIPLE 5.