What was found
DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FUSELAGE FRAME, BS 344 AT STRINGER 23R. REPAIRED PER SRM 53-10-4, FIGURE 1. (Z)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FUSELAGE FRAME, BS 344 AT STRINGER 23R. REPAIRED PER SRM 53-10-4, FIGURE 1. (Z)