What was found
CORROSION ON FUSELAGE EXTERIOR SKIN BETWEEN BS 523 TO 540 AT STRINGER 23 LT. REMOVED FASTENERS, BLENDED OUT CORROSION, RESTORED FINISH & INSTALLED FASTENERS IAW EA B737-53-034528.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON FUSELAGE EXTERIOR SKIN BETWEEN BS 523 TO 540 AT STRINGER 23 LT. REMOVED FASTENERS, BLENDED OUT CORROSION, RESTORED FINISH & INSTALLED FASTENERS IAW EA B737-53-034528.