What was found
CORROSION ON FUSELAGE SKIN FWD EDGE OF STA 887 BUTT JOINT BETWEEN STRINGER S-24R AND S-26R. REMOVED CORROSION ON FUSELAGE BELLY SKIN BLEND FWD OF BS 887; S-24R TO S-26R) FOUND TO BE IN LIMITS PER SRM 51-10-02 AND EA 25-153-01849.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON FUSELAGE SKIN FWD EDGE OF STA 887 BUTT JOINT BETWEEN STRINGER S-24R AND S-26R. REMOVED CORROSION ON FUSELAGE BELLY SKIN BLEND FWD OF BS 887; S-24R TO S-26R) FOUND TO BE IN LIMITS PER SRM 51-10-02 AND EA 25-153-01849.