As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE BS 1000 LT BETWEEN STR 37 & 40 HAS CORROSION ON SKIN INSIDE OF FWD PIT. REMOVED CORROSION AT STA 1000 STR 39-41 LT PER B747 SRM 53-30-03 FIG 12. CUT OUT LIMIT SKIN AREA PER B747 SRM 53-10-01 FIG 1, NDT CHECKED NO CRACK NOTED FABRICATED INSTALLED REPAIR PER B747 SRM 53-30-03 FIG 12 PGS 27-30. ALODINED AND PRIMED PER B747 SRM 51-10-02 PG 2-8.