What was found
FORWARD BILGE FUSELAGE FRAME UPPER FLANGE CORRODED AT BS 860, LBL 32. FRAME REPAIRED IAW B747 SRM 51-40-04 FIG 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FORWARD BILGE FUSELAGE FRAME UPPER FLANGE CORRODED AT BS 860, LBL 32. FRAME REPAIRED IAW B747 SRM 51-40-04 FIG 1.