What was found
DURING BRIDGE CHECK, MX FOUND CENTER WING TANK RT UPPER SKIN SURFACE CORROSION AT STA Y1150-1239, X-8 TO -120. REPAIRED CENTER WING TANK UPPER SKIN CORROSION AREA IAW ENGINEERING INSTRUCTION W2008A57B-1061 REV 00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING BRIDGE CHECK, MX FOUND CENTER WING TANK RT UPPER SKIN SURFACE CORROSION AT STA Y1150-1239, X-8 TO -120. REPAIRED CENTER WING TANK UPPER SKIN CORROSION AREA IAW ENGINEERING INSTRUCTION W2008A57B-1061 REV 00.