What was found
CORROSION - WEB, L/H WING FIXED T/E REAR SPAR STA WS248 FUEL JETTISON TRANSFER VALVE FIXED POINT. I.A.W AMM 28-31-04-404-004 REV 148 INSTALLED THE ACTUATOR OF THE TRANSFER VALVE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION - WEB, L/H WING FIXED T/E REAR SPAR STA WS248 FUEL JETTISON TRANSFER VALVE FIXED POINT. I.A.W AMM 28-31-04-404-004 REV 148 INSTALLED THE ACTUATOR OF THE TRANSFER VALVE.