What was found
IN C/W AD 85-22-05, WING BOLT REJECTED DUE TO MINUTE GALLING CORROSION SPOT IN THE INNER RADIUS. BOLT REMOVED FROM THE LT LOWER FORWARD OUTER WING PANEL ATTACHMENT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
IN C/W AD 85-22-05, WING BOLT REJECTED DUE TO MINUTE GALLING CORROSION SPOT IN THE INNER RADIUS. BOLT REMOVED FROM THE LT LOWER FORWARD OUTER WING PANEL ATTACHMENT.