What was found
RT WING UPPER SKIN AT THE FRONT SPAR PITCH LOAD FITTING WAS FOUND 1EA FASTENER CRACK INDICATION. ONE FASTENER CRACK HOLE REPAIR ACCOMPLISHED IAW WC 5724-01005-12 AND DAL VA 82327ADMA, REV.C.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT WING UPPER SKIN AT THE FRONT SPAR PITCH LOAD FITTING WAS FOUND 1EA FASTENER CRACK INDICATION. ONE FASTENER CRACK HOLE REPAIR ACCOMPLISHED IAW WC 5724-01005-12 AND DAL VA 82327ADMA, REV.C.