What was found
PERFORMED OHEC INSPECTION OF THE FORWARD UPPER SPAR HIDDEN PORTIONS OF CHORD-CF6-80C STRUT,FOUND 01EA CRACK ON THE INBOARD FASTENER HOLE OF THE WEB AT NSTA221.25. REPAIRED AS PER PRI 581786-14.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PERFORMED OHEC INSPECTION OF THE FORWARD UPPER SPAR HIDDEN PORTIONS OF CHORD-CF6-80C STRUT,FOUND 01EA CRACK ON THE INBOARD FASTENER HOLE OF THE WEB AT NSTA221.25. REPAIRED AS PER PRI 581786-14.