What was found
NR 1 PYLON MID SPAR O/B LOWER TANG CLOSE OUT ANGLE, HFEC INDICATES CRACKED O/B MOST AFT FASTENER (CRACK INDICATED ON AFT SIDE) :CORRECTION-SHOULD BE MID SPAR I/B LOWER TANG. :VERIFIED CRACK WITH FPI INSPECTION AND NOTIFIED FOREMAN. PERM REPAIR WAS ACP'D REF ECRA 5400-01140. CRACK WAS STOP DRILLED AND VERIFIED BY HFEC. ACP'D CLOSE OUT ANGLE REPAIR PER FIG 1, 2, AND 3 OF THE ECRA. ACCOMPLISH PERMANENT REPAIR NO LATER THAN 10/SEP/14 BY REPLACING MIDSPAR FITTING. BOEING RECOMMENDS THAT THE SIP SB 767-54-0080 BE PERFORMED UPON THE UPCOMING PERMANENT REPAIR.