As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING SCHEDULED INSPECTION IAW AD91-24-11 OF BS 870 FITTING FOUND CRACK INDICATION TOP SIDE OF HOLE IN ROW NR 3, BOTTOM HOLE IN SPLICE PLATE AND FITTING BELOW STR 9R. NO CRACK DETECTED AFTER REAMING. INSTALLED EXTERNAL DOUBLER IAW SB 727-53-0194 DWG 65C25277.