As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTIONS OF THE UPPER RIB CHORD ON THE RT WING AT RBL 70.5 PER BAC S/B 727-57-0112 AND AD 94-07-08 REVEALED A CRACK IN A FASTENER HOLE AT FS 760.95. THE HOLE WAS OVERSIZED TO REMOVE THE CRACK AND THEN COLD WORKED. THE HOLE WAS BUSHED AND THE CHORD REINFORCED WITH AN ALUMINUM ANGLE PER THE BAC S/B AND PER ER/A 382192-14AD, REV A.