As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE PERFORMING E03/062/457 MODIFICATION LT AND RT WING REAR SPARS, A FASTENER HOLE WAS MISDRILLED. HOLE DIAMETER .213 INCH AT TRAILING EDGE WS 129, 2 INCHES IB OF JACKING PAD POINT ON RT WING. (M) MAINTENANCE REAMED HOLE TO ACCOMMODATE .25 INCH HOLE TO BE COLD WORKED AND INSTALLED HST11A68 HI-LITE IAW BSC EO 601R-57-10936. (K)