As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE PERFORMING INITIAL INSPECTION REQUIREMENTS OF AD 2011-23-05 FRAME LOCATION BS 500E BETWEEN S21L AND S20L AT THE 1.04-INCH DIAMETER WIRE CABLE HOLE. ACCOMPLISHED REPAIR PER AD INSTRUCTIONS, BOEING SB 737-53A1279 PART 3 AND 737-400 SRM 53-00-07 REPAIR 13.