As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION OF THE CENTER WING REAR SPAR WEB PER AD 2000-14- 07 AND BAC S/B 727-57A0182 REVEALED A .25 INCH CRACK IN THE WEB BELOW THE UPPER SPAR CAP. THE CRACK WAS ROUTED OUT OF THE WEB WITH A 2 INCH CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 383243-14AD, REV A.