As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE / SKIN / L1 DOOR CUTOUT / UPPER HINGE CUTOUT : CRACK REPAIR A .75" CRACK WAS FOUND IN THE SKIN AT THE UPPER HINGE CUTOUTOF THE L1 DOOR OPENING. THE CRACK WAS ROUTED OUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL STEEL DOUBLER PER THE PROCEDURES OF BAC S/B 727-53-0198 AND ER/A 381212-14, REV B.