As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE LT SIDE OF THE FUSELAGE AT STA 263, WL 216 WAS DAMAGED FROM CONTACT WITH A JETWAY. THE DAMAGE INVOLVED AN AREA OF SKIN 18 INCHES LONG BY 5 INCHES WIDE AND INCLUDED STA 263 O/B CHORD. THE DAMAGED FRAME CHORD WAS CUT OUT AND A NEW SECTION WAS SPLICED IN PER SRM GUIDELINES. THE SKIN WAS REPAIRED PER SRM GUIDELINES AS WELL. THIS WAS A MAJOR REPAIR. REF MAJOR REPAIR NUMBER 108, FILE NUMBER C50-53-10.