As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LH AFT FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE (SKATE ANGLE) HAS CHAFE DAMAGE AT FWD AND AFT ENDS AND BARE METAL ALONG ENTIRE LENGTH / LH AFT CLOSURE ANGLE (SKATE ANGLE) DOES NOT HAVE ALLOWABLE DAMAGE PER SRM THEREFORE; WILL BE REPAIRED BY REPLACEMENT PER REF SRM 51-10-02 PARAGRAPH 9. REMOVED AND REPLACED SKATE ANGLE PER REF SRM 51-40-02-0G AND DWG NBR 148A8300