As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
A CRACK WAS FOUND ON BUSHING IN THE INBD HOLE OF THE RT REAR UPPER CAP. FORCE MATE BUSHING INSTALLATION PROCEDURE WAS ACCOMPLISHED IAW DWG SR 09550032, REV B AND FORCE MATE FIT TIP SHEET 238263, REV A PROCEDURE 3.2 PAR 3-12. ON UPPER HOLES.