As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT ELEVATOR HAS AN APPROXIMATELY 8 INCHES L SHAPED CRACK IN THE SKIN STARTING FROM THE SMALL RECTANGULAR ACCESS PANEL JUST FORWARD OF THE OUTBOARD END OF THE TRIM TAB. *S/D* FATIGUE CRACK. INSTALLED REPAIR DOUBLER IN CONJUNCTION WITH BEADED DOUBLER REPAIR REF SRM 55-20-3. REBALANCED ELEV ADDING 3.6 LB-IN. NEW MOMENT IS 120.9 LB-IN.