What was found
LEFT AND RIGHT ELEVATOR CONTROL TAB PUSHROD INBOARD CRANK ARM ATTACH BOLT NUT IS CHAFING STRUCTURE WHEN YOKE IS POSITIONED TO FULL AIRCRAFT NOSE DOWN. TRIMMED FITTING IAW MWX-ORD-01-00467H.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT AND RIGHT ELEVATOR CONTROL TAB PUSHROD INBOARD CRANK ARM ATTACH BOLT NUT IS CHAFING STRUCTURE WHEN YOKE IS POSITIONED TO FULL AIRCRAFT NOSE DOWN. TRIMMED FITTING IAW MWX-ORD-01-00467H.