As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING A ROUTINE INSPECTION OF THE HEAD REST. THE ENGINEER NOTED THAT THE T HANDLE PORTION ON ON QUICK RELEASE PIN, PIP PIN, PN NAS1333A2S07D WAS CRACKED & THE HANDLE IS FREE TO MOVE APPROX 1MM ALONG THE AXIS OF THE PIN. THIS ASSEMBLY IS SUBJECT TO AD CF-91-29R1.