As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE PERFORMING AD 2009-23-01 (E)(3) NDT INSPECTION, INDICATION OF CRACKING WAS IDENTIFIED IN THE END CAP – SEE ATTACHED NDT REPORT. THIS INSPECTION WAS PERFORMED ON UC-93 AND THE ACTUATOR HAD 1015 CYCLES SINCE LAST INSPECTION. NO CRACKS WERE VISUALLY VISIBLE AND NO LEAKS WERE DETECTED.