As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 1 INCH CRACK IN LT THREAD SUPPORT ANGLE AT FIFTH STEP FROM BOTTOM OF VENTRAL STAIRS. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-5 AND 51-30-2. THE VENTRAL STAIRS RETRACTABLE STEPS WERE REMOVED FOR REPAIR AND REINSTALLED IAW MM 52-63-00.