What was found
CRACK ON INNER ANGLE OF ATTACHMENT STRUCTURE FOR INNER DOOR LEVER. REMOVED AND REPLACED THE ANGLE, IAW PJ162163, SRM 51-42-06-001-001-A01, AND SRM 51-40-11-001-001-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON INNER ANGLE OF ATTACHMENT STRUCTURE FOR INNER DOOR LEVER. REMOVED AND REPLACED THE ANGLE, IAW PJ162163, SRM 51-42-06-001-001-A01, AND SRM 51-40-11-001-001-A01.