This document specifies the required characteristics, inspections and test methods, quality assurance, conditions for qualification, acceptance and delivery of rod-ends with self‑aligning bearings metal to metal designed to withstand slight swivelling under load. They are intended for use in fixed or moving parts of the aircraft structure and their control mechanisms.

This document is applicable to all rod-ends with self‑aligning bearings metal to metal. It may be applied when referred to in a product standard or in a design specification.