Just wondered if anyone else had read it:-
AD 2/2015.
There have been a number of reported cases in Australia and overseas of primary flight control cable terminals failing due to stress corrosion cracking. Inspection of primary flight control cable terminals can be difficult and problematic. Surface indication of stress corrosion cracking, such as corrosion pitting or cracking can be very difficult to see, even under 10X magnification and can sometimes emanate from within the sleeve of the terminal. Primary flight control cable terminal failure in flight may result in loss of aircraft control.
This AD has been issued to address the safety concern and feedback received in response to NPRM 1303MS.