Summary
This document proposes to supersede AD 82-25-09 which currently requires repetitively inspecting the pilot and co-pilot control wheel sub-assemblies for cracks, and if cracked, modifying the cracked part on the AeroSpace Technologies of Australia, Limited (ASTA), formerly Government Aircraft Industries (GAF) Nomad Models N22S, N22B, and N24A airplanes. The proposed action would retain the repetitive inspection of the pilot and co-pilot control wheel sub- assemblies for cracks, but would include a modification that would terminate the repetitive inspections by replacing or re-working the control wheel sub-assembly with a part of improved design. This proposed superseding action is prompted by cracking in the control wheel sub-assemblies and the manufacture of an improved part that would terminate the repetitive inspection. The actions specified by the proposed AD are intended to prevent failure of the pilot's and co- pilot's control wheels, which, if not detected and corrected, could result in loss of control of the airplane.