Airworthiness Directive

AD 97-09-08 62 FR 23640 Active

Federal Aviation Administration · 14 CFR part 39

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…

FR document
97-10883
Amendment
39-10004
Published
1997-05-01
Effective
1997-06-23
Models covered
1

Last live check: 2026-08-19

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.
AD

97-09-08

FR doc 97-10883 · 62 FR 23640

AD 97-09-08Published 1997-05-01Effective 1997-06-23

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

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 Factories (GAF) Nomad Models N22S, N22B, and N24A airplanes.

Supersedes an earlier directive that is not in our index. See the official text.

Full official abstract

This amendment supersedes Airworthiness Directive 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 Factories (GAF) Nomad Models N22S, N22B, and N24A airplanes. This 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 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 this 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.

More directives for GAF Nomad N22 / N24

  1. AD 2010-11-06 Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd Mo... Effective 2010-07-06
  2. AD 2009-26-08 Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd Mo... Effective 2010-02-01
  3. AD 2006-21-12 Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd. M... Effective 2006-11-08
  4. AD 2005-10-24 Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd. M... Effective 2005-06-30
  5. AD 2004-06-10 Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd Ai... Effective 2004-04-28

All GAF Nomad N22 / N24 directives

Applies to 1 model in our index