Airworthiness Directive

AD 2006-21-12 71 FR 61636 Active

Federal Aviation Administration · 14 CFR part 39

Requires you to visually inspect the ailerons for damage and replace if necessary; adjust the engine power levers aural warning microswitches; set flap extension and flap down operation limitations; and fabricate and install…

FR document
E6-17425
Amendment
39-14797
Published
2006-10-19
Effective
2006-11-08
Models covered
1

Last live check: 2026-08-19

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AD

2006-21-12

FR doc E6-17425 · 71 FR 61636

AD 2006-21-12Published 2006-10-19Effective 2006-11-08

Supersedes 2003-22-13

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

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 you to visually inspect the ailerons for damage and replace if necessary; adjust the engine power levers aural warning microswitches; set flap extension and flap down operation limitations; and fabricate and install cockpit flap extension and flap down operation restriction placards.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) to supersede AD 2003-22-13, which applies to all AeroSpace Technologies of Australia Pty Ltd. (ASTA) Models N22B and N24A airplanes. AD 2003-22-13 currently requires you to visually inspect the ailerons for damage and replace if necessary; adjust the engine power levers aural warning microswitches; set flap extension and flap down operation limitations; and fabricate and install cockpit flap extension and flap down operation restriction placards. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Australia. The FAA inadvertently omitted Model N22S airplanes from the applicability of AD 2003-22-13. Therefore, this AD retains the actions exactly as required in AD 2003-22-13 and adds Model N22S airplanes to the Applicability section. We are issuing this AD to prevent failure of the aileron due to undetected pre-existing aileron damage and airplane operation outside of the approved limits. Aileron failure could lead to reduced or 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 2005-10-24 Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd. M... Effective 2005-06-30
  4. AD 2004-06-10 Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd Ai... Effective 2004-04-28
  5. AD 2004-05-02 Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd. M... Effective 2004-04-20

All GAF Nomad N22 / N24 directives

Applies to 1 model in our index