Airworthiness Directive

AD 96-24-05 61 FR 59325 Active

Federal Aviation Administration · 14 CFR part 39

FR document
96-29721
Amendment
39-9831
Published
1996-11-22
Effective
1997-01-17
Models covered
1
Last live check
2026-10-01
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AD

96-24-05

FR doc 96-29721 · 61 FR 59325

AD 96-24-05Published 1996-11-22Effective 1997-01-17

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 inspecting the flap and aileron control rod fork ends for water accumulation and corrosion inside the internally drilled holes, and replacing the control rod fork ends if there is visible corrosion, or sealing the hole…

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to Aerospace Technologies of Australia (ASTA) Nomad Models N22B, N22S, and N24A airplanes. This action requires inspecting the flap and aileron control rod fork ends for water accumulation and corrosion inside the internally drilled holes, and replacing the control rod fork ends if there is visible corrosion, or sealing the hole if no corrosion is found. Reports of water entering the internal holes of the flap and aileron control rod fork ends, causing corrosion, prompted this AD action. The actions specified by this AD are intended to prevent corrosion and water accumulation in the flap and aileron control rod fork ends, which, if not detected and corrected, could cause loss of control of the flaps and aileron and possible loss of control of the airplane.

More directives for GAF Nomad N22 / N24

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  5. AD 2004-06-10 Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd Ai... 2004-03-31

All GAF Nomad N22 / N24 directives

Applies to 1 model in our index