Airworthiness Directive

AD 96-23-03 61 FR 57993 Active

Federal Aviation Administration · 14 CFR part 39

FR document
96-28164
Amendment
39-9808
Published
1996-11-12
Effective
1996-12-23
Models covered
1
Last live check
2026-10-01
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AD

96-23-03

FR doc 96-28164 · 61 FR 57993

AD 96-23-03Published 1996-11-12Effective 1996-12-23

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 replacing the existing fuselage stub fin plate with one of improved design, P/N 1E/N-12-57.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to Aerospace Technologies of Australia Pty Ltd. (ASTA) Models N22B, N24A, and N22S airplanes that are not equipped with a part number (P/N) 1E/N-12-57 fuselage stub fin plate (MOD N759). This action requires replacing the existing fuselage stub fin plate with one of improved design, P/N 1E/N-12-57. This action results from several reports of cracks along the forward flange of the fuselage stub fin plate in the area of Rib Water Line (WL) 138.87. The actions specified by this AD are intended to prevent structural failure of the fuselage area caused by a cracked stub fin plate, which could result in loss of control of the airplane.

More directives for GAF Nomad N22 / N24

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  2. AD 2009-26-08 Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd Mo... 2009-12-28
  3. AD 2006-21-12 Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd. M... 2006-10-19
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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