Airworthiness Directive

AD 2004-06-10 69 FR 16775 Active

Federal Aviation Administration · 14 CFR part 39

FR document
04-6417
Amendment
39-13536
Published
2004-03-31
Effective
2004-04-28
Models covered
1
Last live check
2026-10-02
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AD

2004-06-10

FR doc 04-6417 · 69 FR 16775

AD 2004-06-10Published 2004-03-31Effective 2004-04-28

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 inspect the forward and aft face of the rear fuselage frame for cracks and to repair or modify accordingly.

Full official abstract

The FAA adopts a new airworthiness directive (AD) for all AeroSpace Technologies of Australia Pty Ltd Model N22B, N22S, and N24A airplanes. This AD requires you to inspect the forward and aft face of the rear fuselage frame for cracks and to repair or modify accordingly. This AD is the result of mandatory continuing airworthiness information issued by the airworthiness authority for Australia. We are issuing this AD to detect and correct cracks in the rear fuselage frame, which could result in failure of the fuselage rear bulkhead and consequent loss of structural integrity.

More directives for GAF Nomad N22 / N24

  1. AD 2010-11-06 Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd Mo... 2010-06-01
  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
  4. AD 2005-10-24 Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd. M... 2005-05-23
  5. AD 2004-05-02 Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd. M... 2004-03-03

All GAF Nomad N22 / N24 directives

Applies to 1 model in our index