# Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd. Models N22B, N22S, and N24A Airplanes
> **Rule** · Final rule. · Published 2004-03-03 · Effective 2004-04-20 · 69 FR 9927
## Document
- **Document number:** 04-4374
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 69 FR 9927
- **Publication date:** 2004-03-03
- **Effective date:** 2004-04-20
- **FAA docket:** Docket No. 2003-CE-37-AD
## Abstract

The FAA adopts a new airworthiness directive (AD) for all AeroSpace Technologies of Australia Pty Ltd. (ASTA) Models N22B, N22S, and N24A airplanes. This AD requires you to repetitively inspect wing fittings for fatigue defects, replace or correct defective wing fittings, and replace the stub wing front spar assembly and wing fitting when fatigue life limits are reached. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Australia. We are issuing this AD to detect and correct defects in the wing strut upper end fittings, wing strut lower end fittings, stub wing strut pick up fittings, and the stub wing front spar assembly. These defects could result in failure of the fittings or spar assembly and lead to reduced structural capability or reduced controllability of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2004/03/03/04-4374/airworthiness-directives-aerospace-technologies-of-australia-pty-ltd-models-n22b-n22s-and-n24a)
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