Airworthiness Directive

AD 2004-05-02 69 FR 9927

Federal Aviation Administration · 14 CFR part 39

FR document
04-4374
Amendment
39-13494
Published
2004-03-03
Models covered
1
Last live check
2026-08-17
AD

2004-05-02

FR doc 04-4374 · 69 FR 9927

AD 2004-05-02Published 2004-03-03Effective 2004-04-20

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.

Full official 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.

Applies to 1 model in our index