Airworthiness Directive

AD 2006-24-09 71 FR 70300 Active

Federal Aviation Administration · 14 CFR part 39

Requires actions that are intended to address the unsafe condition described in the MCAI.

FR document
E6-20325
Amendment
39-14838
Published
2006-12-04
Effective
2007-01-08
Models covered
1

Last live check: 2026-08-19

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AD

2006-24-09

FR doc E6-20325 · 71 FR 70300

AD 2006-24-09Published 2006-12-04Effective 2007-01-08

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 actions that are intended to address the unsafe condition described in the MCAI.

Full official abstract

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as a discrepancy between the design documentation and the Technical Service Manual. In 1981, a castellated nut with cotter pin was introduced to secure the rudder, replacing the self-locking nut through PZL-Bielsko Bulletin No. BE-06/50-3/81. This change has not been introduced to the Technical Service Manual and use of a self-locking nut, in accordance with the Manual, is still possible. We are issuing this AD to require actions that are intended to address the unsafe condition described in the MCAI.

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Applies to 1 model in our index