Airworthiness Directive

AD 2006-03-17 71 FR 6973 Active

Federal Aviation Administration · 14 CFR part 39

FR document
06-1198
Amendment
39-14481
Published
2006-02-10
Effective
2006-02-24
Models covered
1

Last live check: 2026-08-19

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AD

2006-03-17

FR doc 06-1198 · 71 FR 6973

AD 2006-03-17Published 2006-02-10Effective 2006-02-24

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 repetitively inspect fuselage frame No.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for certain Polskie Zaklady Lotnicze Spolka zo.o. Model PZL M26 01 airplanes. This AD requires you to repetitively inspect fuselage frame No. XI for cracks and to replace fuselage frame No. XI and install reinforcement modifications if any cracks are found. The installation of reinforcement modifications is terminating action for the repetitive inspection requirement. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for the European Union. We are issuing this AD to detect and correct cracks in fuselage frame No. XI, which could result in failure of this frame. This failure could lead to failure of the tail section of the airplane.

More directives for PZL M26

  1. AD 2009-02-02 Airworthiness Directives; Polskie Zaklady Lotnicze Spolka zo.o Model PZL... Effective 2009-02-12

All PZL M26 directives

Applies to 1 model in our index