What this page is: a restatement of what the official Federal Register
and manufacturer records show as of the date listed below each item. It is not
a determination that any specific aircraft or engine is, or is not, in compliance.
Under 14 CFR §91.403 and §91.417, the aircraft owner/operator is responsible
for maintaining airworthiness and required records. Always verify against the official FAA
and manufacturer sources linked below before making a maintenance or airworthiness decision.
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Airworthiness Directives
2 records
AD
2009-02-02
FR doc E9-776 · 74 FR 4119
AD 2009-02-02Published 2009-01-23Effective 2009-02-12
Polskie Zaklady Lotnicze Spolka zo.o Model PZL M26 01 Airplanes
Prompted by mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product.
Full official abstract
Airworthiness Directives; Polskie Zaklady Lotnicze Spolka zo.o Model PZL M26 01 Airplanes
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Source: Federal Register document E9-776, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
AD 2006-03-17Published 2006-02-10Effective 2006-02-24
Polskie Zaklady Lotnicze Spolka zo.o. Model PZL M26 01 Airplanes
Requires you to repetitively inspect fuselage frame No.
Full official abstract
Airworthiness Directives; Polskie Zaklady Lotnicze Spolka zo.o. Model PZL M26 01 Airplanes
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.
Source: Federal Register document 06-1198, retrieved 2026-08-17 · re-verified against the live Federal Register API 2026-08-17
