PZL M26 Airworthiness Directives

Q: What is the newest Airworthiness Directive for the PZL M26?

AD 2009-02-02, published 2009-01-23: Airworthiness Directives; Polskie Zaklady Lotnicze Spolka zo.o Model PZL M26 01 Airplanes.

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This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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Also known as: M26 01

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What Airworthiness Directives apply to the PZL M26

The FAA has published 2 Airworthiness Directives that name the PZL M26 (Polskie Zaklady Lotnicze), the earliest in 2006 and the newest on 2009-01-23.

Newest

AD 2009-02-02 Airworthiness Directives; Polskie Zaklady Lotnicze Spolka zo.o Model PZL M26 01 Airplanes 2009-01-23
AD 2006-03-17 Airworthiness Directives; Polskie Zaklady Lotnicze Spolka zo.o. Model PZL M26 01 Airplanes 2006-02-10

See all 2 directives

The ones owners meet again

AD 2006-03-17 Airworthiness Directives; Polskie Zaklady Lotnicze Spolka zo.o. Model PZL M26 01 Airplanes 2006-02-10 Repetitive inspection or action

We index directives by model, not by serial number or N-number; the record page and the official document say which serials apply.

How to use this page: check the newest directives at every annual, keep the repetitive items on your inspection calendar, and open the official Federal Register text before any work - our summaries are a reading aid, not a determination of compliance.

Airworthiness Directives

2 records

ADAD 2009-02-02Polskie Zaklady Lotnicze Spolka zo.o Model PZL M26 01 Airplanes2009-02-12Active

2009-02-02

FR doc E9-776 · 74 FR 4119

AD 2009-02-02Published 2009-01-23Effective 2009-02-12

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.

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 · checked against the live Federal Register record on 2026-10-02

View on Federal Register View this AD in FAA DRS Print AD packet

ADAD 2006-03-17Polskie Zaklady Lotnicze Spolka zo.o. Model PZL M26 01 Airplanes2006-02-24Active

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.

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 · checked against the live Federal Register record on 2026-10-02

View on Federal Register View this AD in FAA DRS Print AD packet

Service Bulletins

0 records

No Service Bulletins in our index yet for this airframe. We only list SBs we have individually sourced from the manufacturer — we never invent one.

This page indexes 2 ADs and 0 SBs from primary sources. The FAA may have issued additional directives for this airframe that are not yet included.

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