Aircraft model

PZL PW-5 / PW-6

PZL-Swidnik / Zaklad Jezow

Airworthiness Directives
2
Manufacturer bulletins
00 Service Bulletins
Last live check
2026-10-022 of 2 re-checked
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.

Also known as: Smyk

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What Airworthiness Directives apply to the PZL PW-5 / PW-6

The FAA has published 2 Airworthiness Directives that name the PZL PW-5 / PW-6 (PZL-Swidnik / Zaklad Jezow), the earliest in 2005 and the newest on 2010-07-27.

Newest

  1. AD 2010-15-07 Airworthiness Directives; Zaklad Szybo wcowy “Jeżów” Henryk Mynarski Model PW-6U Sailplane... 2010-07-27
  2. AD 2005-19-17 Airworthiness Directives; PZL-Swidnik S.A. Models PW-5 “Smyk” and PW-6U Gliders 2005-09-21

See all 2 directives

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 2010-15-07Zaklad Szybo wcowy “Jeżów” Henryk Mynarski Model PW-6U Sailplanes2010-08-16Active
AD

2010-15-07

FR doc 2010-17924 · 75 FR 43807

AD 2010-15-07Published 2010-07-27Effective 2010-08-16

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.

Zaklad Szybo wcowy “Jeżów” Henryk Mynarski Model PW-6U Sailplanes

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; Zaklad Szybo wcowy “Jeżów” Henryk Mynarski Model PW-6U Sailplanes

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 2010-17924, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-02

ADAD 2005-19-17PZL-Swidnik S.A. Models PW-5 “Smyk” and PW-6U Gliders2005-10-31Active
AD

2005-19-17

FR doc 05-18526 · 70 FR 55248

AD 2005-19-17Published 2005-09-21Effective 2005-10-31

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.

PZL-Swidnik S.A. Models PW-5 “Smyk” and PW-6U Gliders

Requires you to inspect for the minimum dimension of the left side aileron, right side aileron, and airbrake push-rod ends for certain Model PW-5 "Smyk" gliders; inspect for the minimum dimension of the aileron, airbrake, and…

Full official abstract

Airworthiness Directives; PZL-Swidnik S.A. Models PW-5 “Smyk” and PW-6U Gliders

The FAA adopts a new airworthiness directive (AD) for certain PZL-Swidnik S.A. (PZL-Swidnik) Models PW-5 "Smyk" and PW-6U gliders. This AD requires you to inspect for the minimum dimension of the left side aileron, right side aileron, and airbrake push-rod ends for certain Model PW-5 "Smyk" gliders; inspect for the minimum dimension of the aileron, airbrake, and elevator control push-rod ends for certain Model PW-6U gliders; and replace any push-rod end that does not meet the minimum dimension. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Poland. We are issuing this AD to detect and replace any push-rod end that does not meet the minimum dimension, which could result in failure of the control system. This failure could lead to loss of control of the glider.

Source: Federal Register document 05-18526, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-02

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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