PZL-Krosno KR-03A Airworthiness Directives

Q: What is the newest Airworthiness Directive for the PZL-Krosno KR-03A?

AD 2002-16-17, published 2002-08-16: Airworthiness Directives; Barry Aviation, LLC Model PZL-Krosno KR-03A “Peregrine” (Puchatek) Sailplanes.

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Also known as: Peregrine, Puchatek

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What Airworthiness Directives apply to the PZL-Krosno KR-03A

The FAA has published one Airworthiness Directive that names the PZL-Krosno KR-03A, published on 2002-08-16.

Newest

AD 2002-16-17 Airworthiness Directives; Barry Aviation, LLC Model PZL-Krosno KR-03A “Peregrine” (Puchate... 2002-08-16

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Airworthiness Directives

1 record

ADAD 2002-16-17Barry Aviation, LLC Model PZL-Krosno KR-03A “Peregrine” (Puchatek) Sailplanes2002-08-30Active

2002-16-17

FR doc 02-20400 · 67 FR 53475

AD 2002-16-17Published 2002-08-16Effective 2002-08-30

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.

Barry Aviation, LLC Model PZL-Krosno KR-03A “Peregrine” (Puchatek) Sailplanes

Requires you to inspect to ensure that the correct horizontal stabilizer attachment fittings are installed, install the correct fittings if necessary, and incorporate a "NO LIFT" placard to the vertical stabilizer.

Full official abstract

Airworthiness Directives; Barry Aviation, LLC Model PZL-Krosno KR-03A “Peregrine” (Puchatek) Sailplanes

This amendment adopts a new airworthiness directive (AD) that applies to certain Barry Aviation, LLC Model PZL-Krosno KR-03A "Peregrine" (Puchatek) sailplanes. This AD requires you to inspect to ensure that the correct horizontal stabilizer attachment fittings are installed, install the correct fittings if necessary, and incorporate a "NO LIFT" placard to the vertical stabilizer. This AD is the result of reports of cracks in the horizontal stabilizer attachment fittings on the affected sailplanes. Analysis of these incidents reveals that incorrect fittings were installed. The actions specified by this AD are intended to prevent such cracks in the horizontal stabilizer attachment fittings, which could result in the horizontal stabilizer separating from the sailplane with consequent loss of control of the sailplane.

Source: Federal Register document 02-20400, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-02

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Service Bulletins

0 records

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This page indexes 1 AD 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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