AircraftDirectives
MembershipSign inCreate free account
Menu
Airworthiness Directive

AD 2005-19-17 70 FR 55248 Active

Federal Aviation Administration · 14 CFR part 39

FR document
05-18526
Amendment
39-14282
Published
2005-09-21
Effective
2005-10-31
Models covered
1
Last live check
2026-10-02

Printed from https://aircraftdirectives.com/ad/2005-19-17 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

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.

Opens your browser's print dialog. Choose “Save as PDF” to export a file. Keyboard: Ctrl+P or Cmd+P.

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.

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

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.

More directives for PZL PW-5 / PW-6

  1. AD 2010-15-07 Airworthiness Directives; Zaklad Szybo wcowy “Jeżów” Henryk Mynarski Mod... 2010-07-27

All PZL PW-5 / PW-6 directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab)

Applies to 1 model in our index