AircraftDirectives
MembershipSign inCreate free account
Menu
Airworthiness Directive

AD 2005-25-22 70 FR 75390 Active

Federal Aviation Administration · 14 CFR part 39

Requires you to perform a visual inspection of the turnbuckle link for cracks or wear and replace if cracks or wear is found.

Federal Register (opens in a new tab)FAA DRS (opens in a new tab)

FR document
05-23896
Amendment
39-14415
Published
2005-12-20
Effective
2006-01-27
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2005-25-22 · 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

2005-25-22

FR doc 05-23896 · 70 FR 75390

AD 2005-25-22Published 2005-12-20Effective 2006-01-27

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 perform a visual inspection of the turnbuckle link for cracks or wear and replace if cracks or wear is found.

Full official abstract

The FAA adopts a new airworthiness directive (AD) for all Przedsiebiorstwo Doswiadczalno-Produkcyjne Szybownictwa "PZL-Bielsko" Model SZD-50-3 "Puchacz" gliders. This AD requires you to perform a visual inspection of the turnbuckle link for cracks or wear and replace if cracks or wear is found. This action only applies to those gliders where the turnbuckle is directly connected to the pedal. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Poland. We are issuing this AD to detect and correct cracks in the turnbuckle link, which could result in failure of the rudder cable. This failure could lead to loss of control of the glider.

More directives for PZL-Bielsko SZD-50 Puchacz

  1. AD 2015-13-03 Airworthiness Directives; Przedsiebiorstwo Doswiadczalno-Produkcyjne Szy... Effective 2015-08-03
  2. AD 2014-12-08 Airworthiness Directives; Przedsiebiorstwo Doswiadczalno-Produkcyjne Szy... Effective 2014-07-22
  3. AD 2008-09-08 Airworthiness Directives; Przedsiebiorstwo Doswiadczalno-Produkcyjne Szy... Effective 2008-06-05
  4. AD 2008-02-09 Airworthiness Directives; Przedsiebiorstwo Doswiadczalno-Produkcyjne Szy... Effective 2008-02-01
  5. AD 2007-06-08 Airworthiness Directives; Przedsiebiorstwo Doswiadczalno-Produkcyjne Szy... Effective 2007-04-19

All PZL-Bielsko SZD-50 Puchacz directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index