Airworthiness Directive

AD 2000-24-23 65 FR 77261 Active

Federal Aviation Administration · 14 CFR part 39

FR document
00-30945
Amendment
39-12030
Published
2000-12-11
Effective
2001-01-27
Models covered
1
Last live check
2026-10-01
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AD

2000-24-23

FR doc 00-30945 · 65 FR 77261

AD 2000-24-23Published 2000-12-11Effective 2001-01-27

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 inspect the airbrake control system for cracks; and if cracks are detected, replace the airbrake control system.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain S.N. CENTRAIR 101 series gliders. This AD requires you to inspect the airbrake control system for cracks; and if cracks are detected, replace the airbrake control system. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified in this AD are intended to detect cracks in the airbrake control system and replace cracked parts with parts of improved design. A crack in the airbrake control system could prevent the pilot from using the airbrake system.

More directives for Centrair 101/201

  1. AD 2014-07-08 Airworthiness Directives; Centrair Gliders 2014-04-22
  2. AD 2010-24-10 Airworthiness Directives; CENTRAIR Models 101, 101A, 101P, and 101AP Gli... 2010-12-01
  3. AD 2005-24-01 Airworthiness Directives; CENTRAIR 101 Series Gliders 2005-11-18
  4. AD 2005-08-12 Airworthiness Directives; CENTRAIR 101 Series Gliders 2005-04-21
  5. AD 2005-08-06 Airworthiness Directives; CENTRAIR 101 Series Gliders 2005-04-19

All Centrair 101/201 directives

Applies to 1 model in our index