Airworthiness Directive

AD 2000-24-22 65 FR 77774 Active

Federal Aviation Administration · 14 CFR part 39

FR document
00-30903
Amendment
39-12029
Published
2000-12-13
Effective
2001-01-27
Models covered
1
Last live check
2026-10-02
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AD

2000-24-22

FR doc 00-30903 · 65 FR 77774

AD 2000-24-22Published 2000-12-13Effective 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 modify the rear canopy emergency release system.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to all S.N. CENTRAIR Model 201B gliders. This AD requires you to modify the rear canopy emergency release 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 prevent the rear canopy retaining strap from not releasing properly during the emergency egress procedure because of the current design of the rear canopy emergency release system. This condition, if not corrected, will not allow the rear canopy to completely separate from the glider and could result in potential injury to the pilot during an emergency egress.

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