Airworthiness Directive

AD 2000-22-17 65 FR 68065 Active

Federal Aviation Administration · 14 CFR part 39

FR document
00-28439
Amendment
39-11964
Published
2000-11-14
Effective
2000-12-29
Models covered
1
Last live check
2026-10-01
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AD

2000-22-17

FR doc 00-28439 · 65 FR 68065

AD 2000-22-17Published 2000-11-14Effective 2000-12-29

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 repetitively inspect, and, if necessary, replace elevator clevis and rudder governor control clevis that are too thin.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to all SOCATA--Groupe AEROSPATIALE (Socata) Models MS 880B, MS 885, MS 892A-150, MS 892E-150, MS 893A, MS 893E, MS 894A, MS 894E, Rallye 100S, Rallye 150T, Rallye 150ST, Rallye 235C, and Rallye 235E airplanes. This AD requires you to repetitively inspect, and, if necessary, replace elevator clevis and rudder governor control clevis that are too thin. 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 correct rudder and elevator control clevis that are too thin because of abnormal wear, with consequent failure of the rudder and elevator clevis. Such failure could lead to loss of directional or pitch control.

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  3. AD 2003-06-07 Airworthiness Directives; Socata-Groupe Aerospatiale Models MS 892A-150,... 2003-03-27
  4. AD 2002-05-04 Airworthiness Directives; SOCATA-Groupe AEROSPATIALE Models MS 892A-150,... 2002-03-11

All SOCATA Rallye / MS 880 directives

Applies to 1 model in our index