Airworthiness Directive

AD 2001-23-05 66 FR 57850 Active

Federal Aviation Administration · 14 CFR part 39

FR document
01-28419
Amendment
39-12502
Published
2001-11-19
Effective
2002-01-04
Models covered
1
Last live check
2026-10-02
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AD

2001-23-05

FR doc 01-28419 · 66 FR 57850

AD 2001-23-05Published 2001-11-19Effective 2002-01-04

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 front seats that have solid metal seat pans.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to all SOCATA--Groupe Aerospatiale (SOCATA) Models TB 9, TB 10, TB 20, TB 21, and TB 200 airplanes that do not have factory Modification 165, any edition, incorporated on the front seats. This AD requires you to modify the front seats that have solid metal seat pans. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified by this AD are intended to eliminate the potential for the front seats to inadvertently unlock from their fixed positions. Such uncontrolled movement could prevent the pilot from making the necessary flight maneuvers to control the airplane.

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  4. AD 2007-13-18 Airworthiness Directives; SOCATA-Groupe Aerospatiale Models TB9, TB10, a... 2007-07-06
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All SOCATA TB (Tampico/Tobago/Trinidad) directives

Applies to 1 model in our index