Airworthiness Directive

AD 2002-20-04 67 FR 61980 Active

Federal Aviation Administration · 14 CFR part 39

FR document
02-24687
Amendment
39-12899
Published
2002-10-03
Effective
2002-11-18
Models covered
1
Last live check
2026-10-02
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AD

2002-20-04

FR doc 02-24687 · 67 FR 61980

AD 2002-20-04Published 2002-10-03Effective 2002-11-18

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 exhaust system.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain SOCATA--Groupe AEROSPATIALE (Socata) Model TB 21 airplanes. This AD requires you to modify the exhaust system. 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 prevent high levels of carbon monoxide from entering the cockpit during certain flight configurations, which could result in the pilot becoming incapacitated or impairing his/her judgement. Such a condition could lead to the pilot not being able to make critical flight safety decisions and result in loss of control of 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