Airworthiness Directive

AD 98-08-21 63 FR 19178 Active

Federal Aviation Administration · 14 CFR part 39

FR document
98-10057
Amendment
39-10470
Published
1998-04-17
Effective
1998-06-03
Models covered
1
Last live check
2026-09-30
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AD

98-08-21

FR doc 98-10057 · 63 FR 19178

AD 98-08-21Published 1998-04-17Effective 1998-06-03

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 inspecting the wing rear attachment fittings for cracks, replacing any cracked fitting, and incorporating wing rear attachment fitting reinforcement kits.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain SOCATA-Groupe AEROSPATIALE (Socata) Models TB10 and TB200 airplanes. This AD requires inspecting the wing rear attachment fittings for cracks, replacing any cracked fitting, and incorporating wing rear attachment fitting reinforcement kits. This AD is the result of mandatory continued airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified by this AD are intended to prevent structural failure of the wing rear attachment fittings caused by cracks in this area, which could result in the wing separating from the airplane if the airplane is operated with cracked wing rear attachment fittings over an extended period of time.

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All SOCATA TB (Tampico/Tobago/Trinidad) directives

Applies to 1 model in our index