Airworthiness Directive

AD 98-04-03 63 FR 6638 Active

Federal Aviation Administration · 14 CFR part 39

FR document
98-3230
Amendment
39-10316
Published
1998-02-10
Effective
1998-03-24
Models covered
1
Last live check
2026-09-30
This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.
AD

98-04-03

FR doc 98-3230 · 63 FR 6638

AD 98-04-03Published 1998-02-10Effective 1998-03-24

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 bolts and spacers of the upper attachments of the front belts for cracks, dents, etc.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Socata-Groupe Aerospatiale (Socata) Models TB9, TB10, TB20, TB21, and TB200 airplanes. This AD requires inspecting the bolts and spacers of the upper attachments of the front belts for cracks, dents, etc. (damage); replacing any damaged bolts or spacers; incorporating a front belts upper attachment reinforcement kit; and reconditioning the belts. 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 failure of the upper seat belt attachment caused by excessive loads on the upper attachment of the belt, which could result in bodily injury to the occupants during landing.

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All SOCATA TB (Tampico/Tobago/Trinidad) directives

Applies to 1 model in our index