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Airworthiness Directive

AD 99-07-11 64 FR 14820 Active

Federal Aviation Administration · 14 CFR part 39

FR document
99-7385
Amendment
39-11096
Published
1999-03-29
Effective
1999-04-16
Models covered
1
Last live check
2026-10-01

Printed from https://aircraftdirectives.com/ad/99-07-11 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

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.

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AD

99-07-11

FR doc 99-7385 · 64 FR 14820

AD 99-07-11Published 1999-03-29Effective 1999-04-16

Superseded by 2014-09-03

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

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 left-hand and right-hand outboard hinge fittings of the horizontal stabilizer for cracks, and replacing any cracked fitting.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to all SOCATA--Groupe Aerospatiale (SOCATA) Model TBM 700 airplanes. This AD requires inspecting the left-hand and right-hand outboard hinge fittings of the horizontal stabilizer for cracks, and replacing any cracked fitting. 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 structural damage to the stabilizer caused by outboard hinge fitting cracks, which could result in uncontrolled flight if the hinges break.

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All SOCATA/Daher TBM 700 directives

View on Federal Register (opens in a new tab) Search DRS manually for AD 99-07-11 (opens in a new tab)

Applies to 1 model in our index