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Airworthiness Directive

AD 98-21-15 63 FR 54565 Active

Federal Aviation Administration · 14 CFR part 39

FR document
98-26968
Amendment
39-10824
Published
1998-10-13
Effective
1998-11-20
Models covered
1
Last live check
2026-09-30

Printed from https://aircraftdirectives.com/ad/98-21-15 · 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

98-21-15

FR doc 98-26968 · 63 FR 54565

AD 98-21-15Published 1998-10-13Effective 1998-11-20

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 modifying the oxygen generators.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain SOCATA--Groupe AEROSPATIALE (SOCATA) Model TBM 700 airplanes. This AD requires modifying the oxygen generators. 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 oxygen generators caused by misalignment of the firing pin, which could result in crew incapacitation and loss of the airplane.

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All SOCATA/Daher TBM 700 directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab)

Applies to 1 model in our index