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Airworthiness Directive

AD 2007-04-08 72 FR 7559 Active

Federal Aviation Administration · 14 CFR part 39

Requires you to inspect the pilot door locking stop-fittings for correct length and, if any incorrect length pilot door locking stop-fittings are found, replace them.

Federal Register (opens in a new tab)

FR document
E7-2507
Amendment
39-14939
Published
2007-02-16
Effective
2007-03-23
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2007-04-08 · 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

2007-04-08

FR doc E7-2507 · 72 FR 7559

AD 2007-04-08Published 2007-02-16Effective 2007-03-23

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 inspect the pilot door locking stop-fittings for correct length and, if any incorrect length pilot door locking stop-fittings are found, replace them.

Full official abstract

The FAA adopts a new airworthiness directive (AD) for certain EADS SOCATA airplanes. This AD requires you to inspect the pilot door locking stop-fittings for correct length and, if any incorrect length pilot door locking stop-fittings are found, replace them. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. We are issuing this AD to detect and replace incorrect length pilot door locking stop- fittings. This condition, if not corrected, could result in depressurization of the airplane.

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All SOCATA/Daher TBM 700 directives

View on Federal Register (opens in a new tab) Search DRS manually for AD 2007-04-08 (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index