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Airworthiness Directive

AD 2006-24-06 71 FR 68997 Active

Federal Aviation Administration · 14 CFR part 39

FR document
06-9428
Amendment
39-14835
Published
2006-11-29
Effective
2007-01-03
Models covered
1
Last live check
2026-10-01

Printed from https://aircraftdirectives.com/ad/2006-24-06 · 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

2006-24-06

FR doc 06-9428 · 71 FR 68997

AD 2006-24-06Published 2006-11-29Effective 2007-01-03

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 actions that are intended to address the unsafe condition described in the MCAI.

Full official abstract

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as ripped pressure lines between Airbox-Carburetor-Differential fuel pressure sensor. We are issuing this AD to require actions that are intended to address the unsafe condition described in the MCAI.

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All Stemme S10/S12 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