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Airworthiness Directive

AD 2001-10-05 66 FR 27591 Active

Federal Aviation Administration · 14 CFR part 39

FR document
01-12007
Amendment
39-12231
Published
2001-05-18
Effective
2001-06-22
Models covered
1
Last live check
2026-10-03

Printed from https://aircraftdirectives.com/ad/2001-10-05 · 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

2001-10-05

FR doc 01-12007 · 66 FR 27591

AD 2001-10-05Published 2001-05-18Effective 2001-06-22

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 removing certain foam filters from the cabin ducting installation located below the dado panels on the left- and right-hand sides of the airplane.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Bombardier Model DHC-8-100, -200, and -300 series airplanes, that requires removing certain foam filters from the cabin ducting installation located below the dado panels on the left- and right-hand sides of the airplane. The actions specified by this AD are intended to prevent an increased risk of spreading a fire or failure of the cabin to pressurize adequately if certain foam filters are installed. This action is intended to address the identified unsafe condition.

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All de Havilland DHC-8 Dash 8 directives

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Applies to 1 model in our index