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Airworthiness Directive

AD 2001-22-03 66 FR 54421 Active

Federal Aviation Administration · 14 CFR part 39

FR document
01-26953
Amendment
39-12482
Published
2001-10-29
Effective
2001-12-03
Models covered
1
Last live check
2026-10-03

Printed from https://aircraftdirectives.com/ad/2001-22-03 · 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

2001-22-03

FR doc 01-26953 · 66 FR 54421

AD 2001-22-03Published 2001-10-29Effective 2001-12-03

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 modifying the oxygen flow control valve.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Bombardier Model DHC-8-102, -103, -106, -201, - 202, -301, -311, and -315 series airplanes, that requires modifying the oxygen flow control valve. This action is necessary to ensure that proper oxygen flow will be available to passengers when needed. This action is intended to address the identified unsafe condition.

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Applies to 1 model in our index