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Airworthiness Directive

AD 2006-07-02 71 FR 16023 Active

Federal Aviation Administration · 14 CFR part 39

Requires replacing the pressure control valve of the Type 1 emergency door.

Federal Register (opens in a new tab)FAA DRS (opens in a new tab)

FR document
06-2960
Amendment
39-14529
Published
2006-03-30
Effective
2006-05-04
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2006-07-02 · 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

2006-07-02

FR doc 06-2960 · 71 FR 16023

AD 2006-07-02Published 2006-03-30Effective 2006-05-04

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 replacing the pressure control valve of the Type 1 emergency door.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model DHC-8-301, -311, and -315 airplanes. This AD requires replacing the pressure control valve of the Type 1 emergency door. This AD results from reports that the pressure control valve of the Type 1 emergency door is susceptible to freezing. We are issuing this AD to ensure that the pressure control valve does not freeze and prevent the door seal from deflating, which could result in the inability to open the door in an emergency.

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Applies to 1 model in our index