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Airworthiness Directive

AD 2001-13-21 66 FR 35535 Active

Federal Aviation Administration · 14 CFR part 39

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FR document
01-16738
Amendment
39-12303
Published
2001-07-06
Effective
2001-08-10
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2001-13-21 · 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

2001-13-21

FR doc 01-16738 · 66 FR 35535

AD 2001-13-21Published 2001-07-06Effective 2001-08-10

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 repair of the flight deck angle.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Bombardier Model DHC-8-102, -103, and -301 series airplanes, that requires repair of the flight deck angle. The actions specified by this AD are intended to prevent the flight deck angle from interfering with the clevis of the roll control disconnect cable, which could lead to an uncommanded disconnection of the roll control, resulting in reduced controllability of the airplane. This action is intended to address the identified unsafe condition.

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All de Havilland DHC-8 Dash 8 directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (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