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Airworthiness Directive

AD 2018-23-04 84 FR 2707 Active

Federal Aviation Administration · 14 CFR part 39

Requires an inspection of the auto ignition system and applicable rectification.

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

FR document
2019-00858
Amendment
39-19490
Published
2019-02-08
Effective
2019-03-15
Models covered
1

Last live check: 2026-10-04

Printed from https://aircraftdirectives.com/ad/2018-23-04 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

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AD

2018-23-04

FR doc 2019-00858 · 84 FR 2707

AD 2018-23-04Published 2019-02-08Effective 2019-03-15

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 an inspection of the auto ignition system and applicable rectification.

Full official abstract

We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model DHC-8-102, -103, and -106 airplanes; Model DHC- 8-200 series airplanes; and Model DHC-8-300 series airplanes. This AD was prompted by a report that a certain modification to the auto relight system is incompatible with a certain beta lockout system modification and could result in de-activation of the auto ignition feature of the No. 2 engine. This AD requires an inspection of the auto ignition system and applicable rectification. We are issuing this AD to address the unsafe condition on these products.

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Applies to 1 model in our index