Airworthiness Directive

AD 2015-04-08 80 FR 15149 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2015-05033
Amendment
39-18110
Published
2015-03-23
Effective
2015-04-27
Models covered
1
Last live check
2026-10-03
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AD

2015-04-08

FR doc 2015-05033 · 80 FR 15149

AD 2015-04-08Published 2015-03-23Effective 2015-04-27

Supersedes 2014-06-08

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

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 a terminating action modification.

Full official abstract

We are superseding Airworthiness Directive (AD) 2014-06-08 for certain Bombardier, Inc. Model DHC-8-100, -200, and -300 series airplanes. AD 2014-06-08 required repetitive functional checks of the nose and main landing gear, and corrective actions if necessary; and also provided optional terminating action modification for the repetitive functional checks. This new AD requires a terminating action modification. This AD was prompted by a report that the emergency downlock indication system (EDIS) had given a false landing gear down- and-locked indication and a determination that a terminating action modification is necessary to address the identified unsafe condition. We are issuing this AD to detect and correct a false down-and-locked landing gear indication, which, on landing, could result in possible collapse of the landing gear.

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All de Havilland DHC-8 Dash 8 directives

Applies to 1 model in our index