Airworthiness Directive

AD 2014-25-01 79 FR 73808 Superseded

Federal Aviation Administration · 14 CFR part 39

FR document
2014-28923
Amendment
39-18042
Published
2014-12-12
Effective
2015-01-16
Models covered
1

Last live check: 2026-10-04

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AD

2014-25-01

FR doc 2014-28923 · 79 FR 73808

AD 2014-25-01Published 2014-12-12Effective 2015-01-16

Superseded by 2017-19-09 Supersedes 2010-13-04

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 installing a new pivot pin retention mechanism.

Full official abstract

We are superseding Airworthiness Directive (AD) 2010-13-04 for certain Bombardier, Inc. Model DHC-8-400 series airplanes. AD 2010-13- 04 required modifying the nose landing gear (NLG) trailing arm. This new AD requires installing a new pivot pin retention mechanism. This new AD also adds airplanes to the applicability. This AD was prompted by a report of several missing or damaged pivot pin retention bolts. We are issuing this AD to prevent failure of the pivot pin retention bolt, which could result in a loss of directional control or loss of a NLG tire during take-off or landing.

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All de Havilland DHC-8 Dash 8 directives

Applies to 1 model in our index