Airworthiness Directive

AD 2019-16-09 84 FR 46434 Superseded

Federal Aviation Administration · 14 CFR part 39

Requires one-time inspections for cracks and damage of the elevator PCU brackets and surrounding area, horizontal stabilizer rear spar, and elevator front spar, and related investigative and corrective actions if necessary.

FR document
2019-18965
Amendment
39-19712
Published
2019-09-04
Effective
2019-10-09
Models covered
1

Last live check: 2026-10-04

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AD

2019-16-09

FR doc 2019-18965 · 84 FR 46434

AD 2019-16-09Published 2019-09-04Effective 2019-10-09

Superseded by 2025-19-05

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 one-time inspections for cracks and damage of the elevator PCU brackets and surrounding area, horizontal stabilizer rear spar, and elevator front spar, and related investigative and corrective actions if necessary.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model DHC-8-400 series airplanes. This AD was prompted by reports of cracked elevator power control unit (PCU) brackets on the horizontal stabilizer rear spar and cracking on the elevator front spar. This AD requires one-time inspections for cracks and damage of the elevator PCU brackets and surrounding area, horizontal stabilizer rear spar, and elevator front spar, and related investigative and corrective actions if necessary. The FAA is issuing this AD to address the unsafe condition on these products.

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Applies to 1 model in our index