Airworthiness Directive

AD 2026-08-07 91 FR 23009 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2026-08303
Amendment
39-23315
Published
2026-04-29
Effective
2026-06-03
Models covered
1
Last live check
2026-10-03
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AD

2026-08-07

FR doc 2026-08303 · 91 FR 23009

AD 2026-08-07Published 2026-04-29Effective 2026-06-03

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 replacing bushings and installing new washers on the elevator PCU arm fitting assembly, installing doublers at the front spar of the elevator structure assembly, replacing horizontal stabilizer rear spar elevator PCU…

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for certain De Havilland Aircraft of Canada Limited Model DHC-8-401 and - 402 airplanes. This AD was prompted by multiple in-service reports of cracks in elevator power control unit (PCU) brackets (fittings) and the elevator front spar. This AD requires replacing bushings and installing new washers on the elevator PCU arm fitting assembly, installing doublers at the front spar of the elevator structure assembly, replacing horizontal stabilizer rear spar elevator PCU fittings, and applicable on-conditions actions. The FAA is issuing this AD to address the unsafe condition on these products.

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All de Havilland DHC-8 Dash 8 directives

Applies to 1 model in our index