Airworthiness Directive

AD 2023-07-06 88 FR 31148 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2023-10333
Amendment
39-22408
Published
2023-05-16
Effective
2023-06-20
Models covered
1
Last live check
2026-10-03
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AD

2023-07-06

FR doc 2023-10333 · 88 FR 31148

AD 2023-07-06Published 2023-05-16Effective 2023-06-20

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 inspecting the horizontal stabilizer lower center skin panel for corrosion, and reworking, repairing, or replacing the lower center skin panel if necessary.

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 reports of corrosion on the horizontal stabilizer lower center skin panel, including a finding of corrosion where the skin thickness had been substantially reduced, which affected design margins. This AD requires inspecting the horizontal stabilizer lower center skin panel for corrosion, and reworking, repairing, or replacing the lower center skin panel if necessary. 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