Airworthiness Directive

AD 2024-12-06 89 FR 58061 Active

Federal Aviation Administration · 14 CFR part 39

Requires a visual inspection of the fuselage front and rear spar frames, an ultrasonic test if applicable, other specified actions, and repair if necessary.

FR document
2024-15657
Amendment
39-22770
Published
2024-07-17
Effective
2024-08-21
Models covered
1

Last live check: 2026-10-04

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AD

2024-12-06

FR doc 2024-15657 · 89 FR 58061

AD 2024-12-06Published 2024-07-17Effective 2024-08-21

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 visual inspection of the fuselage front and rear spar frames, an ultrasonic test if applicable, other specified actions, and repair 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 moisture in the wing- to-fuselage joint, between the mating front spar and rear spar frame segments. This AD requires a visual inspection of the fuselage front and rear spar frames, an ultrasonic test if applicable, other specified actions, and repair if necessary. The FAA is issuing this AD to address the unsafe condition on these products.

More directives for de Havilland DHC-8 Dash 8

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All de Havilland DHC-8 Dash 8 directives

Applies to 1 model in our index