Airworthiness Directive

AD 2024-02-02 89 FR 11713 Active

Federal Aviation Administration · 14 CFR part 39

Requires inspecting the horizontal stabilizer to vertical joint for gaps and bending of the saddle washer and adjacent washers, and replacing parts if necessary.

FR document
2024-03081
Amendment
39-22666
Published
2024-02-15
Effective
2024-03-21
Models covered
1

Last live check: 2026-10-04

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AD

2024-02-02

FR doc 2024-03081 · 89 FR 11713

AD 2024-02-02Published 2024-02-15Effective 2024-03-21

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 inspecting the horizontal stabilizer to vertical joint for gaps and bending of the saddle washer and adjacent washers, and replacing parts 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 that the saddle washer (radius filler) for the front and rear spar joints may have been incorrectly manufactured for several years. This AD requires inspecting the horizontal stabilizer to vertical joint for gaps and bending of the saddle washer and adjacent washers, and replacing parts 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