Airworthiness Directive

AD 2019-12-17 84 FR 32255 Active

Federal Aviation Administration · 14 CFR part 39

Requires inspecting the two balance weights and the two hinge arms on each elevator spring tab, and corrective actions if necessary.

FR document
2019-14412
Amendment
39-19672
Published
2019-07-08
Effective
2019-08-12
Models covered
1

Last live check: 2026-10-04

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AD

2019-12-17

FR doc 2019-14412 · 84 FR 32255

AD 2019-12-17Published 2019-07-08Effective 2019-08-12

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 two balance weights and the two hinge arms on each elevator spring tab, and corrective actions if necessary.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model DHC-8-102, -103, and -106 airplanes; Model DHC-8-200 series airplanes; and Model DHC-8-300 series airplanes. This AD was prompted by the reported loss of an elevator spring tab balance weight prior to takeoff. This AD requires inspecting the two balance weights and the two hinge arms on each elevator spring tab, and corrective actions if necessary. The FAA is issuing this AD to address the unsafe condition on these products.

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