Airworthiness Directive

AD 98-14-04 63 FR 35792 Active

Federal Aviation Administration · 14 CFR part 39

FR document
98-17418
Amendment
39-10638
Published
1998-07-01
Effective
1998-08-05
Models covered
1
Last live check
2026-10-03
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AD

98-14-04

FR doc 98-17418 · 63 FR 35792

AD 98-14-04Published 1998-07-01Effective 1998-08-05

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 modification of the lever assembly of the roll disconnect system.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain de Havilland Model DHC-8-100, -200, and -300 series airplanes, that requires modification of the lever assembly of the roll disconnect system. This amendment is prompted by mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to prevent uncommanded disconnects of the roll control system, which could result in a limited degree of roll control and consequent reduced controllability of the airplane.

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Applies to 1 model in our index