Airworthiness Directive

AD 98-11-16 63 FR 29098 Active

Federal Aviation Administration · 14 CFR part 39

FR document
98-13820
Amendment
39-10541
Published
1998-05-28
Effective
1998-07-11
Models covered
1
Last live check
2026-10-03
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AD

98-11-16

FR doc 98-13820 · 63 FR 29098

AD 98-11-16Published 1998-05-28Effective 1998-07-11

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 modifying the logic in the failure detection circuits of the landing gear uplock switches.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Dornier Luftfahrt GmbH (Dornier) Models 228-100, 228-101, 228-200, 228-201, 228-202, and 228-212 airplanes. This AD requires modifying the logic in the failure detection circuits of the landing gear uplock switches. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to prevent a false warning indication of landing gear failure because of the design of the landing gear warning system, which could result in incorrect actions from the pilot based on the warning indications.

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All Dornier 228 directives

Applies to 1 model in our index