Airworthiness Directive

AD 98-11-21 63 FR 29546 Active

Federal Aviation Administration · 14 CFR part 39

Requires a one-time inspection for wear and breakage of wire segments of the individual lighting units of the ceiling and sidewall lights, and replacement of any damaged wiring.

FR document
98-14025
Amendment
39-10546
Published
1998-06-01
Effective
1998-07-06
Models covered
1

Last live check: 2026-08-19

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AD

98-11-21

FR doc 98-14025 · 63 FR 29546

AD 98-11-21Published 1998-06-01Effective 1998-07-06

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 one-time inspection for wear and breakage of wire segments of the individual lighting units of the ceiling and sidewall lights, and replacement of any damaged wiring.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain de Havilland Model DHC-8-102, -103, and -301 series airplanes, that requires a one-time inspection for wear and breakage of wire segments of the individual lighting units of the ceiling and sidewall lights, and replacement of any damaged wiring. This amendment also requires installation of teflon spiral wrap on the wiring of the ceiling and sidewall lights. This amendment is prompted by reports of chafing found on the electrical wiring of the cabin ceiling lighting system. The actions specified by this AD are intended to prevent the possibility of a fire on an airplane due to such chafing and consequent short circuiting, overheating, and smoking of the wires on the aircraft structure.

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Applies to 1 model in our index