Airworthiness Directive

AD 95-09-04 60 FR 20889 Active

Federal Aviation Administration · 14 CFR part 39

FR document
95-10203
Amendment
39-9207
Published
1995-04-28
Effective
1995-05-30
Models covered
1
Last live check
2026-10-02
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AD

95-09-04

FR doc 95-10203 · 60 FR 20889

AD 95-09-04Published 1995-04-28Effective 1995-05-30

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 an inspection to verify the integrity of the shield grounds for the cable harness of the electronic engine control (EEC), and correction of any discrepancy.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain de Havilland Model DHC-8-100 and -300 series airplanes, that requires an inspection to verify the integrity of the shield grounds for the cable harness of the electronic engine control (EEC), and correction of any discrepancy. This amendment also requires measurement of the electrical resistance of certain shield grounds, and repair, if necessary. This amendment is prompted by a report of an engine flameout after a lightning strike, due to several shields for the cable harness of the EEC not being properly grounded to the airframe. The actions specified by this AD are intended to prevent engine flameout due to insufficient protection of the EEC.

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Applies to 1 model in our index