Airworthiness Directive

AD 2004-19-07 69 FR 56682 Active

Federal Aviation Administration · 14 CFR part 39

FR document
04-21174
Amendment
39-13801
Published
2004-09-22
Effective
2004-10-27
Models covered
1
Last live check
2026-10-03
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AD

2004-19-07

FR doc 04-21174 · 69 FR 56682

AD 2004-19-07Published 2004-09-22Effective 2004-10-27

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 electrical power circuit.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Bombardier Model DHC-8-102 airplanes, that requires modification of the electrical power circuit. This action is necessary to prevent component failure in the radar indicator, resulting in an overcurrent condition and consequent overheating or burning of an internal component or the ribbon cable. This could lead to smoke in the cockpit, resulting in incapacitation of the flight crew and loss of control of the airplane. This action is intended to address the identified unsafe condition.

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Applies to 1 model in our index