Airworthiness Directive

AD 2001-02-02 66 FR 6454 Active

Federal Aviation Administration · 14 CFR part 39

FR document
01-1659
Amendment
39-12086
Published
2001-01-22
Effective
2001-02-06
Models covered
1
Last live check
2026-10-03
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AD

2001-02-02

FR doc 01-1659 · 66 FR 6454

AD 2001-02-02Published 2001-01-22Effective 2001-02-06

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 repetitive inspections to detect chafing or arcing damage to the cable/wire and fuel tube assemblies on the right hand side of each engine, and replacement with new components, if necessary.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to certain Bombardier Model DHC-8-200, and -300 series airplanes. This action requires repetitive inspections to detect chafing or arcing damage to the cable/wire and fuel tube assemblies on the right hand side of each engine, and replacement with new components, if necessary. This action also provides an optional terminating action for the repetitive inspections required by this AD. This action is necessary to prevent chafing of the cable/wire bundles against the fuel line, which could result in arcing and a consequent fire or explosion. This action is intended to address the identified unsafe condition.

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Applies to 1 model in our index