Airworthiness Directive

AD 2013-15-06 79 FR 54891 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2014-21770
Amendment
39-17522
Published
2014-09-15
Effective
2014-10-20
Models covered
1
Last live check
2026-10-03
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AD

2013-15-06

FR doc 2014-21770 · 79 FR 54891

AD 2013-15-06Published 2014-09-15Effective 2014-10-20

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 revising the maintenance program to incorporate certain tasks for the electrical wiring interconnection system inspection program.

Full official abstract

We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-102, -103, -106, -201, -202, -301, -311, and --315 airplanes. This AD was prompted by reports of dual alternating current (AC) generator failure during flight. The failure was attributed to wire chafing along the wing lower flap shroud. This AD requires revising the maintenance program to incorporate certain tasks for the electrical wiring interconnection system inspection program. We are issuing this AD to prevent failure of both AC generators due to wire chafing, which could result in loss of power to the anti-icing heaters for the elevator horn, engine inlet, and propeller, and consequent ice accumulation in these areas, which could adversely affect the controllability of the airplane.

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Applies to 1 model in our index