Airworthiness Directive

AD 2016-24-01 81 FR 85116 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2016-28054
Amendment
39-18718
Published
2016-11-25
Effective
2016-12-30
Models covered
1
Last live check
2026-10-03
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AD

2016-24-01

FR doc 2016-28054 · 81 FR 85116

AD 2016-24-01Published 2016-11-25Effective 2016-12-30

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 detect damage on the nacelle firewalls and the terminal block assemblies and to make sure the insulating sleeves are installed and have no damage, and corrective action if necessary.

Full official abstract

We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-102, -103, and -106 airplanes; and Model DHC-8-200 and -300 series airplanes. This AD was prompted by a report of heat damage found on a nacelle firewall after an unsuccessful engine ground start and several events of heat damage found on direct current starter/generator terminal block assemblies. This AD requires an inspection to detect damage on the nacelle firewalls and the terminal block assemblies and to make sure the insulating sleeves are installed and have no damage, and corrective action if necessary. We are issuing this AD to address the unsafe condition on these products.

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Applies to 1 model in our index