Airworthiness Directive

AD 2001-19-01 66 FR 47883 Active

Federal Aviation Administration · 14 CFR part 39

FR document
01-23068
Amendment
39-12440
Published
2001-09-14
Effective
2001-10-01
Models covered
1
Last live check
2026-10-03
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AD

2001-19-01

FR doc 01-23068 · 66 FR 47883

AD 2001-19-01Published 2001-09-14Effective 2001-10-01

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 removal of the access panels of the upper wings to determine the manufacturing date of the panels to verify compliance with Model 301 wing specifications, and corrective action, if necessary.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Bombardier Model DHC-8-301 series airplanes. This action requires removal of the access panels of the upper wings to determine the manufacturing date of the panels to verify compliance with Model 301 wing specifications, and corrective action, if necessary. This action is necessary to find and fix panels that do not meet such specifications, which could result in elongation of the attachment holes in the panels due to critical design loads, and consequent reduced structural integrity of the wings. This action is intended to address the identified unsafe condition.

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Applies to 1 model in our index