Airworthiness Directive

AD 2001-17-23 66 FR 45570 Active

Federal Aviation Administration · 14 CFR part 39

Requires a one-time detailed visual inspection to detect damage of the ladder plates and access cover areas of the upper surface of the wings; repair, if necessary; and installation of new O- ring seals.

FR document
01-21494
Amendment
39-12414
Published
2001-08-29
Effective
2001-10-03
Models covered
1

Last live check: 2026-08-19

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AD

2001-17-23

FR doc 01-21494 · 66 FR 45570

AD 2001-17-23Published 2001-08-29Effective 2001-10-03

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 a one-time detailed visual inspection to detect damage of the ladder plates and access cover areas of the upper surface of the wings; repair, if necessary; and installation of new O- ring seals.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Bombardier Model DHC-8-100, -200, and -300 series airplanes, that requires a one-time detailed visual inspection to detect damage of the ladder plates and access cover areas of the upper surface of the wings; repair, if necessary; and installation of new O- ring seals. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to prevent damage of the upper wing ladder plates, which could result in displacement of the adjacent channel seals and consequent reduced lightning strike protection of the fuel tanks.

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Applies to 1 model in our index