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Airworthiness Directive

AD 2017-15-11 82 FR 35634 Active

Federal Aviation Administration · 14 CFR part 39

Requires replacement of the MLG retraction actuator rod-ends on both MLG assemblies.

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FR document
2017-15476
Amendment
39-18971
Published
2017-08-01
Effective
2017-09-05
Models covered
1

Last live check: 2026-10-04

Printed from https://aircraftdirectives.com/ad/2017-15-11 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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AD

2017-15-11

FR doc 2017-15476 · 82 FR 35634

AD 2017-15-11Published 2017-08-01Effective 2017-09-05

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 replacement of the MLG retraction actuator rod-ends on both MLG assemblies.

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 undamped main landing gear (MLG) extension in-service. This AD requires replacement of the MLG retraction actuator rod-ends on both MLG assemblies. We are issuing this AD to address the unsafe condition on these products.

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Applies to 1 model in our index