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Airworthiness Directive

AD 2001-26-23 67 FR 495 Active

Federal Aviation Administration · 14 CFR part 39

Requires replacement of the observer's seat latch assembly with a new, improved seat latch assembly.

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FR document
02-6
Amendment
39-12589
Published
2002-01-04
Effective
2002-02-08
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2001-26-23 · 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

2001-26-23

FR doc 02-6 · 67 FR 495

AD 2001-26-23Published 2002-01-04Effective 2002-02-08

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 observer's seat latch assembly with a new, improved seat latch assembly.

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 replacement of the observer's seat latch assembly with a new, improved seat latch assembly. This action is necessary to prevent the observer's seat from separating from its attachment points in the event of an accident or emergency landing, due to an understrength seat latch assembly. This action is intended to address the identified unsafe condition.

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Applies to 1 model in our index