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Airworthiness Directive

AD 95-24-14 60 FR 61647 Active

Federal Aviation Administration · 14 CFR part 39

FR document
95-29329
Amendment
39-9444
Published
1995-12-01
Effective
1995-12-18
Models covered
1
Last live check
2026-10-02

Printed from https://aircraftdirectives.com/ad/95-24-14 · 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

95-24-14

FR doc 95-29329 · 60 FR 61647

AD 95-24-14Published 1995-12-01Effective 1995-12-18

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 eddy current inspections to detect cracking of the pivot tubes in the drag strut of the nose landing gear (NLG), and repair or replacement of any cracked tube with a serviceable or new tube.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to certain de Havilland Model DHC-8 series airplanes. This action requires eddy current inspections to detect cracking of the pivot tubes in the drag strut of the nose landing gear (NLG), and repair or replacement of any cracked tube with a serviceable or new tube. This amendment is prompted by reports that the pivot tubes cracked or failed completely due to fatigue. The actions specified in this AD are intended to prevent such fatigue cracking and subsequent failure of the pivot tube, which could result in a nose gear-up landing.

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All de Havilland DHC-8 Dash 8 directives

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Applies to 1 model in our index