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Airworthiness Directive

AD 95-08-01 60 FR 17988 Active

Federal Aviation Administration · 14 CFR part 39

FR document
95-8446
Amendment
39-9190
Published
1995-04-10
Effective
1995-05-10
Models covered
1
Last live check
2026-10-03

Printed from https://aircraftdirectives.com/ad/95-08-01 · 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

95-08-01

FR doc 95-8446 · 60 FR 17988

AD 95-08-01Published 1995-04-10Effective 1995-05-10

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 modification of the spoiler system.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Jetstream Model 4101 airplanes, that requires modification of the spoiler system. This amendment is prompted by reports of fatigue failures of the tee fittings of the spoiler bleed nipples. The actions specified by this AD are intended to ensure that the tee fittings do not fail, and subsequently lead to loss of the main system hydraulics.

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All British Aerospace Jetstream 41 directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab)

Applies to 1 model in our index