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Airworthiness Directive

AD 95-17-10 60 FR 43707 Active

Federal Aviation Administration · 14 CFR part 39

Requires modifying the central annunciator panel test button circuit.

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FR document
95-20277
Amendment
39-9340
Published
1995-08-23
Effective
1995-10-03
Models covered
1

Last live check: 2026-10-04

Printed from https://aircraftdirectives.com/ad/95-17-10 · 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

95-17-10

FR doc 95-20277 · 60 FR 43707

AD 95-17-10Published 1995-08-23Effective 1995-10-03

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 modifying the central annunciator panel test button circuit.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Jetstream Aircraft Limited (JAL) Jetstream Models 3101 and 3201 airplanes. This action requires modifying the central annunciator panel test button circuit. A report of diode failure in this circuit and subsequent inadvertent engine shutdown on one of the affected airplanes prompted this action. The actions specified by this AD are intended to prevent failure of a diode in the central annunciator panel test button circuit, which could result in inadvertent engine shutdown while in flight if the central annunciator panel test button is pressed.

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All British Aerospace Jetstream 31/32 directives

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Applies to 1 model in our index