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Airworthiness Directive

AD 96-23-11 61 FR 58980 Active

Federal Aviation Administration · 14 CFR part 39

FR document
96-29259
Amendment
39-9816
Published
1996-11-20
Effective
1996-12-05
Models covered
1
Last live check
2026-10-03

Printed from https://aircraftdirectives.com/ad/96-23-11 · 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

96-23-11

FR doc 96-29259 · 61 FR 58980

AD 96-23-11Published 1996-11-20Effective 1996-12-05

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 a one-time test to verify if the disconnect lock of the aileron disconnect control system functions properly, and follow-on actions, if necessary.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to certain Jetstream Model 4101 airplanes. This action requires a one-time test to verify if the disconnect lock of the aileron disconnect control system functions properly, and follow-on actions, if necessary. This amendment is prompted by a report that a disconnect unit of the aileron control system was found to be jammed and unserviceable. The actions specified in this AD are intended to detect and correct such jamming, which could result in reduced controllability of the airplane.

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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