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Airworthiness Directive

AD 96-20-06 61 FR 50994 Active

Federal Aviation Administration · 14 CFR part 39

Requires inspection to determine the number of hours time-in- service on the landing gear control unit, and modification of the cable (electrical wiring circuit) of the landing gear control unit.

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FR document
96-24651
Amendment
39-9772
Published
1996-09-30
Effective
1996-11-04
Models covered
1

Last live check: 2026-10-04

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AD

96-20-06

FR doc 96-24651 · 61 FR 50994

AD 96-20-06Published 1996-09-30Effective 1996-11-04

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 inspection to determine the number of hours time-in- service on the landing gear control unit, and modification of the cable (electrical wiring circuit) of the landing gear control unit.

Supersedes an earlier directive. See the official text.

Full official abstract

This amendment supersedes an existing airworthiness directive (AD), applicable to certain Jetstream Model 4101 airplanes, that currently requires inspection to determine the number of hours time-in- service on the landing gear control unit, and modification of the cable (electrical wiring circuit) of the landing gear control unit. That AD was prompted by a report of failure of a micro-switch in the landing gear control unit. This amendment requires installation of a new landing gear control unit. This amendment also expands the applicability of the existing AD to include additional airplanes. The actions specified by this AD are intended to prevent uncommanded retraction of a landing gear, which could adversely affect airplane controllability.

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Applies to 1 model in our index