Airworthiness Directive

AD 96-20-06 Amendment 39-9772

Federal Aviation Administration · 14 CFR part 39

FR document
96-24651
Amendment
39-9772
Published
1996-09-30
Models covered
1
Last live check
Not yet re-verified
AD

96-20-06

FR doc 96-24651

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

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.

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.

Applies to 1 model in our index