Airworthiness Directive

AD 99-10-04 Amendment 39-11158

Federal Aviation Administration · 14 CFR part 39

FR document
99-11224
Amendment
39-11158
Published
1999-05-05
Models covered
1
Last live check
Not yet re-verified
AD

99-10-04

FR doc 99-11224

AD 99-10-04Published 1999-05-05Effective 1999-06-09

Requires modification of the pulley assemblies of the elevator and rudder control cables on the rear pressure bulkhead.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to all British Aerospace (Jetstream) Model 4101 airplanes, that requires modification of the pulley assemblies of the elevator and rudder control cables on the rear pressure bulkhead. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to prevent failure of the pulley assemblies of the elevator and rudder control cables in the event of an elevator or rudder control cable jam, which could result in reduced controllability of the airplane.

Applies to 1 model in our index