Airworthiness Directive

AD 99-10-04 64 FR 24033 Active

Federal Aviation Administration · 14 CFR part 39

FR document
99-11224
Amendment
39-11158
Published
1999-05-05
Effective
1999-06-09
Models covered
1
Last live check
2026-10-03
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AD

99-10-04

FR doc 99-11224 · 64 FR 24033

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

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 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.

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  2. AD 2009-10-02 Airworthiness Directives; BAE Systems (Operations) Limited (Jetstream) M... 2009-05-07
  3. AD 2009-02-07 Airworthiness Directives; BAE Systems (Operations) Limited (Jetstream) M... 2009-02-26
  4. AD 2008-18-02 Airworthiness Directives; BAE Systems (Operations) Limited (Jetstream) M... 2009-02-20
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All British Aerospace Jetstream 41 directives

Applies to 1 model in our index