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Airworthiness Directive

AD 94-14-07 R1 60 FR 32901 Active

Federal Aviation Administration · 14 CFR part 39

Requires modification of the mounting structure of the elevator controls on the rear pressure bulkhead.

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FR document
95-14053
Amendment
39-9265
Published
1995-06-26
Effective
1995-07-26
Models covered
1

Last live check: 2026-10-04

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AD

94-14-07 R1

FR doc 95-14053 · 60 FR 32901

AD 94-14-07 R1Published 1995-06-26Effective 1995-07-26

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 mounting structure of the elevator controls on the rear pressure bulkhead.

Full official abstract

This amendment revises an existing airworthiness directive (AD), applicable to all Jetstream Model 4101 airplanes, that currently requires modification of the mounting structure of the elevator controls on the rear pressure bulkhead. That AD was prompted by results of a structural analysis which indicate that certain structure in the elevator control system may be subject to deformation when maximum load is exerted by the pilot(s) in the event of a jam in the elevator control cables. The actions specified in that AD are intended to prevent reduced controllability of the airplane due to structural deformation in the elevator control system. This amendment limits the applicability of the rule.

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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) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index