AD 94-14-07 R1
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | BAE Systems (Operations) Limited | Jetstream Model 4101 | Airworthiness Directives; Jetstream Model 4101 Airplanes |
Unsafe Condition
Structural deformation in the elevator control system may occur when maximum load is exerted by the pilot(s) in the event of a jam in the elevator control cables, leading to reduced controllability of the airplane.
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Required Actions
Modify the mounting structure of the elevator controls on the rear pressure bulkhead in accordance with Jetstream Service Bulletin J41-53-012 or J41-53-012-41262A, Revision 1. An alternative method of compliance or adjustment of the compliance time may be approved by the FAA.
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Compliance Time
Within 6 months after August 10, 1994
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Affected Aircraft
BAE Systems (Operations) Limited Model 4101 airplanes as listed in Jetstream Service Bulletin J41-53-012-41262A, Revision 1, dated October 3, 1994.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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