AD 89-24-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 767-200 Series | Airworthiness Directives; BOEING Model 767 Series Airplanes |
| aircraft | The Boeing Company | 767-300 Series | Airworthiness Directives; BOEING Model 767 Series Airplanes |
| aircraft | The Boeing Company | 767-300F Series | Airworthiness Directives; BOEING Model 767 Series Airplanes |
Unsafe Condition
Binding of the pilot's control wheel due to the Aircraft Integrated Data System (AIDS) position transducer, crank assembly, and rod assembly.
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Required Actions
Deactivate the control wheel AIDS by removing the position transducer, crank assembly, and rod assembly as per Boeing Alert Service Bulletin 767-31A0029. An alternate means of compliance or adjustment may be used if approved by the FAA Manager, Seattle Aircraft Certification Office.
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Compliance Time
Within 45 days after the effective date of this AD (December 1, 1989), unless previously accomplished.
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Affected Aircraft
BOEING Model 767-200 Series, 767-300 Series, 767-300F Series airplanes listed in Boeing Alert Service Bulletin 767-31A0029 dated March 23, 1989.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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