Airworthiness Directives (ADs)
89-767-155
The aircraft owner or operator shall comply with Airworthiness Directives issued by the CAA or the aeronautics authority of the State of Design (SoD) of the aviation products, appliances and parts, and take all necessary actions thereto.
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Issue Date
- 2000/08/30
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Applicability
- 767-200, -300, and -300F
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Model Number
- 767
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CAA AD Number
- 89-767-155
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2000-17-05
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Effective Date
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Subject
- To detect and correct any failed or partially yielded shear rivets of the elevator power control actuator (PCA) bellcrank assembly, which could result in (1) failure of two bellcrank assemblies on one side of the airplane and consequent movement of the single elevator to a hardover position independent of pilot command, resulting in a significant pitch upset recoverable by the crew; or (2) failure of three bellcrank assemblies on one side and consequent loss of controllability of the airplane.
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Reference Publications (Revision/ATA/SB)
- ASB767-27A0166
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Remarks
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Download
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