Airworthiness Directives (ADs)
87-B200-041
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
- 1998/10/29
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Applicability
- B200,B300
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Model Number
- B200
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CAA AD Number
- 87-B200-041
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 98-21-35
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Effective Date
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Subject
- To prevent failure of the actuator clevis assembly in the main landing gear caused by fatigue cracking of the original design part, which could result in loss of control of the airplane during landing operations.
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Reference Publications (Revision/ATA/SB)
- MSB 2728 R1
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Remarks
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Download
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