Airworthiness Directives (ADs)
85-SD3-027
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
- 1996/11/29
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Applicability
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Model Number
- SD3-60
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CAA AD Number
- 85-SD3-027
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 96-22-09
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Effective Date
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Subject
- To detect and correct stress corrosion or cracking of the bland nut on the shock absorber of the main landing gear (MLG) in a timely manner and consequent reduced structural integrity of the nut, which could result in separation of the shock absorber cyli
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Reference Publications (Revision/ATA/SB)
- SD360-32-34
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Remarks
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Download
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