Airworthiness Directives (ADs)
87-R44-010
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
- 1998/06/12
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Applicability
- R44
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Model Number
- R44
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CAA AD Number
- 87-R44-010
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 98-12-19
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Effective Date
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Subject
- To detect main rotor blade skin fatigue cracks which originate from the inboard trim tab alignment rivet holes, that could result in failure of the main rotor blade and subsequent loss of control of the helicopter.
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Reference Publications (Revision/ATA/SB)
- SB SB-27A
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Remarks
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Download
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