Airworthiness Directives (ADs)
2002-05-001
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
- 2002/05/07
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Applicability
- 205A, 205A-1, 205B, 212, 412, 412EP, and 412CF helicopters with a tail rotor blade
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Model Number
- Bell 412
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CAA AD Number
- 2002-05-001
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2002-09-04
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Effective Date
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Subject
- To prevent loss of the forward tip weight retention block (tip block) or aft tip closure (tip closure), loss of the tail rotor blade, and subsequent loss of control of the helicopter.
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Reference Publications (Revision/ATA/SB)
- ASB 205-00-80, 205B-00-34, 212-00-111, 412-00-106, and 412CF-00-13, all Revision A.
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Remarks
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Download
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