Airworthiness Directives (ADs)
2002-02-013A
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
- 2002/03/08
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Applicability
- Hamilton Sundstrand
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Model Number
- QE
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CAA AD Number
- 2002-02-013A
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2002-05-51
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Effective Date
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Subject
- To prevent blade failure due to corrosion-induced fatigue, which could result in blade separation and possible loss of airplane control.
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Reference Publications (Revision/ATA/SB)
- Hamilton Sundstrand ASB 568F-61-A35R1, Supersedes Emergency AD 2002-04-52(CCAA AD 2002-02-013 )
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Remarks
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