Airworthiness Directives (ADs)
CAA-2004-11-008修訂
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
- 2007/03/01
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Applicability
- Raytheon Aircraft Company 65, 90, 99, 100, 200, and 1900 Series Airplanes, and Models 70 and 300 Airplanes
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Model Number
- Raytheon Aircraft Company 65, 90, 99, 100, 200, and 1900 Series Airplanes, and Models 70 and 300 Airplanes
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CAA AD Number
- CAA-2004-11-008修訂
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2004-23-02 Correction
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Effective Date
- 2004/12/23
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Subject
- To detect and correct cracks in the NLG fork, which could result in reduced structural integrity and inability of the NLG fork to carry design limit and ultimate loads. The reduced residual strength may cause separation failure of the NLG fork, which could result in loss of control of the airplane during take off, landing, and taxi operations.
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Reference Publications (Revision/ATA/SB)
- Supersedes AD 87-22-01 R1(CCAA AD 77-B200-015)
Ref. Raytheon Aircraft Company Mandatory Service Bulletin SB 32-2102, Revision 7, Revised: July, 2003.
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Remarks
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