Airworthiness Directives (ADs)
CAA-2005-01-016(已有後續修訂版)
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
- 2005/01/20
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Applicability
- Beech 100, 200, and 300 Series
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Model Number
- B200, B300
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CAA AD Number
- CAA-2005-01-016(已有後續修訂版)
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2005-01-18
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Effective Date
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Subject
- To detect and correct any cracked fuselage stringers in the rear pressure bulkhead area, which could result in structural damage to the fuselage. This damage could lead to failure of the fuselage with potential loss of control of the airplane
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Reference Publications (Revision/ATA/SB)
- Supersedes AD 93-25-07(CCAA AD 82-B200-027).
Ref. Raytheon Mandatory Service Bulletin SB 53-2472, Rev. 4
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Remarks
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Download
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