Airworthiness Directives (ADs)
CAA-2004-03-002(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
- 2004/03/08
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Applicability
- 767
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Model Number
- 767
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CAA AD Number
- CAA-2004-03-002(已有後續修訂版)
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2004-05-10
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Effective Date
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Subject
- To prevent fatigue cracking of the aft pressure bulkhead, which could result in rapid depressurization of the airplane and possible damage or interference with the airplane control systems that penetrate the bulkhead, and consequent loss of controllability of the airplane.
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Reference Publications (Revision/ATA/SB)
- Supersedes AD 88-19-03 R1(CCAA AD 77-767-041)
Ref. SB 767-53-0026, R1; ASB 767-53A0026R5.
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Remarks
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