Airworthiness Directives (ADs)
CAA-2004-08-012
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
- 2004/08/18
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Applicability
- 767-200, -300, and -300F
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Model Number
- 767
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CAA AD Number
- CAA-2004-08-012
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2004-16-12
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Effective Date
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Subject
- To prevent fatigue cracking in primary strut structure, which could result in separation of the strut and engine from the airplane.
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Reference Publications (Revision/ATA/SB)
- Supersede AD 2001-02-07; AD 2001-06-12(CCAA AD 90-767-164); and AD 2001-08-23(CCAA AD 90-767-167).
Ref. SB 767-29-0057, 767-54-0069, 767-54-0080, 767-54-0081, 767-54-0083, 767-54-0088, 767-54A0094, 767-57-0053, and 767-57A0070.
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Remarks
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