Airworthiness Directives (ADs)
CAA-2005-05-011
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
- 2005/05/24
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Applicability
- 747-100, -100B, -100B SUD, - 200B, -200C, -300, -400, and -400D series
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Model Number
- 747
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CAA AD Number
- CAA-2005-05-011
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2005-10-18
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Effective Date
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Subject
- To detect and correct stress corrosion cracking of the stop support fittings of the MEDs, which could result in damage to the adjacent forward edge frame of the door and consequent loss of a MED and rapid decompression of the airplane.
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Reference Publications (Revision/ATA/SB)
- Supersedes AD 98-26-13(CCAA AD 88-747-291)
Ref. SB 747-53-2358, SB 747-53-2358R1 and Boeing Special Attention SB 747-53-2485.
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Remarks
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