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Airworthiness Directives (ADs)

CAA-2005-03-020

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.

Issue Date
2005/03/15
Applicability
747-100B SUD, -300, -400, and -400D Series
Model Number
747
CAA AD Number
CAA-2005-03-020
Aeronautics Authority of Original AD
FAA
Original AD Number
2005-05-08
Effective Date
Subject
To prevent fatigue cracking of the fuselage frame to tension tie joints, which could result in severing of the tension ties and consequent rapid decompression of the airplane fuselage.
Reference Publications (Revision/ATA/SB)
Boeing Special Attention Service Bulletin 747- 53-2483, Revision 1
Remarks
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