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Airworthiness Directives (ADs)

CAA-2005-04-016

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
2005/04/22
Applicability
747-200B, -200C, -200F, and -400F Series
Model Number
747
CAA AD Number
CAA-2005-04-016
Aeronautics Authority of Original AD
FAA
Original AD Number
2005-08-09
Effective Date
Subject
To find and fix fatigue cracking of the fuselage frame, which could result in reduced structural integrity of the frame and consequent rapid decompression of the airplane.
Reference Publications (Revision/ATA/SB)
ASB 747-53A2504
Remarks
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