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Airworthiness Directives (ADs)

87-747-284

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
1998/10/01
Applicability
747
Model Number
747
CAA AD Number
87-747-284
Aeronautics Authority of Original AD
FAA
Original AD Number
98-20-20
Effective Date
Subject
To detect and correct fatigue cracking of the upper segment of the bulkhead web, which could result in rapid depressurization of the airplane, and consequent reduced controllability of the airplane.
Reference Publications (Revision/ATA/SB)
AD 87-23-10, ASB 747-53A2275R6, SB 747-53-2275R1R2R3R4R5R6
Remarks
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