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Airworthiness Directives (ADs)

87-747-270A

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
2000/06/09
Applicability
747-100,-200,-300,747SR,and 747SP series
Model Number
747
CAA AD Number
87-747-270A
Aeronautics Authority of Original AD
FAA
Original AD Number
2000-10-23
Effective Date
Subject
To detect and correct fatigue cracking of the longeron splice fittings at stringer 11, which could result in reduced controllability of the horizontal stabilizer.
Reference Publications (Revision/ATA/SB)
ASB 747-53A2410R2,SB 747-53A2410R3
Remarks
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