Airworthiness Directives (ADs)

Aviation Industry

CAA-2016-01-002

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: 2016/01/22

Applicability: This AD applies to The Boeing Company Model 747-100, -100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, and 747SR series airplanes; certificated in any category.

Model Number: The Boeing Company Model 747-100, -100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, and 747SR series airplanes.

CAA AD Number: CAA-2016-01-002

Aeronautics Authority of Original AD: FAA

Original AD Number: 2016-01-04

Effective Date: 2016/02/17

Subject: FUSELAGE - Body Station 2231 Frame Inner Chord Crack - Inspection/ Repair

Reference Publications (Revision/ATA/SB): (i) This AD replaces FAA AD 2005-01-09(CAA-2005-01-005). (ii) Boeing Alert Service Bulletin 747-53A2494, Revision 1, dated January 9, 2015.

Remarks

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