Airworthiness Directives (ADs)
CAA-2008-12-007
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.
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Issue Date
- 2008/12/23
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Applicability
- Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-
200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, and 747SR series airplanes.
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Model Number
- Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-
200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, and 747SR Series Airplanes
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CAA AD Number
- CAA-2008-12-007
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2008-25-07
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Effective Date
- 2009/01/15
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Subject
- To detect and correct cracks or fractures of the primary
structural and fail-safe load paths of the inboard and outboard trailing edge flaps, which could result
in the loss of a flap during takeoff or landing, reducing flightcrew ability to maintain the safe flight
and landing of the airplane.
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Reference Publications (Revision/ATA/SB)
- Boeing Alert Service Bulletin 747-57A2323.
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Remarks
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