Airworthiness Directives (ADs)
CAA-2008-11-007
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
- 2008/11/18
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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-2008-11-007
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2008-22-17
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Effective Date
- 2008/12/19
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Subject
- To detect and correct failed carriage
spindles or aft links of the inboard or outboard trailing edge flaps. Such failure could cause the flap to
depart the airplane, reducing the flightcrew's ability to maintain the safe flight and landing of the
airplane.
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Reference Publications (Revision/ATA/SB)
- This AD supersedes FAA AD 90-17-19(CAA-77-747-085B). Ref. Boeing Service Bulletin 747-27-2280 R3, Boeing Service Bulletin 747-27-2280 R6 and Boeing Service Bulletin 747-27-2371.
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Remarks
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