Airworthiness Directives (ADs)
CAA-2007-05-001
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
- 2007/05/10
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Applicability
- Boeing Model 777-200, -300, and -300ER series airplanes.
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Model Number
- Boeing Model 777-200, 777-300, and 777-300ER Series Airplanes.
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CAA AD Number
- CAA-2007-05-001
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2007-09-04
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Effective Date
- 2007/06/04
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Subject
- To detect and correct corrosion or
cracking of the torque tube and closeout rib fittings that support the inboard end of the inboard
trailing edge flap. Cracking in these components could lead to a fracture, which could result in loss of
the inboard trailing edge flap and consequent reduced controllability of the airplane.
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Reference Publications (Revision/ATA/SB)
- Boeing Service Bulletin 777-57A0048, Revision 1.
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Remarks
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