Airworthiness Directives (ADs)
CAA-2005-10-002
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.
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Issue Date
- 2005/10/07
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Applicability
- Boeing Model 747-100, -200B, -200F, - 200C, -100B, -300, -100B SUD, -400, -400D, and -400F Series Airplanes; and Model 747SR Series Airplanes
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Model Number
- 747
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CAA AD Number
- CAA-2005-10-002
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2005-20-18
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Effective Date
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Subject
- To prevent cracking and other damage of the actuator attach fittings of the trailing edge flaps, which could result in abnormal operation or
retraction of a trailing edge flap, and possible loss of controllability of the airplane.
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Reference Publications (Revision/ATA/SB)
- Supersedes AD 2001-13-12(CCAA AD 90-747-359) and AD 2003-08-11(CCAA AD 2003-04-018).
Ref. Boeing Alert Service Bulletin 747–57A2316, Boeing Service Bulletin 747–57A2310R1 and Boeing Service Bulletin 747–57A2310R2.
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Remarks
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