Airworthiness Directives (ADs)
88-747-304A
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
- 2001/08/27
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Applicability
- 747 Series Airplanes Equipped With General Electric Model CF6-45 or -50 Series Engines or Pratt & Whitney Model JT9D-3, -7, or -70 Series Engines; and 747-E4B (Military) Airplanes
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Model Number
- 747
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CAA AD Number
- 88-747-304A
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Aeronautics Authority of Original AD
- FAA
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Original AD Number
- 2001-16-08
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Effective Date
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Subject
- To prevent fatigue cracking or fracture of the steel attachment fittings of the diagonal brace to the nacelle struts, which could result in failure of a nacelle strut diagonal brace load path and possible separation of the nacelle from the wing
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Reference Publications (Revision/ATA/SB)
- AD 95-10-16,95-13-07,97-20-01R1, 99-09-11, SB 747-54A2196R1
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Remarks
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Download
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