Summary
The FAA is superseding an existing airworthiness directive (AD) that applies to all Boeing Model 747-100B SUD, 747-300, 747-400, and 747-400D series airplanes; and Model 747-200B series airplanes having a stretched upper deck. The existing AD currently requires repetitively inspecting for cracking or discrepancies of the fasteners in the tension ties, shear webs, and frames at body stations 1120 through 1220, and performing related investigative and corrective actions if necessary. This new AD reduces the repetitive interval for certain inspections. This AD results from new reports of multiple severed adjacent tension ties, in addition to the previous reports of cracked and severed tension ties, broken fasteners, and cracks in the frame, shear web, and shear ties adjacent to tension ties for the upper deck. We are issuing this AD to detect and correct cracking of the tension ties, shear webs, and frames of the upper deck, which could result in rapid decompression and reduced structural integrity of the airplane.
Directive Details
AD Number
FAA-2007-0194
Document Number
07-5794
Type
Rule
Publication Date
November 23, 2007
Effective Date
November 28, 2007
Affected Manufacturer
Boeing Model 747-100B SUD, 747-200B, 747-300, 747-400, and 747-400D Series
Criticality
important
Emergency
No
Docket ID
Docket No. FAA-2007-0194
Topics
Official Documents
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