Summary
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 747-100B SUD, 747-200B, 747-300, 747-400, 747- 400D, and 747SP series airplanes. This AD requires repetitive inspections for cracking of the crease beam and adjacent intercostals, stringers, frames, and skin panels; and related investigative and corrective actions if cracking is found. This AD results from a report indicating that an operator discovered crease beam cracking on two Model 747 airplanes. We are issuing this AD to detect and correct cracking of the crease beam and adjacent structure, which could become large and result in in-flight depressurization and inability of the airframe structure to sustain flight loads.
Directive Details
AD Number
FAA-2006-25518
Document Number
E7-910
Type
Rule
Publication Date
January 25, 2007
Effective Date
March 1, 2007
Affected Manufacturer
Boeing Model 747-100B SUD, 747-200B, 747-300, 747-400, 747-400D, and 747SP Series
Criticality
routine
Emergency
No
Docket ID
Docket No. FAA-2006-25518
Topics
Official Documents
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