Summary
We are adopting a new airworthiness directive (AD) for certain Boeing Model 737-100, -200, -300, -400, and -500 series airplanes. This AD requires repetitive inspections for fatigue cracking in the longitudinal floor beam web, upper chord, and lower chord located at certain body stations, and repair if necessary. This AD results from several reports of cracks in the center wing box longitudinal floor beams, upper chord, and lower chord. We are issuing this AD to detect and correct fatigue cracking of the upper and lower chords and web of the longitudinal floor beams, which could result in rapid loss of cabin pressure.
Directive Details
AD Number
FAA-2007-0224
Document Number
E8-3810
Type
Rule
Publication Date
March 4, 2008
Effective Date
April 8, 2008
Affected Manufacturer
Boeing Model 737-100, -200, -300, -400, and -500 Series
Criticality
important
Emergency
No
Docket ID
Docket No. FAA-2007-0224
Topics
Official Documents
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