Summary
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 737-600, -700, -700C, -800 and -900 series airplanes. This AD requires a one-time general visual inspection of frames between body station (BS) 360 and BS 907 to determine if certain support brackets of the air conditioning (A/C) outlet extrusions are installed; medium- and high-frequency eddy current inspections for cracking of the frames around the attachment holes of the subject brackets; and repair if necessary. This AD also requires installing new, improved fittings for all support brackets of the A/C outlet extrusions between BS 360 and BS 907. This AD results from numerous reports of multiple cracks in the frames around the attachment holes of certain support brackets of the A/C outlet extrusions. We are issuing this AD to prevent frame cracking, which, if not corrected, could lead to a severed frame that, combined with cracking of the skin lap splice above stringer 10, could result in rapid decompression of the airplane.
Directive Details
AD Number
FAA-2007-28283
Document Number
E8-31395
Type
Rule
Publication Date
January 23, 2009
Effective Date
February 27, 2009
Affected Manufacturer
Boeing Model 737-600, -700, -700C, -800 and -900 Series
Criticality
important
Emergency
No
Docket ID
Docket No. FAA-2007-28283
Topics
Official Documents
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