Here it is:
http://rgl.faa.gov/Regulatory_and_Guidance.../2006-15-15.pdf
http://rgl.faa.gov/Regulatory_and_Guidance...ight=2006-15-15
Incorporates by reference the various revisions of the SB (which aren't online).
Thank you very much for posting that link.
The AD refers specifically to the issue in question in the section entitled, "Installation of Additional Wiring Protection:"
For airplanes in Configuration 4, as defined in Boeing Alert Service Bulletin MD80-29A070,
Revision 1, dated July 28, 2005: Within 18 months after the effective date of this AD, install
additional protective sleeving on the upper portion of the auxiliary hydraulic pump wire assembly in
accordance with the procedures under Configuration 4 in the Accomplishment Instructions of the
service bulletin.
Since I am not a mechanic, I am not sure if it is possible, but does anyone know where the "Accomplishment Instructions" might be viewable? I'd love to see how the specifics of the wiring attachment to the wheel well assembly were described in the original AD.