Since there were no floods today things went a little smoother. Hotter, but smoother. There are two stringers on the left aft wing that support the trailing edge skin that need replacement, so I've been conjuring up a method to replace them without disassembling the entire aft wing.

This first one isn't hard to access--it's on the trailing edge just above where the flap normally rests when retracted. The problem is that Boeing didn't design the stringers to be removed, and there is a three foot section missing. The first photo is of the skin joint that the removed stringer attaches to:
Here is a little overview of the general area that needs attention. Someone removed the discrepant stringer sometime before I got involved, and I'm not sure how he got it out without cutting it into sections.
The missing stringer goes through three bays.
An interesting aspect of working on this airplane is the use of production splices on stringers, longerons, etc throughout the machine. This splice is located just outboard of the area I'm working in, and it is quite the example of haste on the assembly line. It's strong, but it's also ugly:
These are scattered throughout the wing and fuselage wherever a splice was needed. I am used to being around Boeing products of modern construction that have neat, well made structural components, and when I stumble on things like this I have to remember how hard the production lines worked to crank warplanes out for the boys overseas.
Alan, if you would like to come down again here is the little job I would LOVE to give you (or any other unsuspecting soul):
This little section of stringer is buried just behind the intercooler vent ports aft of #2. You can see the vents forward of the corroded stringer. I decided to learn as I go on the trailing edge stringer so I have a little experience for this one. It is going to be a bear to work for an old fossil like me.
Scott