I responded by PM, but here is some of the information I provided for those interested.
Here is a good comment on intergranular corrosion -
http://www.corrosion-doctors.org/Forms/intergranular.htm
Here is a good comment on exfoliation corrosion -
http://www.corrosion-doctors.org/Forms/exfoliation.htm
http://www.metalimprovement.com/exfoliation_corrosion.php
http://www.alu-info.dk/HTML/alulib/modul/A00121.htm
More general reference
http://www.boeing.com/commercial/aeromagazine/aero_07/corrosn.html
This is a nice reference -
http://www.engr.ku.edu/~rhale/ae510/corrosion.pdf
Corrosion essentially initiates on the grain boundaries and spreads across grains. The grain boundaries have a higher chemical (electrochemical) potential because of the mismatch of crystal lattices.
In solidification, grains nucleate more readily at phases or intermetallic of higher melting temperatures, e.g. carbides or silicides of metals. Because of the extra energy, grain boundaries are the last parts of the grains to form. During that time (milliseconds), atoms of different elements diffuse and concentrate on the grain boundaries, which is why grain boundaries can have significantly different chemical stoichiometry than the nominal composition, and it is for this reason that rapid quenching is desirable during welding or casting, otherwise subsequent heat treating is necessary.
are you asking me what the heat treatment is of my 2024?
I was wondering about the temper. See - http://www.wisoven.com/heatreat.htm (Look at comments on T4, T5 and T6)
With regard to 2024 - see http://www.auf.asn.au/scratchbuilder/metals.html#aluminium_alloys
This might be of use -
http://www.aviationmetals.net/aluminum_sheet.html
I'll have to get back later with more information on IGSCC in Al alloys.