Battson
Well-Known Member
Hi everyone,
I am looking for some wisdom, from experienced builders:
When you assemble alloy wing parts (say 2024-T3 for instance), is it important that all parts which are permenantly afixed together receive primer between them. My example is the spar cap strips and spar C-section. Will priming over the assembed spar give the same (and adequate) protection against intra-spar corrosion, compared to painting the parts seperately then assembling them?
I am no expert, but see advantages and disadvantages each way:
I appreciate any wisdom, experience, or advice you can share. Thanks.
I am looking for some wisdom, from experienced builders:
When you assemble alloy wing parts (say 2024-T3 for instance), is it important that all parts which are permenantly afixed together receive primer between them. My example is the spar cap strips and spar C-section. Will priming over the assembed spar give the same (and adequate) protection against intra-spar corrosion, compared to painting the parts seperately then assembling them?
I am no expert, but see advantages and disadvantages each way:
- Priming individual parts gives protection to the surfaces in contact, but increases weight, and permanent fixtures (e.g. rivets after priming) introduce unprimed ingress points for corrosion.
- Priming the assembled spar provides a single unbroken layer of protection, in theory, but leaves the internal mating surfaces exposed and in contact with each other, and corrosion could develop in there.
I appreciate any wisdom, experience, or advice you can share. Thanks.