Use of 1100-F "A" Aluminum Rivets - Aircraft engineering aluminium 1100 aluminum 1100 aircraft materials
Sep 30, 2005 · According to the note, I should avoid 1100F. 1100 alloy is a minimum 99% pure aluminum. In what way is it incompatible with 2000 or 7000 aluminums? Is this a corrosion issue? I understand "A" rivets are relatively weak at 9.5 ksi shear, but that is not an issue for this application.
BVF.. That table [note] does NOT include 1100 ["A"] rivets it is for 5056 ["B"] rivets only. And, Yes it is a "dissimilarity" issue aluminium 1100 aluminum 1100 aircraft materials not to ment aluminium 1100 aluminum 1100 aircraft materialsBrent, I would instl the rivet with sealant to prevent moisture from getting into the joint. This would be to protect the 7075. Another thought is aluminium 1100 aluminum 1100 aircraft materialsThanks, guys. Wil Not to be pedantic, but the note clearly says not to use 1100F rivets in 2000 or 7000 series aluminum. Should I just interpret t aluminium 1100 aluminum 1100 aircraft materialsBrent, I can get you this info tomorrow. Working landing gear out of state this week.BVF aluminium 1100 aluminum 1100 aircraft materials The liaison Hdbk (Ref page 60.2.2) I have access to DOES NOT include 1100 alloy rivets in this statememt aluminium 1100 aluminum 1100 aircraft materials only 5056. Regards, Wil TaylorThanks, Wil. That's really interesting. I've checked the three books I can find in our office. The 1986 edition has no note at all. In 1989, the no aluminium 1100 aluminum 1100 aircraft materialsThe info that I have is to use AD type rivets for 2024 and E for 7075. This will minimize galvanic corrosion. Now, this issue with this is that bu aluminium 1100 aluminum 1100 aircraft materialsAPI 521 Tw (vessel wall temperature) - Safety Relief aluminium 1100 aluminum 1100 aircraft materialsJan 03, 2008inconel 718 threaded
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