Are these the AC docs you are referring to? If so, I didn't see anything on rivets and their installation. 1B is over 600 pages and would not upload.Please refer to AC 43.13-1B & AC 43.13-2B - Aircraft Inspection, Repair & Alterations: Acceptable Methods, Techniques and Practices, section 4. All info can be found online.
I am not familiar with FWIW, I used the aircraft rivets that I have access to. The aluminum alloys used in boat building probably differ from those used in aircraft fabrication. A softer rivet. It’s probably recommended in boat fabrication.FWIW tin boat mfg'rs recommend Type A for repairing tin boats.
I am not familiar with FWIW, I used the aircraft rivets that I have access to. The aluminum alloys used in boat building probably differ from those used in aircraft fabrication. A softer rivet. It’s probably recommended in boat fabrication.
I noticed the Type A are the 1100 designation you have referred to in other posts (softer than parent material).FWIW tin boat mfg'rs recommend Type A for repairing tin boats.
Referring to the material that is being drilled and riveted together as parent material is probably the wrong Termanology. My thought on the subject was that the act of bucking, a Harder, rivet, or several in a given area with minimal edge distance and pitch, could possibly have the undesired effect of work, hardening that area, making it more susceptible to stress cracks.I noticed the Type A are the 1100 designation you have referred to in other posts (softer than parent material).