Thank you mrbliaison for your answer. If this practice is OK, do you think long term secondary effects might occured (corrosion, etc.) because of the two dissimilar materials ?
Hi everyone,
I am working in the aircraft heavy maintenance support for deHavilland Canada Dash-8 100/300 airplanes. On the exhaust shroud ("fingernail" in jargon) they have stainless 347 parts (different thickness) riveted to 2024 aluminum parts (different thickness) with monel...