mikeone
Aerospace
- Jul 20, 2002
- 4
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 rivets (MS 20615M--).
Most of the technicians are using a steel washer under the rivet bucked (formed) head "for strenght" (after bucking the rivet, the washer rests under the rivet formed head).
Is this a standard practice or a bad practice (no separator, like sealant is used between the two different materials) ? Can anyone help me with some information ?
Thank you in advance.
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 rivets (MS 20615M--).
Most of the technicians are using a steel washer under the rivet bucked (formed) head "for strenght" (after bucking the rivet, the washer rests under the rivet formed head).
Is this a standard practice or a bad practice (no separator, like sealant is used between the two different materials) ? Can anyone help me with some information ?
Thank you in advance.