bbs...
In aerospace material... and associated fabrication process callouts... usually get VERY specific, to ensure consistent/repeatable material as intended, like this...
Alloy/temper [initial] + temper [during/after any follow-on heat-treatments or processing-forming-etc...
Heat treatment and NDI requirements [must include explicit specifications how-to]
Exact procurement specification + type, class, etc...
FORM [plate, bare-sheet, clad-sheet, extrusion, forging, casting, etc...]
Special qualities and/or inspection requirements [ultrasonic inspection, FPI, MPI, etc... to meet specific expectations... including destructive testing and metallurgical examinations if/as required.
NOTE. Material-lab Certifications MUST validate material meets physical, chemistry, metallurgical requirements.
Raw-stock definition
Plate, sheet strip, etc = Thickness x Width x Length [min-to-max allowed]
Extrusion = profile/shape x Length [min-to-max allowed]
Drawn shape = cross-section X Length [min-to-max allowed]
Billet
etc...
NOTE.
IF optional materials/tempers/forms/etc are appropriate/acceptable then each of these options must be fully defined, as noted.
NOTHING is ever left to amateur guess-work or imagination or experience or 'best shop practices'... unless there is a very clear SOP on how to 'proceed'.
NOTE. FAA considers manufacturing parts [replacement and repair] is so critical, that specialized training is required with sign-off... since average mechanics simply don't understand how materials + fabrication processes critically affect airworthiness of finished parts. AC43-18 Fabrication of Aircraft parts by Maintenance Personnel...
Regards, Wil Taylor
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