SAE AS7475
Superseded
View Superseded by
BOLTS AND SCREWS, WORK-STRENGTHENED ALLOY, CORROSION AND HEAT RESISTANT Forged Head, Roll Threaded After Aging
Hardcopy , PDF
English
01-17-1991
03-01-1997
| DocumentType |
Standard
|
| Pages |
26
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy |
This procurement specification covers aircraft quality bolts and screws made from a corrosion and heat resistant, work-strengthened, cobalt-chromium-nickel alloy of the type identified under the Unified Numbering System as UNS R30159, and of 260 000 psi tensile strength at room temperature, with maximum test temperature of parts at 1200°F.
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