SAE AMS7466B
Current
The latest, up-to-date edition.
Bolts and Screws Nickel Alloy, Corrosion and Heat Resistant, Upset Headed, Roll Threaded, Fatigue Resistant
01-10-1993
1. SCOPE
2, APPLICABLE DOCUMENTS
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. ACKNOWLEDGMENT
7. REJECTIONS
8. NOTES
Describes aircraft-quality bolts and screws made from a corrosion and heat resistant nickel alloy.
DocumentType |
Standard
|
PublisherName |
SAE International
|
Status |
Current
|
SupersededBy | |
Supersedes |
MIL-STD-1891 Base Document:1992 | BOLTS AND SCREWS, INSPECTION OF |
SAE AMS5662N | Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 52.5Ni - 19Cr - 3.0Mo - 5.1Cb (Nb) - 0.90Ti - 0.50AI - 18Fe Consumable Electrode or Vacuum Induction Melted 1775 °F (968 °C) Solution Heat Treated, Precipitation-Hardenable |
SAE AS3062C | Bolts, Screws and Studs, Screw Thread Requirements |
SAE AS1177A | Nondestructive Inspection Standards for Bolts and Screws |
SAE AMS2350BA | Standards and Test Methods |
MIL-STD-794 Revision E:1982 | PART AND EQUIPMENT, PROCEDURES FOR PACKAGING AND PACKING OF |
ASTM E 8 : 2004 | Standard Test Methods for Tension Testing of Metallic Materials |
SAE AS1132J | Bolts, Screws and Nuts - External Wrenching UNJ Thread, Inch - Design Standard |
SAE AMS 2373 : 1998 | QUALITY ASSURANCE SAMPLING OF BOLTS AND SCREWS |
SAE AS3063B | Bolts, Screws, and Studs, Geometric Control Requirements |
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