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SAE AMS7466B

Current

Current

The latest, up-to-date edition.

Bolts and Screws Nickel Alloy, Corrosion and Heat Resistant, Upset Headed, Roll Threaded, Fatigue Resistant

Published date

01-10-1993

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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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