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SAE International - AS3412A

BOLT, TEE HEAD - AMS 5662, CHAMFERED, .375-24UNJF-3A (STRESS RUPTURE RESISTANT)

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Organization: SAE International
Publication Date: 1 October 2001
Status: active

Document History

AS3412A
October 1, 2001
BOLT, TEE HEAD - AMS 5662, CHAMFERED, .375-24UNJF-3A (STRESS RUPTURE RESISTANT)
A description is not available for this item.

References

This document references:
AMS2645 - Fluorescent Penetrant Inspection
Published by SAE International on July 1, 1948
This specification has been declared 'SUPERSEDED' by the Aerospace Materials Division, SAE, as of February 1995. The requirements of this specification are embodied in the latest issue of ASTM E 1417.
This document references:
AMS2645K - FLUORESCENT PENETRANT INSPECTION
Published by SAE International on February 1, 1995
A description is not available for this item.
This document references:
AMS5662 - ALLOY BARS, FORGINGS, AND RINGS, CORROSION AND HEAT RESISTANT Nickel Base - 19Cr - 3.1Mo - 5.1(Cb + Ta) - 0.90Ti - 0.50Al Consumable Electrode or Vacuum Induction Melted, Solution Treated
Published by SAE International on September 1, 1965
A description is not available for this item.
This document references:
AMS7467 - BOLTS AND SCREWS, NICKEL ALLOY, CORROSION AND HEAT RESISTANT Upset Headed, Roll Threaded, Stress-Rupture Resistant
Published by SAE International on April 15, 1978
This specification covers aircraft quality bolts and screws made from a corrosion and heat resistant nickel alloy.
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