Browse Standards AMS6325L
Current REVISED 2020-04-10

Steel, Bars, and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 105 ksi (724 MPa) Tensile Strength AMS6325L

This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings.
AMS6325L
2020-04-10
Latest
Revised
AMS6325K
2015-12-20
Historical
Revised
AMS6325J
2010-04-19
Historical
Revised
AMS6325H
2004-10-18
Historical
Revised
AMS6325G
2000-09-01
Historical
Reaffirmed
AMS6325F
1988-07-01
Historical
Revised
AMS6325E
1972-11-15
Historical
Revised
AMS6325D
1966-09-30
Historical
Revised
AMS6325C
1951-06-01
Historical
Revised
AMS6325B
1945-07-01
Historical
Revised
AMS6325A
1943-04-01
Historical
Revised
AMS6325
1942-09-01
Historical
Issued

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 10% off list price.
Login to see discount.
Special Offer: AeroPaks offers a customized subscription plan that is cost-effective and allows you to choose the number of downloads and Aerospace and Aerospace Material documents you need. Find more information here.
We also recommend:
STANDARD

Steel Bars and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 125 ksi (862 MPa) Tensile Strength

AMS6327L

View Details

STANDARD

BOLT, MACHINE - STEEL, DIFFUSED NICKEL-CADMIUM PLATED, DOUBLE HEXAGON EXTENDED WASHER HEAD, UNS K14675, 195 KSI MIN, .1900-32 UNJF-3A

AS9208C

View Details

STANDARD

Steel, Chrome-Nickel-Molybdenum (8740) Bars and Reforging Stock (Aircraft Quality)

AMSS6049B

View Details

Get Involved

Want to participate in updating this standard?

X