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SAE AMS-S-6758

Steel, Chrome-Molybdenum (4130) Bars and Reforging Stock (Aircraft Quality)

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Organization: SAE
Publication Date: 1 November 2017
Status: active
Page Count: 14
scope:

This specification covers chrome-molybdenum (4130) steel bars and forging stock of aircraft quality.

Classification

The steel bars and reforging stock shall be as follows:

Physical condition: Materials shall be furnished in one of the following physical conditions, as specified (see 6.2c):

a.As forged

b.As rolled

c.Annealed

d.Normalized

e.Normalized and tempered

f.Hardened and tempered

Surface conditions: Materials shall be furnished in one of the following surface conditions, as specified (see 6.2c):

1. Black, as forged or rolled

2. Pickled or blast cleaned

3. Rough turned

4. Cold finished (drawn)

5. Turned, ground and polished

intended Use:

The material covered by this specification is intended for general use in the manufacture of parts and components hardened by heat treatment to tensile a strength of 180,000 psi or less. It is... View More

Document History

SAE AMS-S-6758
November 1, 2017
Steel, Chrome-Molybdenum (4130) Bars and Reforging Stock (Aircraft Quality)
This specification covers chrome-molybdenum (4130) steel bars and forging stock of aircraft quality. Classification The steel bars and reforging stock shall be as follows: Physical condition:...
September 1, 2003
Steel, Chrome-Molybdenum (4130) Bars and Reforging Stock (Aircraft Quality)
This specification covers chrome-molybdenum (4130) steel bars and forging stock of aircraft quality. Classification: The steel bars and reforging stock shall be as follows: Physical condition:...
September 1, 2003
Steel, Chrome-Molybdenum (4130) Bars and Reforging Stock (Aircraft Quality)
The material covered by this specification is intended for general use in the manufacture of parts and components hardened by heat treatment to tensile a strength of 180,000 psi or less. It is...
September 1, 2003
Steel, Chrome-Molybdenum (4130) Bars and Reforging Stock (Aircraft Quality)
The material covered by this specification is intended for general use in the manufacture of parts and componets hardened dy heat treatment to tensile a strengh of 180,000 psi or less.it is weldable...
July 1, 1998
Steel, Chrome-Molybdenum (4130) Bars and Reforging Stock (Aircraft Quality)
1. SCOPE: 1.1 Scope: This specification covers chrome-molybdenum (4130) steel bars and forging stock of aircraft quality. 1.2 Classification: The steel bars and reforging stock shall be as follows:...

References

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