SAE AF 1410 Structural and constructional steels

Material group: Ferrous Alloys / Structural and constructional steels

Country / Standard: United States / SAE

Data updates

Latest Update: 2022-04

Total number of updates: 9

Update History

2021-07 2021-03 2020-11 2019-09 2018-05 2017-03 2016-06 2013-11

This material has 297 properties — only a subset is shown here.

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SAE AF 1410 Chemical Composition

CRITERIA

VALUE

UNIT

CAS NUMBER

CRITERIA

VALUE

≤ 0.015

UNIT

CAS NUMBER

7429-90-5

CRITERIA

VALUE

0.13 – 0.17

UNIT

CAS NUMBER

7440-44-0

CRITERIA

VALUE

13.50 – 14.50

UNIT

CAS NUMBER

7440-48-4

CRITERIA

VALUE

val1

UNIT

CAS NUMBER

7440-47-3

CRITERIA

VALUE

val1

UNIT

CAS NUMBER

7439-96-5

CRITERIA

VALUE

val1

UNIT

CAS NUMBER

7439-98-7

CRITERIA

VALUE

val1

UNIT

CAS NUMBER

7727-37-9; 17778-88-0

CRITERIA

VALUE

val1

UNIT

CAS NUMBER

7440-02-0

CRITERIA

VALUE

val1

UNIT

CAS NUMBER

7782-44-7; 17778-80-2

CRITERIA

VALUE

val1

UNIT

CAS NUMBER

7723-14-0

CRITERIA

P+S

VALUE

val1

UNIT

CAS NUMBER

CRITERIA

VALUE

val1

UNIT

CAS NUMBER

7704-34-9

CRITERIA

VALUE

val1

UNIT

CAS NUMBER

7440-21-3

CRITERIA

VALUE

val1

UNIT

CAS NUMBER

7440-32-6

SAE AMS 6522D: 2003 / Steel Plate 2.0Cr - 10Ni - 14Co - 1.0Mo (0.13 - 0.17C) Vacuum Melted, Normalized, and Overaged

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SAE AF 1410 Physical Properties

Temperature

0 - 30°C 30 - 100°C 100 - 300°C ≥ 300°C

PROPERTY / VALUE

Compression Modulus

213 GPa

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Modulus of Elasticity

190 — 210 GPa

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Density

val1 kg/dm³

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Poisson Coefficient

val1

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This material has 297 properties — only a subset is shown here.

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SAE AF 1410 Heat Treatments

Normalize by heating to 899°C ± 14°C, holding at heat for 60 minutes ± 5, and cooling to room temperature, and overage by heating to 677°C ± 14°C, holding at heat for not less than 6 hours and forced air cooling. Heated to 899°C ± 14°C, held at heat for 60 minutes ± 5, forced air cooled to room temperature, reheated to 829°C ± 14°C, held at heat for 60 minutes ± 5, forced air cooled to room temperature, cooled to -73°C ± 8°C, held at that temperature for 60 minutes ± 5, warmed in air to room temperature, and aged by heating to 510°C ± 6°C, holding at heat for not less than 5 hours and forced air cooling.
Normalizing: 885-913°C (1625-1675°F), air quenched. Overage to facilitate machining by normalizing plus 677 ± 13.9°C (1250 ± 25°F) for not less than 6 hours and air quenched.
Furnace cool to 538°C (1000°F) or below (rate of furnace cool should be 28°C (50°F) per hour or slower). Recommended subcritical anneal temperature is 677°C (1250°F).
Austenitizing: 816-843°C (1500-1550°F). Medium for quenching: oil. Cool to -73°C (-100°F) for 1 hour minimum within 2 hours after quenching and before tempering.

SAE AF 1410 Mechanical Properties

Temperature

0 - 30°C 30 - 100°C 100 - 300°C ≥ 300°C

PROPERTY / VALUE

Tensile Strength

1516 — 1820.2 MPa

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Brinell Hardness (HB)

val1

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Elongation, A

val1 %

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Compression Yield Strength

val1 MPa

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Reduction of Area

val1 %

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Rockwell Hardness (HR)

val1

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Yield Strength, Rp0.2

val1 MPa

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Grain Size

val1

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Impact Energy

val1 J

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Vickers Hardness (HV)

val1

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SAE AF 1410 International Equivalent Materials

Showing 4 of 4 results.

MATERIAL

STANDARD

COUNTRY / PRODUCER

EQUIVALENCE CATEGORY

MATERIAL

AF 1410

STANDARD

AISI

COUNTRY / PRODUCER

United States

EQUIVALENCE CATEGORY

Identical

MATERIAL

AF1410

STANDARD

PROPRIETARY

COUNTRY / PRODUCER

EQUIVALENCE CATEGORY

Implicit

MATERIAL

K92571

STANDARD

UNS

COUNTRY / PRODUCER

United States

EQUIVALENCE CATEGORY

Official

MATERIAL

TURBALOY AF1410

STANDARD

PROPRIETARY

COUNTRY / PRODUCER

EQUIVALENCE CATEGORY

Implicit

Equivalence categories reflect chemical-composition and mechanical-property comparison — always verify suitability against the governing specification for your application.

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See all 4 equivalent grades with detailed mapping by standard, producer and equivalence category.

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4Cross References

28Composition
152Mechanical Properties
46Physical Properties
4Heat Treatment
1Metallography
-Machinability

11Stress-Strain
-Formability
-Fatigue
-Fracture
-Creep

-Joints
-Coatings
48Dimensions
-Tribology

-Corrosion
-Ageing
-Weatherability
-Irradiation

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