E-Z 6 NCT 25 (France / AIR) Material Properties
Material group:
Ferrous Alloys / Stainless steels
Country/Standard:
France / AIR
Data updates
Latest Update: 2019-01
Total number of updates: 2
Update History:
2017-12
Mechanical Properties
Temperature
Physical Properties
Temperature
Composition
CRITERIA
VALUE
UNIT
CAS NUMBER
CRITERIA
Al
VALUE
≤ 0.3500
UNIT
%
CAS NUMBER
7429-90-5
CRITERIA
B
VALUE
0.0010 – 0.0100
UNIT
%
CAS NUMBER
7440-42-8
CRITERIA
C
VALUE
≤ 0.0800
UNIT
%
CAS NUMBER
7440-44-0
CRITERIA
Cr
VALUE
val1
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UNIT
%
CAS NUMBER
7440-47-3
CRITERIA
Mn
VALUE
val1
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UNIT
%
CAS NUMBER
7439-96-5
CRITERIA
Mo
VALUE
val1
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UNIT
%
CAS NUMBER
7439-98-7
CRITERIA
Ni
VALUE
val1
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UNIT
%
CAS NUMBER
7440-02-0
CRITERIA
P
VALUE
val1
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UNIT
%
CAS NUMBER
7723-14-0
CRITERIA
S
VALUE
val1
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UNIT
%
CAS NUMBER
7704-34-9
CRITERIA
Si
VALUE
val1
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UNIT
%
CAS NUMBER
7440-21-3
CRITERIA
Ti
VALUE
val1
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UNIT
%
CAS NUMBER
7440-32-6
CRITERIA
V
VALUE
val1
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UNIT
%
CAS NUMBER
7440-62-2
AIR 9160/C: 1973 / General conditions for delivery and use of wrought steels used in aeronautical structures
Heat Treatments
- Hardened and tempered (I) for d = 16 mm: Hardened at 900 +/- 10°C. Returned at 550°C, then regular rise in temperature to 725°C in 1 hour to 1 hour 30 minutes; Tempered 16h at 720 +/- 5°C; <br> Hardened and tempered (II) at 900 +/- 10°C; <br> Hardened and tempered (III): Hardened at 900 +/- 10°C, Tempered 16h at 720 +/- 5°C.
- Hardened and tempered (T960) for d = 16 mm: Hardened at 900 +/- 10°C, Tempered 16h at 720 +/- 5°C; <br /> Hardened and tempered (A) at 890 - 910°C; <br /> Hardened and tempered (T960): Hardened at 890 - 910°C, Tempered 16h at 720 +/- 5°C.
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286 Cross References
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25 Composition
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17 Mechanical Properties
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3 Physical Properties
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2 Heat Treatment
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- Metallography
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- Machinability
-
- Stress-Strain
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- Formability
-
- Fatigue
-
- Fracture
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2 Creep
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- Joints
-
- Coatings
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- Dimensions
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- Tribology
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- Corrosion
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- Ageing
-
- Weatherability
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- Irradiation
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139 Total Suppliers