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Quality 1.6604.5

General Product Description

Material number 1.6604.5

Short name according to EN 30CND8

Applicable standards WL 1.6604

Treatment annealed or quenched and tempered

Variations

QualityTreatmentShapeDimension (mm)
1.6604.5annealed or quenched and temperedRoundRound10 - 127
Your inquiry

Tim Weber
Purchasing / Aviation Sales / Authorized Representative
+49 (0) 23 31 - 387 115
weber@remove-this.remystahl.de
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Pierre Hermsdorf
Authorized Officer / Head of Procurement & Sales
+49 (0) 23 31 - 387 124
hermsdorf@remove-this.remystahl.de
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Description

The material 1.6604 is a Cr-Ni-Mo-alloyed quenched and tempered steel for high strength and toughness requirements with large quenched and tempered cross sections. Its Mo content makes it insensitive to tempering embrittlement. For aerospace applications it is certified according to WL 1.6604.

Chemical composition (in %)

CMnPMoSCrNiSi
Min 0,26 0,30 - 0,30 - 1,8 1,8 0,15
Max 0,34 0,60 0,025 0,50 0,025 2,3 2,3 0,4
ElementMinMax
C 0,26 0,34
Mn 0,30 0,60
P - 0,025
Mo 0,30 0,50
S - 0,025
Cr 1,8 2,3
Ni 1,8 2,3
Si 0,15 0,4

Mechanical properties (quenched and tempered)

Tensile strength Rm 1100–980 N/mm2

0.2% proof stress Rp0.2 900 N/mm2

Elongation at break A5 10 (L) / 7 (Q) %

Notched impact energy (ISO-V) 25 (L) / 15 (Q) J

Hardness < 321 HB

Magnetizability No

Typical areas of application

aerospace technology

heavily loaded structural components

landing gear and engine components

shafts, axles and bolts

General properties (quenched and tempered)

Corrosion Resistance

Weldability

Forgeability

Tensionability

= Low
= Very Good

Note

All information in this data sheet has been compiled to the best of our knowledge and belief. It is for information purposes only and does not constitute a assured property or guarantee. For the suitability of the material in specific applications, we recommend carrying out appropriate inspections and tests. Any liability for damage or errors is excluded.