Contact sales

Tel. 44(0)1494 484844 Fax. 44(0)1494 482155



Request for Quotation

Part Number

Chromium and Vanadium Alloyed Silver steel CCV-120

Chemical Composition Limits

Weight %  C Cr Mn V Si Fe


 1.10-1.25  0.50-0.80 0.20-0.40 0.07-0.12 0.15-0.30 Rem

Other Chemically similar Specifications 

Weight %  C Cr Mn V Si Fe
 WS 1.2210  1.10-1.25  0.50-0.80 0.20-0.40 0.07-0.12 0.15-0.30 Rem
DIN 115 CrV3  1.10-1.25  0.50-0.80 0.20-0.40 0.07-0.12 0.15-0.30 Rem
AISI A681 / L2 ~  1.10-1.25  0.50-0.80 0.20-0.40 0.07-0.12 0.15-0.30 Rem
EN107CrV3 ~  1.10-1.25  0.50-0.80 0.20-0.40 0.07-0.12 0.15-0.30 Rem

CCV-120 material is Manufactured in Rod, Bar and coil

AISI A681 /L2 Chromium and Vanadium Alloyed Silver steel

WS 1.2210 Chromium and Vanadium Alloyed Silver steel


Material Features:

Alloyed steel with best hardening properties and reduced critical cooling rate. CCV-120 Cr V is characterised by a lower risk of stress cracking and distortion this alloy is relatively insensitive to overheating.


Available in: 

Cold drawn and polished; 10-35kg/coil

Bars 0-3.50 mm cold drawn and polished

Bars 3.50-40mm cold drawn, ground and polished.

Standard length of bars 2m Surface roughness N6


Tensile Strength

about 750 N/mm2 (before heat treatment)


Standard tolerance

Diameter  ISO h8

Out of roundness/ eccentricity 1/2 of dia. tolerance.


Heat treatment

Hardening water 800-820C above 10mm

Oil: 820-840C up to 10mm


Cutting rate

15-25m/min (dependent on lubrication oil, the cutting tools, the form of parts)


Stock Range





Every effort is made to ensure that technical specifications are accurate. However, technical specifications included herein should be used as a guideline only. All specifications are subject to change without notice.

Site © 2005 Quantum Alloys UK

Group Companies aircraftmaterials.com Ltd