High Temp Metals 800-500-2141

Alloy AM350

Description

Alloy 350 is a chromium-nickel-molybdenum stainless steel which can be hardnened by martensitic transformation and/or precipitation hardening. It has been used for gas turbine compressor components such as blades, discs, rotors, shafts, and similar parts where high strength was required at room and intermediate temperatures. Depending upon the heat treatment, alloy 350 may have an austenitic structure for best formability, or a martensitic structure with strengths comparable to those of martensitic steels. The alloy normally contains about 5 to 10% delta ferrite. The corrosion resistance of alloy 350 approaches that of the chromium-nickel austenitic stainless steel

TYPICAL SPECIFICATION PACKAGES

UNS-S-35000

SHEET:AMS 5548, AMS-S-8840, B50T1140A, ASTM-A-693

ALLOYSIZEWEIGHT
CURRENT SHEET INVENTORY
Alloy AM3500.020 X 35.000 X 120.000
0.508MM X 889 X 3048
1530 LBS
694 KG
Alloy AM3500.025 X 35.500 X 120.000
0.635MM X 901.7 X 3048
2353 LBS
1067 KG
Alloy AM3500.032 X 36.000 X 120.000
0.8128MM X 914.4 X 3048
5432 LBS
2464 KG
Alloy AM3500.040 X 36.000 X 120.000
1.016MM X 914.4 X 3048
1462 LBS
663 KG
Alloy AM3500.050 X 36.000 X 120.000
1.27MM X 914.4 X 3048
3191 LBS
1447 KG
Alloy AM3500.063 X 36.000 X 120.000
1.6002MM X 914.4 X 3048
383 LBS
174 KG
Alloy AM350 - DUE DATE: 09-01-170.063 X 36.000 X 120.000
1.6002MM X 914.4 X 3048
4000 LBS
1814 KG
Alloy AM3500.125 X 36.000 X 120.000
3.175MM X 914.4 X 3048
4049 LBS
1837 KG