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
1457 LBS
661 KG
Alloy AM3500.025 X 35.500 X 120.000
0.635MM X 901.7 X 3048
2293 LBS
1040 KG
Alloy AM3500.032 X 36.000 X 120.000
0.8128MM X 914.4 X 3048
4613 LBS
2092 KG
Alloy AM3500.040 X 36.000 X 120.000
1.016MM X 914.4 X 3048
1217 LBS
552 KG
Alloy AM3500.050 X 36.000 X 120.000
1.27MM X 914.4 X 3048
2878 LBS
1305 KG
Alloy AM3500.063 X 36.000 X 120.000
1.6002MM X 914.4 X 3048
1618 LBS
734 KG
Alloy AM350 - DUE DATE: 09-01-180.063 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
3739 LBS
1696 KG