Heat Treating Material to H950 Condition PH13-8Mo H950 Condition Custom 455 H950 Condition 15-5 Ph H950 Condition
Tag Archives: PH 13-8 Mo
BMS7-189
REQUEST QUOTE BMS7-189 is a BOEING specification for PH 13-8 Mo calling for “BAR & FORGINGS. HEAT & CORROSION RESISTANT ALLOY, IRON BASE, 13 Cr, 8 Ni, 1 Al, 2.25 Mo (Ph 13-8 Mo)” BMS stands for “Boeing Material Specification” and originate from Boeing’s headquarters in Seattle, WA. For more information on BMS7-189 please referContinue reading “BMS7-189”
BMS7-332
REQUEST QUOTE BMS7-332 is a BOEING specification for PH 13-8 Mo calling for “PH13-8Mo CRES BAR, FORGING STOCK, FORGINGS AND EXTRUSIONS WITH CONTROLLED FRACTURE TOUGHNESS” BMS stands for “Boeing Material Specification” and originate from Boeing’s headquarters in Seattle, WA. For more information on BMS7-332 please refer to: D1-4426 Approved Process Lists As a TierContinue reading “BMS7-332”
BMS7-349
REQUEST QUOTE BMS7-349 is a BOEING specification for PH 13-8 Mo calling for “BARS, FORGINGS, AND FORGING STOCK VACUUM INDUCTION MELTED – VACUUM ARC REMELTED (VIM – VAR) PH13-8Mo CRES” BMS stands for “Boeing Material Specification” and originate from Boeing’s headquarters in Seattle, WA. For more information on BMS7-349 please refer to: D1-4426 Approved Process ListsContinue reading “BMS7-349”
DMS 2100
DMS 2100 is a BOEING specification for PH 13-8 Mo calling for “STEEL, CORROSION RESISTANT, PH 13-8 MO” REQUEST QUOTE DMS specifications originate from Boeing’s Long Beach facility under D1-4426 Approved Process Lists. DMS2100 / DMS 2100 originated at the Long Beach facility, therefore it is widely used for Boeing’s aircraft manufacturing at multiple locations. Continue reading “DMS 2100”
HMS-6-1105
REQUEST QUOTE PH 13-8 Mo Stainless Steel per Hughes Aircraft HMS-6-1105 Ph 13-8 Mo is a martensitic precipitation-hardening stainless steel that has excellent strength, high hardness, superior toughness, and good corrosion resistance. Good transverse toughness properties are achieved by tight chemical composition control, low carbon content, and vacuum melting. The alloy is produced by vacuumContinue reading “HMS-6-1105”
LAT1-9048
REQUEST QUOTE PH 13-8 Mo per Liebherr Aerospace specification LAT1-9048 Ph 13-8 Mo is a martensitic precipitation-hardening stainless steel that has excellent strength, high hardness, superior toughness, and good corrosion resistance. Good transverse toughness properties are achieved by tight chemical composition control, low carbon content, and vacuum melting. The alloy is produced by vacuum inductionContinue reading “LAT1-9048”
EMCM-001-1013
REQUEST QUOTE PH 13-8 Mo per Ph 13-8 Mo is a martensitic precipitation-hardening stainless steel that has excellent strength, high hardness, superior toughness, and good corrosion resistance. Good transverse toughness properties are achieved by tight chemical composition control, low carbon content, and vacuum melting. The alloy is produced by vacuum induction melting (VIM) followed byContinue reading “EMCM-001-1013”
IPS 01-04-004
REQUEST QUOTE PH 13-8 Mo per Airbus specification Ph 13-8 Mo is a martensitic precipitation-hardening stainless steel that has excellent strength, high hardness, superior toughness, and good corrosion resistance. Good transverse toughness properties are achieved by tight chemical composition control, low carbon content, and vacuum melting. The alloy is produced by vacuum induction melting (VIM)Continue reading “IPS 01-04-004”
ABS 5259A
REQUEST QUOTE PH 13-8 Mo per Airbus specification ABS 5259A Ph 13-8 Mo is a martensitic precipitation-hardening stainless steel that has excellent strength, high hardness, superior toughness, and good corrosion resistance. Good transverse toughness properties are achieved by tight chemical composition control, low carbon content, and vacuum melting. The alloy is produced by vacuumContinue reading “ABS 5259A”