February 1, 2003. Subscribers can view annotate, and download all of SAE's content. E4340 steel per SAE AMS-S-5000 (formerly MIL-S-5000) heat treated to 260 to 280 ksi (pounds per square inch ×1000) as the baseline. Document Number. BMS-7-26 Boeing Spec Alloy Steel. superseded a superseded standard is one,. astm-d5363 mil-a-101-s/s by mmm-a-250. 45CR (0. Identification numbers. MIL S-5000: AMS 6409 Specifications. 750"dia: 72. Steel Bars. Specifications: AMS 6359, AMS 6409, AMS 6414, AMS 6415, AMS 6454, ASTM A29, ASTM A322, ASTM A331, ASTM A506,ASTM A519, ASTM A646, ASTM A752, ASTM A829, MIL-S-5000, UNS G43400 . AMS2774 Heat Treatment Wrought Nickel Alloy and Cobalt Alloy Parts Specification Treatment Heat Treatment Wrought Nickel Alloy & Cobalt Alloy Parts Rapid Response RFQ Contact Us. Multi - user online standards collection: secure, flexibile and cost effective. 625, . To those users, I hope to provide a4130 Plate 4130 Sheet 4130 Bar 4130 Rod, 4130 Tube, 4130 Tubing 4130 Pipe, 4130 Noramlized and Heat Treat Aircraft Alloy Round,4130 Bar to AMS 2301, AMS-S-6758, ASTM-A-331,ASTM-A-322 MIL-S-6758, AMS 6346, AMS 6370, AMS 6348 4330 MOD Vacuum Melt Normalized & Tempered Round Barsuperseded a superseded standard is one,. MIL-S-5000 | Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock (Superseded by SAE AMS-S-5000) | Document Center, Inc. 60 Si, 0. Find Standards By. 400 Series Stainless Steel. astm-d5363 mil-a-101-s/s by mmm-a-250. This specification is drawn to present general instructions for carburizing and nitriding of carbon and alloy steels and cyanide hardening operation used in the fabrication of aircraft and aircraft engine parts. AMS S 8802 type 1 is a dichromate cured sealant. 000" (177. 025 . mil-a-5540. SAE AMS 6484 : 2016. 1 Al. 3) 6al-6v-2sn: ams 4918, ams 4936, ams 4937, ams 4971, ams 4978, ams 4979, mil-t-9046, mil-t-9047, uns 56620 6Al-6V-2Sn Titanium Alloy is an alpha-beta alloy that can be heat treated to higher strengths and heavier section sizes than titanium alloy 6AL-4V. , This specification presents requirements for the carburizing and nitriding of carbon and allow steels to produce the mechanical properties specified by drawings, detail specifications,. Condition A AMS 5648 Not in MMPDS. QUALITY MANAGEMENT SYSTEMS - REQUIREMENTS FOR AVIATION, SPACE AND DEFENSE DISTRIBUTORS. Nov. 12, 1967. 4435 ws 1. REV A AMENDMENT 2. Inconel 706 ™ Super Alloy in Sheet, Strip and Plate. Historical. Status. 284 lb/in³, a thermal conductivity of 24 Btu/ (hr/ft²/°F), and a specific heat of 0. AMS 6931 6al/4v Titanium Alloy. 455 Stainless Steel. 9510-00-993-5760, BAR,METAL. AMS-S-13165 was made redundant by AMS 2430 and AMS 2432. 5, 1973. , This specification covers chrome-molybdenum (4130) steel bars and forging stock of aircraft quality. AMS 6265 Alloy Steel. This document comes with our free Notification Service, good for the life of the document. 85g/cm³ and a melting point of 1450°C. Steel Reforging Stock. The passivation treatments provided by this specification are intended to improve the corrosion resistance of parts made from austenitic, ferritic and martensitic corrosion-resistant steels of the 200, 300 and 400 series. 7004 State Route 123 Franklin, OH 45005 . 60Mn (2024-T3) (2024-T351) Solution Heat Treated QQ-A-250/4. 4130 Alloy Steel in Department of Defense Military MilSpec Specification MIL-S-6758 per SAE International’s AMS Standard: “This specification covers chrome-molybdenum (4130) steel bars and forging stock of aircraft quality. ams 2658 d ams 2700 f ams 2759 g ams 2759/1 j ams 2759/3 j ams 2770 r ams 2772 g ams 2801 b ams-c-27725 d ams-h-6875 (stabilized with use of ams 2761) c ams-qq-p-35 (cancelled - superseded by ams 2700) a ams-qq-p-416 f astm e1417/e1417m 21 mil-a-8625 (superseded by mil-prf-8625) f amm 1 mil-c-5541 (superseded by mil-dtl-5541) e Buy MIL-S-5000 Revision E:1982 STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS AND REFORGING STOCK from SAI Global ams 2658 d ams 2700 f ams 2759 g ams 2759/1 j ams 2759/3 j ams 2770 r ams 2772 g ams 2801 c ams-c-27725 d ams-h-6875 (stabilized with use of ams 2761) c ams-qq-p-35 (cancelled - superseded by ams 2700) a ams-qq-p-416 g astm 2021, e1 QQ-S-763 Rev. G43406. Tensile strength. Subscribers can. 28/. Because this revision clarifies changes from revision D, changes for both revisions are maintained. Superseded. 4340 Alloy Steel. 4330M Alloy Steel. Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock (Superseded by SAE AMS-S-5000) To find similar documents by Federal Supply Class Code: FSC 9510 (Bars and Rods) ORDER. 6Cu 0. Heat Treatment of Steel Raw Materials (STABILIZED Sep 2020) AMSH6875C. HP9-4-20 High Strength Alloy Steel. 6. Heat treatment. AMS 5598. 35 0. tw; Taipei Branch Office. 4), and Identification (5. 4364: ABS 5064: 7175: AMS 4148 7175-T6 Die Forgings: IPS03-02-000/0008-03: 7175:. mil-a-1058 . 2 Timothy 1:7 . Victoria San Juan Cruises sails May through October between Bellingham,. AMS-S-5000; AMS-S-6758; Other Military Grade Alloys & Steels; View All Alloys & Metals by Grade. A-286 Stainless Steel. Buy SAE AMS 5620 : 2012, a superseded standard which covers two types of corrosion and heat-resistant steel, from SAE International. EN ISO 13533:2002. It provides details, methods, and procedures for these various. MIL-S-6758. 1998-04-01. 4340 RD BAR COND C 2. Nickel INVAR 36 . 025 . Revised. VIEW CART · CONTACT · HOME. 2 Classification: The steel bars and reforging stock shall be as follows:. Your Message. 0. Our discussion here is driven by the fact that several end-users continue to use the original MIL specification for their peening operations. 1 pageMIL-S-6090, Revision A, June 4, 1971 - STEEL, CARBURIZING AND NITRIDING, PROCESSES FOR This specification presents requirements for the carburizing and nitriding of carbon and alloy steels to produce the mechanical properties specified by drawings, detail metal specifications, or other applicable specifications (see 6. QQ-P-35C/AMS-QQ-P-35A SPECIFICATIONS Passivation Types Type I – Withdrawn Type II – 20-25 v% Nitric, 2-2. 60Mn (2024-T3) (2024-T351) Solution Heat Treated QQ-A-250/4. Alloy 4130 is also vacuum degassed to meet the magnetic particle. Superseded By: SAE AMS6415 Document Language: English Published By: SAE International (SAE) Page Count: 12 ANSI Approved: No DoD Adopted: No Document History:. 316L Condition A Sheet, Strip, Plate QQ-S-766 AMS 5507 Not in MMPDS. Historical. Status. Infostore. Since the material usually comes in the annealed condition, additional heat treatments (oil quenching and tempering, or normalizing and tempering) can produce parts with even higher strength and fatigue resistance. AMS-S-6758 has excellent physical properties. Version: F. AMS 6415 material’s unique combination of properties makes it ideal for various high-stress engineering applications. Revision Level. 13-8MO Stainless Steel in AMS 5629 Specification, per SAE International: “This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, flash welded rings, extrusions, and stock for forging, flash welded rings, or extrusion. The AMS-5000 also provides the capability to perform vertical "direct to" descents to meetMIL-S-5000 Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock. Status. SAE AMS S 5000 : 1999 : STEEL, CHROME-NICKEL-MOLYBDENUM (E4340) BARS AND REFORGING STOCK: ASTM E 1158 : 2014 : REDLINE : Standard Guide for Material Selection and Fabrication of Reference Blocks for the Pulsed Longitudinal Wave Ultrasonic Testing of Metal and Metal Alloy Production Material: SAE AMS QQ A 200/11 : 2014 MIL-S-5000E, MILITARY SPECIFICATION: STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS, AND FORGING STOCK (12-NOV-1982) [S/S BY SAE-AMS-S-5000]. 1. AMS 6414 sheet is an alloy steel that consists of carbon, manganese, chromium, molybdenum, vanadium, and nickel. 7. Per D8-5000 Finish Code VF-1. EN ISO 15156-2 - PETROLEUM AND NATURAL GAS INDUSTRIES - MATERIALS FOR USE IN H [2]S CONTAINING ENVIRONMENTS IN. 15-5ph plt 0. Withdrawal Date:MIL-H-6875H HEAT TREATMENT OF STEEL was superseded 2 Feb 1999 by AMS-H-6875 Heat Treatment of Steel Raw Materials ($59 from SAE). Superseded By: SAE AMS4115 Document Language: English Published By: SAE International (SAE) Page Count: 6 ANSI Approved: No DoD Adopted: No Document History:. Rationale: AMS-S-5000A was issued to cancel and supersede AMS-S-5000 with current, technically equivalent specifications. 4340 Alloy Steel. E. titanium. FSC Code: 9510 - Bars and Rods, Iron and Steel. 375, . 36% to 0. 15/. 0. This specification covers a carbon steel in the form of sheet, strip, and plate. 3125, . Buy SAE AMS S 5000 : 1999 STEEL, CHROME-NICKEL-MOLYBDENUM (E4340) BARS AND REFORGING STOCK from SAI Global. 3. STEEL PLATE, SHEET, AND STRIP, ALLOY, 4130, AIRCRAFT QUALITY (S/S BY SAE-AMS6350, SAE-AMS6351 OR SAE-AMS6345. Having a lower carbon content improves weldability. , This specification presents requirements for thin-walled (inside diameter greater than four times the wall thickness and outside diameter 1/4 inch. Technical Data Sheet. Popular Metal Specs. Our extensive product offerings include alloy, stainless, nickel, aluminum, titanium, carbon and cast iron. Perry encouraged the military to use Non-Government Standards and do away with outdated military specifications, asserting that doing so would reduce government oversight and lower costs. AMS-S-5000. Report Problem (email) Status: Cancelled. 5Mg 0. Alloy Steel MIL-S-8699 . For our AISI 4130 (E4130) aircraft quality steel products please visit. A-286 Stainless Steel. AMS-S-5000 Specification 4340 High Tensile Steel (MilSpec here) Steel Bars. Talk To Us About the Alloys You Need Most. 284 lb/in³, a thermal conductivity of 24 Btu/ (hr/ft²/°F), and a specific heat of 0. Buy SAE AMS S 5000 : 2007 STEEL, CHROME-NICKEL-MOLYBDENUM (E4340) BARS AND. Defense industry. May 1, 1999 Sealing Compound, Temperature Resistant, Integral Fuel Tanks and Fuel Cell Cavities, High Adhesion This specification covers temperature resistant, two component synthetic rubber compounds of the polysulfide type for sealing and repairing integral fuel tanks and fuel cell cavities, for continuous. Scope: This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. Bars, and Forging Stock (Superseded by SAE AMS-S-5000) To find similar documents by Federal Supply Class Code: FSC 9510 (Bars and Rods) ORDER. Revision Level. Max. Sealing compound, temperature-resistant, integral fuel tanks and fuel cell cavities, high-adhesion (superseded by SAE AMS-S-8802). We carry, process and forge MISC United States Federal GSA Specification QQ-S-764 Grade Stainless Steel. 1 MIL-H-81200 replaced by AMS-H-81200. AMS 5630 MS21154B GROOVED RACE & MS21155B CHAMFERED RACE, BRONZE SERIES. Cancelled. Due to E-4340's high alloy content it obtains a uniformed hardness by heat treatment. sae ams s 6090 : 2006 : steel carburizing and nitriding, processes for: sae as 5944 : 1999 :MIL-T-9047 Military (Department of Defense) Specification MilSpec 6al/4v Alpha/Beta Titanium Alloy. March 1, 1999. 1. AMS-2769 Rev C Heat Treatment of Parts in Vacuum (07-12-19) AMS-2770 Rev P Heat Treatment of Wrought Aluminum Alloy Parts (04-08-19) ARP-1962 Rev B Training and Approval of Heat Treating. 25, 2. Alloy Steel AMS 6411 . Inconel X750 ™ Super Alloy in Sheet, Strip and Plate. mil-a-907. AMS 6414 Alloy Steel. Use our Rapid Response RFQ to request a quote. We carry, process and forge MISC United States Federal GSA Specification QQ-S-766. We are a pre-eminent alloy steel distributor who has proudly serviced the needs for over 30 years as metal and alloy suppliers to the world’s major Aerospace and Aero-Engine Manufacturers. Status. 4Cu 1. 5Mg 1. , This specification covers chrome-molybdenum (4140) steel bars, rods, and forging stock of aircraft quality. Status. Reference to AMS2759 on a drawing, fabrication order, purchase order, etc. Due to E-4340's high alloy content it obtains a uniformed hardness by heat treatment. 000 HEX. 1), ASTM-A295 17-22 AMS 6304 COBALT ALLOYS 28CR-6Mo ASTM F1537. 4340 air melt bms 7˜28, mil˜s˜5000, dms 1555 gr. HP9-4-20 High Strength Alloy Steel. Heat treatment. 17-22a: uns k14675 specs: ams-6304, ams-6305 17-22a(s) uns k23015 specs: ams-6302 4130: uns g41300 specs: ams-6345, ams-6348, ams-6350, ams-6370, ams-s-6758, atm-a-322, mil-s-18729 4140: uns g41400 specs: ams-6382, ams-s-5626 4330 mod vac melt: uns k23080 specs: ams-6411, ams-6427, bms-7-122, bms-7-27, gm-1010,. Apr 22, 2015 #3MIL-S-8802. AMS 6414 Alloy Steel. All Grades. Use our Rapid Response RFQ to request a quote. Condition A AMS 5648 Not in MMPDS. , Canada, Mexico, U. Our service centers are located throughout the U. Coatings, colorants, and finishes. 12, 1982. Test procedures. The alloy’s melting point stands at approximately 2,800°F, and its coefficient of thermal expansion is 6. TOLERANCES, CORROSION AND HEAT-RESISTANT STEEL TUBING. 92. Country: USA: Britain: Britain: Japan: Standard: ASTM A29: EN 10250: BS 970: JIS G4103: Grades: 4340: 36CrNiMo4/ 1. This product is not available online at this time. Prior to that date, processors may perform shot peening in accordance with AMS-S-13165 or AMS 2430. SAE AMS 6415 : 2016. Aluminum alloys. AMS 6349 Bar AMS 6382 Bar AMS S 5626 MIL-S- 5626 AMS 6349/ 6382 Bar Stock List: ASTM S331 : UNS G41400: 4140 Normalised: AMS 6349 AMS 6382 AMS 6529 AMS S 5626 MIL-S-5626: ASTM A322: 708M40 709M40: 1. Theams 6257 / ams 6419 ams 6417 / bs s155 gm 1012-3 mil-s-qq-8844(class 3) 5: 4340: 10≦Φ≦454: g43400: ams 6409 / ams 6414 ams 6415 / bms 7-28 ams-s-5000 mil-s-8844(class 1) 6: 4330m: 10≦Φ≦454: k23080: ams 6411 / ams 6427 bms 7-122 / bms 7-27 be 0886 / ce 0906 gm 1010: 7: 9310: 10≦Φ≦454: g93106: ams 6265 ams 6260: 8: 4130:. 00. MIL-S-5000. Talk To Us About the Alloys You Need Most. current specification revisions revision 122022. ALLOY ROD/BAR HEX 4340 AMS-S-5000 1. AMS-S-5000A was issued to cancel and supersede AMS-S-5000 with current, technically equivalent specifications. Subscribers can view annotate, and download all of SAE's content. We carry, process and forge MISC Specification MTL-1201 Grade 300M / 4340M Alloy Steel. All Grades. This combination of alloy and heat treat level. As aviation enthusiasts we are pleased to serve all of your aircraft alloy needs. 20 1. 0000. All Grades. Quality assurance. 1. AMS5085. BMS-7-26 Boeing Spec Alloy Steel. 4CU - 1. 44 C, 1. Use our Rapid RFQ to request a quote. fluid connection, 5000 psi: mil-i-45934 base document:1971 : insert, screw thread, keyring locked, self locking and non self locking, 125, 180, and 220 ksi ftu: general specification for. Publication Date. BMS-7-26 Boeing Spec Alloy Steel. Our extensive product offerings include alloy, stainless, nickel, aluminum, titanium, carbon and cast iron. Rationale: AMS-S-13165 has been designated Cancelled and Superseded because equivalent technical requirements are provided by AMS 2430. 302 Foil (Shim) is available in various thicknesses. Please request a quote below or head over to the general catalog by clicking the "Products" link in. 3. Technical Data Sheet. SAE AMS-S-5000, Revision A, March 2007 - Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock. AMS-S-5000 Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock 2. SCOPE: 1. 30V, CONSUMABLE ELECTRODE MELTED 1800 DEGREES F (982 DEGREES C) SOLUTION TREATED AND WORK-STRENGTHENED, 160 KSI (1103 MPA) TENSILE STRENGTH from SAI Global. HP9-4-20 High Strength Alloy Steel. Aeronautical Design Standard (ADS) Documents. 6511: EN24/817M40: SNCM 439/SNCM8: AMS 6415 Uses. 1 for heat treatment of steel parts (see 8. MIL-STD-2154 Military (Department of Defense) Specification MilSpec Alloy Inspection MilSpec Ultrasonic Inspection. 595A colour chart. If you require technical assistance or would like to receive a quote, please call our Customer Service team TOLL FREE at (866) 610-1660. 7 Cooling The load shall be cooled from the nitriding temperature in a suitable atmosphere to 300 °F (149 °C) or below. Titanium Industries Inc. 4330M Alloy Steel. STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS, AND FORGING STOCK (S/S BY SAE-AMS6415P AND SAE-AMS-S-5000) (SUPERSEDING MIL-S-5000D) standard by Military Specifications and Standards, 11/12/1982. Feb. 3). AMS 5735 is a sub-type specification of Stainless Steel A286, a precipitation-hardenable super-alloy that possesses many favorable properties. HP9-4-30 High Strength Alloy Steel. mil-a-3316 mil-a-3920. The military paid to have its old specs hosted by commercial standard companies so we can claim we use commercial standards. 40TI (SAE 30321), SOLUTION. All Grades. February 1998 and replaced by AMS-S-13165. 80/1. Minimum Mechanical Properties required property by ASTM A240 and ASME SA 240. 4340 E4 MILS-5000 1. AMS 4091 Superseded by AMS 4081 AMS 4092 Superseded by AMS 4082 AMS 4093 Superseded by AMS 4083 AMS 4113 6061-T6 Extruded shapes AMS 4115 6061-0 Cold. Status. 27, 1995. Classes 202, 302, and 305: When sensitization cannot be tolerated classes 202, 302 and 305 are not recommended for use. devcom-avmc. 4340 Alloy Steel. 1. Steel. Status. Version: F. 19, 1998. 65 0. Publication Date. american aircraft quality alloy steel bar-analysis cmnpmax. s max. Technical Data Sheet. 5CR - 10. Enter code: Categories 300M & 4340M Alloy Steel, Alloy Steel, DMS, Grades, McDonnell Douglas Specifications, Specifications. 4340 VAR AMS 6414 is a low alloy Chromium-Nickel-Molybdenum steel capable of being heat treated to high strength levels. SAE AMS-H-6875. si ni cr mo cu max. Critical updates of standards and customisable alerts and notifications. 455 Stainless Steel. AMS-S-6758 Specification 4130 Alloy Steel (MilSpec here) Steel Bars. 4. 4330M Alloy Steel. This product is not available online at this time. Feb. , e. Document Number. 60MN (CLAD ONE SIDE 2024-O), ANNEALED from SAI Global. Issuing Committee: AMS E Carbon and Low Alloy Steels Committee Publisher: SAE International. Alternate References are: 009935760,9510009935760,00-993-5760,AMS 2806,AMS-S-5000,MIL-S-5000,AMS2806,AMS-S-5000,MIL-S-5000AMS-5000 for the Beechjet 400A Ref. Learn More ». Inconel 625 ™ Super Alloy in Sheet, Strip and Plate. AMS 5564, AMS 5566, AMS 5569 (AMS-T-6845 noncurrent, MIL-T-6845D canceled) 304/LAMS 6484 Bars / Forgings N&T AMS-S-5000 MIL-S-8844 Cl1 ASTM A322 ASTM A331 AISI E4340 BMS-7-28 BPS-299-947-055 BPS-299-949-055. For detailed information and chemical analysis please visit the 4340 (E4340) steel page. טיטניום מפרטים: ams 4928, ams 6931, ams 4911, ams 4965, ams 6930, ams 4967, ams 4920, ams-t-9046, mil-t-9047, bms 7-269, dms 1570, dms 1592, ams 4907. , This specification covers premium quality, multiple vacuum melted, low alloy steel bars, reforging stock, and mechanical tubing intended for use at tensile strength levels of 260,000 psi (1795 MPa) and above. The heat treatment of. Cancelled. Revised. Alloy Steel AMS 6359 . S. S. Test procedures. AMS-S-5000 - BASE - SUPERSEDED -- See the following: AMS-6415 AMS-6484 Show Complete Document History. 75 0. AMS5085. 📝 Amendments Available. Please enable JavaScript to view the page content. tube/pipe: ams 6361 ams 6362 ams 63711. T. 4340 Alloy Steel. March 1, 2007. Titanium alloys. AMS 5571 Seamless tube. 416 ht r. plate/sheet/strip: ams 6350. HP9-4-30 High Strength Alloy Steel. REPLACED BY AMS-S-6758. 347 / 347H. 6Zn 2. AMS-S-5000 has a density of 7. Customers calling us for 4340 plate a lot of times are frustrated with on-time. 43%, manganese ranges from 0. 1. A-286 Stainless Steel. SCOPE: 1. Many contracts still call out MIL-T-9047 and AMS. Differences from AMS-H-6875 are a consequence of removing. AMS2750F is typically communicated via industry standards such as SAE/AMS specifications as well as customer purchase orders and part prints. Alloy Steel Round Bar offers good weldability without compromising steel abrasion and impact resistance, often used for structural applications in gears, fasteners, and aircraft applications. E. Revision Level ADOPT WITHDRAWN Status Superseded Publication Date March 3, 2010 Page Count 1 page AMS-S-5000 Steel, Chrome-Nickel-Molybdenum (E4340) Bars &. Popular Metal Grades. AMS 4091 Superseded by AMS 4081 AMS 4092 Superseded by AMS 4082 AMS 4093 Superseded by AMS 4083 AMS 4113 6061-T6 Extruded shapes AMS 4115 6061-0 Cold. Superseded By: Currently Viewing. 48 - 0. Page Count. AMS 5575 Welded tube. AMS 5654 Bars (aircraft quality)MIL-H-6875H, MILITARY SPECIFICATION HEAT TREATMENT OF STEEL, PROCESS FOR (1 MAR 1989) [S/S BY SAE-AMS-H-6875]. These are used for sealing and repairing integral fuel tanks and fuel cell cavities, for continuous service use from -65 to +250 °F (-54 to 121 °C). Its chromium content provides good hardness penetration, and the molybdenum imparts uniformity of hardness and high. 303 sul mill-s-7720, mil-w-52263 ams-5640 type 1, qqs-763c, qqs-764b, astm-a-582 astm-a-320 grd b8f. Subscribers can view annotate, and download all of SAE's content. sae ams s 6090 : 2006 : steel carburizing and nitriding, processes for: sae as 5944 : 1999 :. REV C CANCELLATION 1. ”. Talk To Us About the Alloys You Need Most. March 3, 2010. . com Performance metal solutions ISO 9001: 2008, AS9100: 2009 Revision CThis document is intended to replace MIL-H-6875 (cancelled) and AMS-H-6875 (stabilized) for new design or when approved by the Cognizant Engineering Organization (CEO) on existing design. Proposed changes to the standard by DoD activities must be submitted to the DoD Adopting Activity at Defense Standardization Program Office, 8725 John J. 5MO (316), SOLUTION HEAT TREATED from SAI Global. 17-4 (PH) Stainless Steel in Sheet, Strip and Plate. MIL-S-13165. 6×10^-6 in/ (in·°F). Talk To Us About the Alloys You Need Most. It is recommended that preheating or. 3 This test method specifies the use of air melted AISI E4340 steel per SAE AMS-S-5000 (formerly MIL-S-5000) heat treated to 260 – 280 ksi (pounds per square inch x 1000) as the baseline. mbx. May 1, 2009. AMS 6414 Alloy Steel. Product Forms: Steel Bars, Forgings, and Tubing. 40. LBS/FT:. , Da-Kang Village, Kuei-Sun, Taoyuan County. This combination of alloy and heat treat level. Magnesium alloys. All Grades.