CAUTION: The supersession information is valid as of the date of this notice and may be superseded by subsequent revisions of the superseding document. AMS 2403 BM L 041001 SAE Plating, Nickel General Purpose M&P AMS 2404 CH F 081201 SAE Plating, Electroless Nickel M&P AMS 2405 C 841010 SAE Electroless Nickel Plate, Low Phosphorous M&P AMS 2406 BV L 070501 SAE Plating, Chromium Hard Deposit M&P AMS 2408 CF J 081101 SAE Plating, Tin M&P AMS 2410 J 040301 SAE. Rationale:AMS 5685K has been designated cancelled and superseded since equivalent technical requirements are contained in AS5685. 302 Foil (Shim) is available in various thicknesses. đ Amendments Available. đ Amendments Available. We carry, process and forge MISC Lockheed Martin Corporation Spec STM05-602 Grade 13-8Mo Stainless Steel. 3). 6al/4v Alpha/Beta Titanium Alloy. AMS 4091 Superseded by AMS 4081 AMS 4092 Superseded by AMS 4082 AMS 4093 Superseded by AMS 4083 AMS 4113 6061-T6 Extruded shapes AMS 4115 6061-0 Cold. 4571 afnor z6cnd17-11 afnor. 1. 3) in accordance with this standard. AMS 5571 Seamless tube. March 1, 2007. Status. Aluminum. 1. TITANIUM AND TITANIUM ALLOY BARS (ROLLED OR FORGED) AND REFORGING STOCK, AIRCRAFT QUALITY (S/S BY SAE-AMS-T-9047)Buy SAE AMS S 5000 : 2007 STEEL, CHROME-NICKEL-MOLYBDENUM (E4340) BARS AND REFORGING STOCK from SAI GlobalBoeing Helicopter support only, Per D8-5000 Finish Code VF-1. Buy SAE AMS 4077 : 2015 ALUMINUM ALLOY SHEET AND PLATE, ALCLAD ONE SIDE, 4. 60Mn (2024-T3) (2024-T351) Solution Heat Treated QQ-A-250/4. Related Topics: Heat resistant materials. AnAlySiS P S ni c Mn Max. Find Standards By. AMS S 8802 standardizes the specifications for temperature-resistant, two-component synthetic rubber compounds of the polysulfide type. 4340 RD BAR COND C 2. HydraulicâŠSAE AMS S 13165 : 1997. AMS 6414 sheet is an alloy steel that consists of carbon, manganese, chromium, molybdenum, vanadium, and nickel. Buy SAE AMS 2251 : 2013 TOLERANCES, LOW-ALLOY STEEL BARS from SAI Global. Heat treatment. 3), Reports (4. 05C) (SAE 52100), PREMIUM AIRCRAFT-QUALITY, CONSUMABLE ELECTRODE VACUUM REMELTED. The requirements of the individual specification applicable to the form required shall be fulfilled whenever reference is made to this specification. AMS 6409 is a chromium-cobalt-molybdenum alloy that offers superior corrosion resistance, high strength and heat resistance for applications requiring increased wear and fatigue properties. K, France, Singapore, and Shanghai. Buy SAE AMS S 5000 : 2007 STEEL, CHROME-NICKEL-MOLYBDENUM (E4340) BARS AND REFORGING STOCK from SAI GlobalMIL S. 1, 3. 38 - 0. 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). Dec. 25Mo (0. A-286; 13-8MO; 15-5PH; 17-4PH; 316; 321; 400; 455; 300M/4340M;. Revision Level. LAMINATED SHEET. 40ti (321), solution heat treated from sai global. All Grades. AMS 6414 Alloy Steel. Technical Data Sheet. Created Date: 8/24/2022 10:15:41 AMBuy SAE AMS 2485 : 2016 COATING, BLACK OXIDE from SAI Global. s max. 4), and Identification (5. This document is available in either Paper or PDF format. american aircraft quality alloy steel bar-analysis cmnpmax. Having a lower carbon content improves weldability. Description: This is a low alloy VAR steel, capable of achieving high strength levels through quench and tempering, it has a high nickel and cobalt content to promote toughness and hardenability. 3. Electroless nickel plating is an process that codeposits a nickel-phosphorous alloy without need for an externally applied electrical current. 5Mg 0. AMS-S-13165 was made redundant by AMS 2430 and AMS 2432. 4340 Alloy Steel. 5MO (316), SOLUTION HEAT TREATED from SAI Global. Quality assurance. 55C (SAE 1050) from SAI Global. 4340 Alloy Steel. All Grades. Standard Digital Reference Images for Inspection of Aluminum Castings. Publication Date. STEEL PLATE, SHEET, AND STRIP, ALLOY, 4130, AIRCRAFT QUALITY (S/S BY SAE-AMS6350, SAE-AMS6351 OR SAE-AMS6345. , The Department of Defense has determined it no longer has an interest in SAE-AMS-H-6088, "Heat Treatment Of Aluminum Alloys" and is withdrawing its adoption. MIL-STD-2154 Military (Department of Defense) Specification MilSpec Alloy Inspection MilSpec Ultrasonic Inspection. AMS 5604. com, your premiere source for free downloads of government and military standards, specifications, handbooks, and documents. 8 Ni, 0. Pages: 7. Heat treatment. 2002-11-21. This blog. Talk To Us About the Alloys You Need Most. 0. Si cr Max. July 1, 1998 Steel, Chrome-Molybdenum (4130) Bars and Reforging Stock (Aircraft Quality) 1. 38 - 0. New and revised standards are added to the database automatically upon publication, so database subscribers always have access to the most current information. SAE AMS-S-6758. The AMS-5000 installation requires replacing the integrated avionics processing system (IAPS) and associated components to provide the latest technology available for the Pro Line 4 system. 000 HEX. A. specifications: aisi4340, astm a 829 / a6 sae j404, ams 2252/ 2301/6359 sae j404 Castle Metals stocks Alloy 4340 plate through our global distribution network. 3V AMS5735 â available for purchase at $48. d2-5000 psd: 9-1, 9-3 d6-5000 br d8-5000 p d8-5000 psd: 8-57 dms1786 p dms1786 030-mc dms2433 b. Steel Extrusions. No. , This specification presents requirements for the carburizing and nitriding of carbon and allow steels to produce the mechanical properties specified by drawings, detail specifications,. Use our Rapid Response RFQ to request a quote. This is a standard used by the aerospace industry to describe and control the passivation of stainless steel. ÂŒ Hard MIL-S-5059 AMS 5907 MMPDS Section 2. This combination of alloy and heat treat level. Also known as: SAE AMST 9047 SAE MOBILUS. 661. 6Zn 2. AMS-S-5000 Specification 4340 High Tensile Steel (MilSpec here) Steel Bars. 5NI - 1. , Canada, Mexico, U. SAE AMS-H-6875. Materials are available in sheets, plates and hex, square, flat and round bars. 1 Al. BAC 5019. BMS-7-26 Boeing Spec Alloy Steel. 010 0. 4130 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 Bar MIL-S-8844D, MILITARY SPECIFICATION: STEEL BAR, REFORGING STOCK, AND MECHANICAL TUBING, LOW ALLOY, PREMIUM QUALITY (30-JUN-1987) [S/S BY SAE-AMS6414 AND SAE-AMS6257]. All Grades. SAE AMS-S-5000. February 1998 and replaced by AMS-S-13165. For our AISI 4130 (E4130) aircraft quality steel products please visit. SAE-AMS-H-6088, WITHDRAWAL OF ADOPTION NOTICE: HEAT TREATMENT OF ALUMINUM ALLOYS (27-JAN-2010) [SUPERSEDES MIL-H-6088H] [NO S/S DOCUMENT]. Withdrawn. 50: si: stk:. This alloy is known for its excellent mechanical properties, corrosion, and heat resistance. AMS 6265 Alloy Steel. Alloy Designation: UK Specifications: US Specifications: US Federal Specifications: European Specifications: Other: 5005: BS N41 5005 : A-G0. Specifications: AMS 4144; AMS A 22771; AMS STD 2154; BSS 7055; ASTM B594; AMS 2772; AMS STD 2154; BAC 5439; ASTM B 594; CLASS A. Simple online access to standards, technical information and regulations. 4340 High Tensile Steel in AMSS5000 Specification, per SAE International: âThis specification. Alloy Steel MIL-S-83030 . 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. Status. AMS 5558 Welded /thin wall tube. 92. Revision Level. 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. Steel. 40 Mo, 0. Use our Rapid Response RFQ to request a quote. 1 for sufficient time to produce the specified depth of case. MIL-S-40046D (NOTICE 1), MILITARY SPECIFICATION: SLING, FLAGSTAFF (08-JAN-1999) MIL-S-9479C (NOTICE-1), MILITARY SPECIFICATION: SEAT SYSTEM, UPWARD. , This specification covers electric furnace steel bars and reforging stock of aircraft quality. 82 Cr, 1. , The purpose of this military standard is to prescribe the non-destructive testing acceptance criteria for the inspection of metal castings that are classified (see 1. May 1, 1999 Sealing Compound, Temperature Resistant, Integral Fuel Tanks and Fuel Cell Cavities, High Adhesion ams-s-8802. Revised. REVISION E. 3 Military and Federal Standards and Commercial Item Descriptions:4MIL-S-7720A, MILITARY SPECIFICATION, STEEL, CORROSION,RESISTANT (18-8) BARS, WIRE AND FORGING STOCK (AIRCRAFT QUALITY) (25 OCT 1967) [S/S BY SAE-AMS-S-7720] MIL-S-7720A, MILITARY SPECIFICATION, STEEL, CORROSION,RESISTANT (18-8) BARS, WIRE AND FORGING STOCK (AIRCRAFT. Cancelled. Production. 2301, ASTM. Here's a link to the history of the MIL, and here's a link to the history of the AMS. mbx. Alloy Steel AMS 6411 . Add to Watchlist. Nickel Hex Bar . 6al/4v Alpha/Beta Titanium Alloy. 26/32 qqs-763c cond h, qqs-764b cond t, astm-a-582 cond t, mil-w-52263. Because this revision clarifies changes from revision D, changes for both revisions are maintained. Metals. Technical Data Sheet. Talk To Us About the Alloys You Need Most. The heat treatment of parts fabricated. Revision Level. Tensile strength. 44 C, 1. 40. Federal Standard 595C from 2008 has now been cancelled and has been superseded by AMS Standard 595A from 2016 and adminstered by SAE®. Apr 22, 2015 #3MIL-S-8802. Document Number. Alloy 4140 is the most widely used alloy for oil patch applications. Chromic Acid Anodizing - Class 5. 6×10^-6 in/ (in·°F). Aero-Vac Alloys & Forge is the metal buyer's trusted resource - we speak metal! Skip to navigation Skip to content. Buy SAE AMS 5853 : 2012 STEEL, CORROSION AND HEAT-RESISTANT, BARS AND WIRE, 15CR - 25. S. sheet/strip/plate: ams 6359 astm a505. 2738 FAX: 210. 7. Feb. AMS 2403 BM L 041001 SAE Plating, Nickel General Purpose M&P AMS 2404 CH F 081201 SAE Plating, Electroless Nickel M&P AMS 2405 C 841010 SAE Electroless Nickel Plate, Low Phosphorous M&P AMS 2406 BV L 070501 SAE Plating, Chromium Hard Deposit M&P AMS 2408 CF J 081101 SAE Plating, Tin M&P AMS 2410 J 040301 SAE Plating, Silver Nickel Strike, High. MIL-S-5626C, MILITARY SPECIFICATION: STEEL, CHROME-MOLYBDENUM (4140) BARS, RODS, AND FORGING STOCK (FOR AIRCRAFT APPLICATION) (17 JUL 1968) [S/S BY SAE-AMS6382, AND SAE-AMS6349]. A description is not available for this item. Chemicals. 316L Condition A Sheet, Strip, Plate QQ-S-766 AMS 5507 Not in MMPDS. 4330M Alloy Steel. 3 This test method specifies the use of air melted SAE 4340 steel (Grade A, see 7. March 3, 2010. Titanium Industries Inc. 60 . Victoria San Juan Cruises sails May through October between Bellingham,. 376. superseded by ams 2700) a ams-qq-p-416 f astm e1417/e1417m 21 mil-a-8625 (superseded by. SPECIFICATIONS: Avion Alloys services Blue Chip customers worldwide with prime top-quality metals like AH 36 bars procured exclusively from United States Mills. 1 Scope: This specification covers chrome-molybdenum (4130) steel bars and forging stock of aircraft quality. 455 Stainless Steel. mil-a-3316 mil-a-3920. 750, . 85 0. MIL-STD-2175A, MILITARY STANDARD: CASTINGS, CLASSIFICATION AND INSPECTION OF (25 AUG 1993) [S/S BY SAE-AMS-STD-2175]. MIL-S-5000 | Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock (Superseded by SAE AMS-S-5000) | Document Center, Inc. THE METAL BUYERSâ TRUSTED RESOURCE. SAE AMS 6415 : 2016. HP9-4-20 High Strength Alloy Steel. Revision Level. 4340 Alloy Steel. 17-4 (PH) Stainless Steel in Sheet, Strip and Plate. Publication Date. MIL S-5000 SAE J1397 (4340) SAE J404 (4340) SAE J412 (4340) UNS G43400: Chemistry Data. Steel, Chrome-Molybdenum (4130) Bars and Reforging Stock (Aircraft Quality) (Superseded by SAE AMS-S-6758) To find similar documents by Federal Supply Class Code: FSC 9510 (Bars and Rods) ORDER. February 1998 and replaced by AMS-S-13165. AMS6361G. 7225 42CrMo4 EN10083-1: UNS G41400 SCM 440: 4330 Mod VM N&T: AMS 6411 AMS 6427 MIL-S-8699 AMS 2300. 0. Credit Cards Accepted: In Business to SERVE CHRIST. 75-110. Steel Blocks. Metallurgy. MIL-S-6090A (NOTICE-3), MILITARY SPECIFICATION: STEELS USED IN AIRCRAFT CARBURIZING AND NITRIDING, PROCESS FOR (20 AUG 1998) [S/S BY SAE-AMS-S-6090]. K, France, Singapore, and Shanghai. Having a lower carbon content improves weldability. Description / Abstract: SAE AMS-QQ-P-35, Revision A, February 2005 - Passivation Treatments for Corrosion-Resistant Steel. We now reference and conform to AMS 2430 and AMS 2432. These include high strength at elevated temperatures, good high-temperature corrosion resistance up to 1300 °F (700 °C), and excellent low-temperature non-magnetic strength, down to -320 °F (-196 °C). Alloy, Seamless. 5000 Series Aluminum Sheet; 6000 Series Aluminum Sheet; 7000 Series Aluminum Sheet; Aluminum Checker / Tread / Diamond Plate; Aluminum Wire. The colours depicted on the following chart are for guidance only. Alloy Steel AMS 6359 . 80Cr - 1. Aug. HP9-4-20 Round Bar. 4140 AMS 6382, AMS-S-5626, 4340 AMS 6415, AMS-S-5000 8740 AMS-S-6049, AMS 6322 9310 AMS 6260 52100 BAR AMS 6440, AMS-S-7420 (Less Par. E. Prior to that date, processors may perform shot peening in accordance with AMS-S-13165 or AMS 2430. 95 Cr, 0. 38 - 0. Processes: This specification presents requirements for the carburizing and nitriding of carbon and alloy steels to produce the mechanical properties specified by drawings, detail metal. Tensile strength. 65 0. Revision Level ADOPT WITHDRAWN Status Superseded Publication Date March 3, 2010 Page Count 1 page AMS-S-5000 Steel, Chrome-Nickel-Molybdenum (E4340) Bars &. 1. 4340 air melt bms 7Ë28, milËsË5000, dms 1555 gr. The high fatigue strength makes E4340 ideal for highly stress parts as it maintains it's strength and hardness at elevated temperatures. 3 Military and Federal Standards and Commercial Item Descriptions:4SEAL, BONDED, ALUMINUM ALLOY 6061-T6, AMS4027, MOLD IN GROOVE, NBR RUBBER, AMS-P-5315: SAE AS 85052 : 2015 : CLAMP ASSEMBLY, LOOP TYPE, CUSHIONED, GENERAL SPECIFICATION FOR: SAE J 24714 : 2001 : Fluid SystemsâConnector TubesâGeneral Specification and Part Standard: SAE AS 4510 :. Customers who bought this document also bought: MIL-S-46850 Steel: Bar, Plate, Sheet, Strip, Forgings, and Extrusions, 18 Percent Nickel Alloy, Maraging, 200 Ksi, 250 Ksi, 300 Ksi, and 350 Ksi, High Quality QQ-N-286 Nickel-Copper-Aluminum Alloy, Wrought (Uns N05500) QQ-S-763 Steel Bars, Wire, Shapes, and Forgings; Corrosion ResistantAluminium Alloy 5000. MIL-S-46033 - STEEL BARS, CARBON and ALLOY, ROUND, SQUARE, and FLAT (FOR SPRINGS) (Use ASTM-A29/A29M) MIL-S-46042 - Steel, Corrosion and Heat Resistant Bar and Forgings (No Superseding Document) MIL-S-46047 - Steel, Bars and Blanks (1-3/4 Inches and over in Diameter) for Barrels of Small Arms Weapons. 43C) Buy SAE AMS S 6090 : 2006 STEEL CARBURIZING AND NITRIDING, PROCESSES FOR from SAI Global. 1 page 455 Stainless Steel. Heat treatment. Perry, was at the forefront of military specification reform. Chrome Vanadium Com K15048 Aâ231 6150 10270â2 2803 735A50 HS OT Chr. astm-d2564. In the early 1990âs, US Secretary of Defense, William J. I. Mo. 010 0. Steel Carburizing and Nitriding, Processes for. Showing 1 to 25 of 88 entries. 43 C. AMS 5575 Welded tube. Cancelled. 3Mo - 1. Sept. As aviation enthusiasts we are pleased to serve all of your aircraft alloy needs. One of the most versatile stainless steel alloys is AMS-S-5000. 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,. Defense industry. mil-a-907. AMS-S-6758. . All Grades. Steel. 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. Version: F. 2 Mo, 1. 36-60. Document Number. Aluminium Alloy 5000. Tempers: 01, T74, T7452 Specifications: AMS 2772; AMS A 22771; AMS 4108, AMS H 6088; AMS STD 2154; BAC 5439 CL A TY I; BMS7-214 Type II; BSS 7055; CLASS A ; GSS 16100 ALL CL A;. REV C CANCELLATION 1. DISCLAIMER: The use of this information should be considered strictly voluntary. Publication Date. MIL-S-5000, AMS-S-5000 (Both are canceled and superseded by AMS 6415) MIL-S-8844 299-947-055 Bell Helicopter SS 9702 Sikorsky DMS 1555 Boeing (Previously McDonnell. MIL-S-6758B, MILITARY SPECIFICATION: STEEL, CHROME-MOLYBDENUM (4130) BARS AND REFORGING STOCK (AIRCRAFT QUALITY) (18 MAY 1993) [S/S BY SAE-AMS-S-6758]. 500 x 36 x 96: 144. 25 APPlicAtionS â Intended for use in the manufacture of parts and components with sections 1/2â thick or less at time of heat treatment which require a through- ASM Aerospace Specification Metals Inc. 00%, and the remaining elements comprise the rest of AMS 6414âs composition. 4Cu 1. 455 Stainless Steel. Changed AMS I-6875 to AMS-H-6875. Dec. Rockwell Collins is offering a dual AMS-5000 system a two-year warranty and will replace or update required line replaceable units (LRUs). BRS-110103. Manganese. 40-0. 7004 State Route 123 Franklin, OH 45005 . 25 . SAE AMS-S-7720. SAE AMS-S-5000. 3 ConditionAMS-6532 Aermet 100 AMS-77184750 (Exc. All Grades. MIL-S-5000E, MILITARY SPECIFICATION: STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS, AND FORGING STOCK (12-NOV-1982) [S/S BY SAE-AMS-S-5000]. 45CR (0. AMS 4037 2024 Aluminum Alloy, Aluminum Sheets and Aluminum Alloy Plate 4. It is considered similar but not equivalent, as it does not cover parts (refer to AMS2759). 4. Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard. AMS ASME; 1050: Aluminum Coil: Aluminum Strip: Aluminum Plate: 1060: Aluminum Coil: ASTM-B209: Aluminum Strip. AMS2750F is typically communicated via industry standards such as SAE/AMS specifications as well as customer purchase orders and part prints. Document Number. Many contracts still call out MIL-T-9047 and AMS. Explore our McDonnell Douglas Specifications product category. Due to E-4340's high alloy content it obtains a uniformed hardness by heat treatment. 2 Timothy 1:7 . Revision Level. EmailïŒhanjustdoit@gmtc. Superseded. Please request a quote below or head over to the general catalog by clicking the "Products" link in the side bar. This specification covers the requirements for heat-treatment of four classes of steel (See 1. SAE AMS-QQ-S-763. 00 0. This specification covers electric furnace steel bars and reforging stock of aircraft quality. Durability. EN ISO 15156-2 - PETROLEUM AND NATURAL GAS INDUSTRIES - MATERIALS FOR USE IN H [2]S CONTAINING ENVIRONMENTS IN. AMS 6414 Alloy Steel. Tensile strength. Contact the customer service department at 859-335-5100 for the latest information on applicable test fees. All Grades. 1) per SAE AMS 6414, and both are heat treated to 260 to 280 ksi (pounds per square inch ×1000). Please enable JavaScript to view the page content. S. 3 This test method specifies the use of air melted SAE 4340 steel (Grade A, see 7. Alloy 4340 is known for its toughness and capability of. Revision Level. AMS 6414 Alloy Steel. Your support ID is: 1013750275635199346. Enter code: Category Controls & Processes. Alloy Steel MIL-S-8699 . Alloy Steel MIL-S-7393 . SAE AMS 6484 and SAE AMS S 5000. Specifications. Issuing Committee: AMS F Corrosion and Heat Resistant Alloys Committee Publisher: SAE International. MIL-H-5606 petroleum base hydraulic fluid for military aircraft (inactive for new designs. AMS-S-13165. 000 HEX. Issuing Committee: AMS F Corrosion and Heat Resistant Alloys Committee Publisher: SAE International. Steel 4340 is a medium-carbon nickel-chromium-molybdenum steel alloy with excellent tensile strength, toughness, and fatigue resistance. February 1, 2003. AMS 2700 Method 1 is the nitric baths, essentially unchanged from QQ-P-35. 6Zn 2. sae ams s 6090 : 2006 : steel carburizing and nitriding, processes for: sae as 5944 : 1999 :. 4330M Alloy Steel. , This specification covers premium quality, multiple vacuum melted, low alloy steel bars, reforging stock, and mechanical tubing intended for use at. 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. 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. Buy SAE AMS S 5000 : 1999 STEEL, CHROME-NICKEL-MOLYBDENUM (E4340) BARS AND REFORGING STOCK from SAI Global. 2. For detailed information and chemical analysis please visit the 4340 (E4340) steel page. 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. Enter code: Categories 300M & 4340M Alloy Steel, Alloy Steel, DMS, Grades, McDonnell Douglas Specifications, Specifications. A-286 Stainless Steel. 75 0. AMS 6265 Alloy Steel. 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. MIL-S-5000, AMS-S-5000 (Both are canceled and superseded by AMS 6415) MIL-S-8844 299-947-055 Bell Helicopter SS 9702 Sikorsky DMS 1555 Boeing (Previously McDonnell Douglas) Superseded By: Currently Viewing.