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-5000 has a density of 7. Subscribers can. Document Number. . SAE AMS-S-5000. This specification applies to manufacturers and suppliers who heat treat aerospace material. Subscribers can view annotate, and download all of SAE's content. 2) and the requirements for furnace equipment, test procedures and information for heat-treating. 7225 42CrMo4 EN10083-1: UNS G41400 SCM 440: 4330 Mod VM N&T: AMS 6411 AMS 6427 MIL-S-8699 AMS 2300. 1) by users or their vendors or subcontractors. Status. Alloy: Specification: Thickness (inches) 2024-T351: AMS QQ A 250/4 AMS 4037 ASTM B 209. , Canada, Mexico, U. Search our products, such as 4340 steel, AMS 5643, AMS 5737 or many others, and receive a quote! Aero-Vac’s focus is on value added processing to help its customers reduce their overall costs and exposure. Electroless nickel plating is an process that codeposits a nickel-phosphorous alloy without need for an externally applied electrical current. 1. sae ams s 6090 : 2006 : steel carburizing and nitriding, processes for: sae as 5944 : 1999 :. Steel. Alloy Steel MIL-S-8699 . All Grades. 7 Cooling The load shall be cooled from the nitriding temperature in a suitable atmosphere to 300 °F (149 °C) or below. AMS 6931 6al/4v Titanium Alloy. 00%, and the remaining elements comprise the rest of AMS 6414’s composition. 9510-00-993-5760, BAR,METAL. 7M Pub Date 01/2015 >oupled Multiwaypoint VNAV – The C AMS-5000 calculates one vertical path through multiple lateral upgrade your Beechjet waypoints, enabling a fully stabilized descent or approach. Revision Level. Critical updates of standards and customisable alerts and notifications. , MIL-S-6090A, dated 4 June 1971, and Amendment 2 dated 20 July 1972, is hereby canceled. Mo. Chromium. 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. Type 321's general corrosion is less than Type 302 . 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]. SAE International. 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. The heat treatment of parts fabricated. 45CR (0. AMS 5558 Welded /thin wall tube. Carbon. Alloy 4140 (AISI 4140) is a low alloy steel containing Chromium and Molybdenum. ›. 0000. 38 - 0. AMS 6414 Alloy Steel. George VI had undergone a lung operation in September 1951 from which he never fully recovered. Aluminium Welding Wire;. Alloy 4130 is also vacuum degassed to meet the magnetic particle. 30 2. March 1, 2007. 80Cr. MIL-S-5000. Alloy Steel AMS 6304 (17-22A) Alloy Steel MIL-S-5000 . E4340, AMS. 2 Classification: Material shall be. Chromic Acid Anodizing - Class 5. 4340 High Tensile Steel in AMSS5000 Specification, per SAE International: “This specification covers electric furnace steel bars and reforging stock of. STEEL PLATE, SHEET, AND STRIP, ALLOY, 4130, AIRCRAFT QUALITY (S/S BY SAE-AMS6350, SAE-AMS6351 OR SAE-AMS6345. AMS-S-13165A SAE AMS-S-13165A - 6 - 3. All Grades. Steel Reforging Stock. Document History. SAE AMS S 6090 : 2006 : STEEL CARBURIZING AND NITRIDING, PROCESSES FOR: MIL-B-9946 Revision E:1987 : BIT, SCREWDRIVER, GENERAL SPECIFICATION FOR:4340 Alloy Steel. Round Bar, Flat Bar, Plate. Related Topics: Test procedures. Steel covered by this specification is intended for use in the manufacture of highly stressed aircraft parts requiring high hardenability. 1), Properties (3. This mil-spec covers the requirements for electrochemically-formed anodic coatings on aluminum and aluminum alloys for non-architectural applications. 888-922-2347 Send us a Message. Type 321 is used where resistance to intergranular corrosion is required and where the parts are subjected to sustained heating or cooling. DISCLAIMER: The use of this information should be considered strictly voluntary. 40 0. BAC 5019. A. 28 - 0. 8 Ni, 0. Publication Date. 3125, . Country: USA: Britain: Britain: Japan: Standard: ASTM A29: EN 10250: BS 970: JIS G4103: Grades: 4340: 36CrNiMo4/ 1. Hydraulic…SAE AMS S 13165 : 1997. 6415, AMS. AMSS5000. 0. Document Number. Grinding of Chromium Plate - Landing gear parts 275 KSI or above. Document Number. 6 Peening intensity: Unless otherwise specified on the drawing or in the contract, the. Learn more about its features, benefits and typical uses in this PDF document. 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. 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. , This specification covers premium quality, multiple vacuum melted, low alloy steel bars, reforging stock, and mechanical tubing intended for use at. Infostore. Steel is a material with a mass content of iron larger than the content of any other chemical element, and with a carbon content of usually less than two percent. All Grades. S. Steel Tubing. MIL-S-5000 › Complete Document History Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock (Superseded by SAE AMS-S-5000) How to Order Standards We ProvideAMS 6414 Alloy Steel. SPECIFICATIONS: Avion Alloys services Blue Chip customers worldwide with prime top-quality metals like AH 36 bars procured exclusively from United States Mills. HP9-4-30 High Strength Alloy Steel. We carry, process and forge AMS 5621 Specification 420 Stainless Steel. Reference to AMS2759 on a drawing, fabrication order, purchase order, etc. Status. titanium. 1 to note that Mil-H-6875 would now apply only to “raw materials” whereas “parts” would be processed in accordance to AMS 2759 E. Steel Reforging Stock. AMS 2700. It is recommended that preheating or. Document Number. ALLOY ROD/BAR HEX 4340 AMS-S-5000 1. 5 w% Sodium Dichromate, 120-130ºF, 20 minutes minimum Type III – Withdrawn Type IV – Withdrawn Type V – Withdrawn Type VI – 25-45 v% Nitric, 70-90ºF, 30 minutes minimum Type VII – 20-25 v% Nitric, 120-150ºF, 20 minutes minimumSteel, 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. 1. , This specification covers procedure requirements for shot peening of metal parts, to induce residual compressive stresses in specified surfaces, for the purpose of improving resistance to fatigue, stress corrosion cracking, and galling. Due to E-4340's high alloy content it obtains a uniformed hardness by heat treatment. 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. Superseded By. 6000 - Magnesium / Silicon - good machinability, corrosion resistance, moderate strength. Kalama, W98625 USA PH: 877-AEROVAC (877-237-6822) FX: 360-673-0100 sales@aerovacalloyforge. Buy SAE AMS H 6875 : 2010, the susperseded specifications for heat-treatment of four classes of steel, from SAE International. MIL-S-8784. MIL-S-6758 Specification 4130 Alloy Steel (AMS Spec here) Steel Bars. AMS 5604. Carbon. TITANIUM AND TITANIUM ALLOY BARS (ROLLED OR FORGED) AND REFORGING STOCK, AIRCRAFT QUALITY (S/S BY SAE-AMS-T-9047) SAE AMS-S-8802. AMS 6931 6al/4v Titanium Alloy. 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;. 4340 Alloy Steel. HP9-4-20 High Strength Alloy Steel. 6al/4v Alpha/Beta Titanium Alloy. 70 0. 9510-00-228-9735, BAR,METAL. 2500. Aug. SCOPE: 1. 1. Effective January 1, 2009, the requirements of the latest issue of AMS 2430 shall be fulfilled whenever reference is made to the cancelled AMS-S-13165. REPLACED BY AMS-S-6758. 38 - 0. 1) per SAE AMS 6414, and both are heat treated to 260 to 280 ksi (pounds per square inch ×1000). Steel Tubing. 316L Condition A Sheet, Strip, Plate QQ-S-766 AMS 5507 Not in MMPDS. Titanium Industries Inc. 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,. A-286 Stainless Steel. 00 Features and benefits • High Strength (1800MPa) • Good ductility • Resistant to shock • Excellent transverse properties in VAR material AMS 6415 / 6414 (4340) | A fatigue-resistent alloy with high toughness and strength PER BAC 5617, AMS-H-6875 Heat Treat Alloy Steel,AMS 6414,AMS 6415,AMS-S-5000 CAPABLE OF AMS 6359 BOEING; LONG BEACH DMS 1555 GRADE A Port of Kalama 2615 N. 010 0. 36% to 0. , This specification covers electric furnace steel bars and reforging stock of aircraft quality. Tensile strength. 80/1. March 1, 1999. Related Topics: Aluminum alloys. , 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. 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. Our service centers are located throughout the U. Your support ID is: 1013750275635199346. 187" (4. Superseded date: 04-11-2012. E. 595A colour chart. AMS6361G. 500, . Perry, was at the forefront of military specification reform. Magnesium alloys. 625, . Inconel 718 ™ Super Alloy in Sheet, Strip and Plate. AMS 6265 Alloy Steel. , This specification covers chrome-molybdenum (4140) steel bars, rods, and forging stock of aircraft quality. Issuing Committee: AMS F Corrosion and Heat Resistant Alloys Committee Publisher: SAE International. AMS 6414 Alloy Steel. We speak metal!321 Stainless Steel. Users may refer to SAE-AMS-S-6090, "Steel Carburizing and Nitriding,. Revision Level. Heat Treatment of Steel Raw Materials. Are you looking for a high-performance steel alloy for your aerospace applications? Check out LIBERTY Steel Group's AMS 6415 / 6414 (4340) steel, which offers high strength, good ductility, shock resistance and excellent transverse properties. Status. Please request a quote below or head over to the general catalog by clicking the "Products" link in. MIL MIL-S-5000E STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS, AND FORGING STOCK (S/S BY SAE-AMS6415P AND SAE-AMS-S-5000) (SUPERSEDING. 1. 25 APPlicAtionS — Intended for use in the manufacture of parts and components with sections 1/2” thick or less at time of heat treatment which require a through- ASM Aerospace Specification Metals Inc. 661. 2002-11-21. 1 Scope: This specification covers chrome-molybdenum (4130) steel bars and forging stock of aircraft quality. Rationale: AMS-S-6758B has been declared Stabilized as it has been replaced by technically equivalent specifications. AMS-S-5000 Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock 2. 00: in: stk: 4130 rnd 1. 11, 2000. All Grades. Service Steel Aerospace stocks Premium Aircraft Quality produced double melted in an. 6×10^-6 in/ (in·°F). 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 e1417/e1417m 2021, e1 mil-a-8625 (superseded by mil-prf-8625) f amm 1 mil-c-5541 e AMS 6409 AMS 6414 AMS 6415 AMS 6454 ASTM A29 (4340) ASTM A320 (L43). STANDARD Steel Tubing, Seamless 0. AMS-S-5000. This grade of the alloy should be forged between 1950 and 2250 degrees F (or about 1066 to 1232 degrees C). Not in MMPDS. 38 - 0. February 1998 and replaced by AMS-S-13165. View all product details. Alloy E 4340 is a widely used deep-hardening constructional steel. Technical Data Sheet. mil-a-1058 . REV E CANCELLATION 2. REVISION D. tube/pipe: ams 6414 ams 6415 astm a519. SAE AMS-QQ-A-225/8 : Aluminum Alloy 6061, Bar, Rod, Wire, and Special Shapes; Rolled, Drawn, or Cold Finished. 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. Noncurrent. This Standard has been added successfully to your. 1 for sufficient time to produce the specified depth of case. AMS 6931 6al/4v Titanium Alloy. 6al/4v Alpha/Beta Titanium Alloy. SPECIFICATIONS: AISI4340, ASTM A 829 / A6 SAE J404, AMS 2252/ 2301/6359 SAE J404. 1), ASTM-A295 17-22 AMS 6304 COBALT ALLOYS 28CR-6Mo ASTM F1537. Historical. Usually supplied hardened and tempered to condition T in sections up to 100mm with a tensile strength of 850 - 1000MPa and aiming for this strength range in larger sections. HARD COAT (S/S BY AMS 2469)4340 Alloy Steel. Created Date: 8/24/2022 10:15:41 AMBuy SAE AMS 2485 : 2016 COATING, BLACK OXIDE from SAI Global. Talk To Us About the Alloys You Need Most. SAE AMS-S-5000. Sealing compound, temperature-resistant, integral fuel tanks and fuel cell cavities, high-adhesion (superseded by SAE AMS-S-8802). Metals. How to Order; Standards We Provide; Updating, Reporting, Audits. Alloy Steel AMS 6411 . D. Your Message. Use our Rapid Response RFQ to request a quote. 1 pageRationale: AMS-QQ-A-250/11 has been designated Cancelled and Superseded because equivalent technical requirements are provided by other specifications. 12, 1967. Grinding of Chromium Plate - Landing gear parts 275 KSI or above. 43%, manganese ranges from 0. 649. 3) test procedures. AMS-7727 : Kovar® Rod : For God gave us a spirit not of fear but of power and love and self-control. AMS-S-13165. 36-60. amrstndz@army. A-286 Stainless Steel. MIL-S-5000 | Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock (Superseded by SAE AMS-S-5000) | Document Center, Inc. Aero-Vac Alloys & Forge is the metal buyer's trusted resource - we speak metal! Skip to navigation Skip to content. 3Mo - 1. It has a density of 0. 00, 2. b, ams 6409, ams 6415, ams 6484, ams˜s˜5000 9310 vac melt ams 6265, ams 6267, bps 299˜947˜032, ems 56280, ems 56279, mil˜s˜83030, pwa lcs f˜17 ams 6260, mil˜s˜7393, ht˜5042 9310 air melt ams 6260, mil˜s˜7393, ht˜5042, pwa lcs f˜17 4330 mod. Superseded. )ULTRASONIC INSPECTION, THIN WALL METAL TUBING. ”. 6Cu 0. The furnace or retort should be purged with inert gas before opening. 40/. A-286 Stainless Steel. mil-a-13881 mil-a-13883 mil-a-21366 mil-a-22010-s/s by astm-d2564 mil-a-22895 mil-a-23941 mil. Buy SAE AMS S 5000 : 2007 STEEL, CHROME-NICKEL-MOLYBDENUM (E4340) BARS AND. Revision A, March 2007. Status: Withdrawn. Nickel Hex Bar . Although I don't know for certain, it's very likely that the AMS has diverged from the MIL. Steel 4340 is a medium-carbon nickel-chromium-molybdenum steel alloy with excellent tensile strength, toughness, and fatigue resistance. In the early 1990’s, US Secretary of Defense, William J. March 1, 1999. SAE revised the scope of paragraph 1. 23Cr (7075-T6) (7075-T651)Solution and Precipitation Heat Treated ASTM B209. 4130 Alloy Steel. Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock AMSS5000. 5000 Series Aluminum Sheet; 6000 Series Aluminum Sheet; 7000 Series Aluminum Sheet; Aluminum Checker / Tread / Diamond Plate; Aluminum Wire. Page Count. The Royal Roads University campus sprawls over 260 hectares of lush parkland, where you will find walking, hiking, and biking trails, magnificent examples of. ; For our AISI 4130 (E4130) aircraft quality steel products please visit the 4130 (E4130) steel section. AMS 5516. Steel Sheets. Publication Date. SAE AMS-S-5000A-2007 (SAE AMS-S-5000A-2007) Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock (Cancelled: Mar 2007) This specification covers electric furnace steel bars and reforging stock of aircraft quality. SAE AMS-QQ-S-763. To request the addition of new colors, please send a paint sample (on an acceptable substrate) to the SAE contact below. 43C) Buy SAE AMS S 6090 : 2006 STEEL CARBURIZING AND NITRIDING, PROCESSES FOR from SAI Global. forging: ams 6382 astm a 646. Titanium alloys. Customers calling us for 4340 plate a lot of times are. Copper. Nickel Hastelloy . STEEL SHEET AND STRIP 0. . Prior to that date, processors may perform shot peening in accordance with AMS-S-13165 or AMS 2430. Alloy, Seamless. BMS-7-26 Boeing Spec Alloy Steel. 48, 160 Lane, Da Hoo Rd. Metal finishing. Welcome to EverySpec. C Si Mn P S Cr Mo Ni Cu Cu Min 0. The electrical resistivity of AMS-S-5000 is 7. AMS 6265 Alloy Steel. We carry, process and forge MIL-S-5626 Military Specification MilSpec 4140 Alloy Steel. Materials are available in sheets, plates and hex, square, flat and round bars. 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. If you require technical assistance or would like to receive a quote, please call our Customer Service team TOLL FREE at (866) 610-1660. 15. Titanium alloys. This alloy is known for its excellent mechanical properties, corrosion, and heat resistance. 0. 75 0. Alloy Designation: UK Specifications: US Specifications: US Federal Specifications: European Specifications: Other: 5005: BS N41 5005 : A-G0. 4. 4340 Alloy Steel. All Grades. Rationale: AMS-S-5000A was issued to cancel and supersede AMS-S-5000 with current, technically equivalent specifications. AMS 6931 6al/4v Titanium Alloy. CANCELLATION NOTICE This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of March 2007 and has been superseded by the applicable AMS specifications listed below. 00, 1. Customers calling us for 4340 plate a lot of times are frustrated with on-time. 60MN (CLAD ONE SIDE 2024-O), ANNEALED from SAI Global. HP9-4-20 High Strength Alloy Steel. Revision Level. Publication Date. Alloy 4340 is known for its toughness and capability of. 1. No. QQ-P-35C/AMS-QQ-P-35A SPECIFICATIONS Passivation Types Type I – Withdrawn Type II – 20-25 v% Nitric, 2-2. Manufacturing processes. 302 stainless steel is available in Sheet, Strip, Plate, Angles, Bars (Round, Hexagon, Squares, Flats). MIL-S-6758 MilSpec Military Grade Alloy Steel. Pages: 7. 6×10^-6 in/ (in·°F). , AMS 2759/3 Heat Treatment Precipitation-Hardening Corrosion. Related Topics: Heat treatment. Publication Date. All Grades. Document Number. 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. 17-4 (PH) Stainless Steel in Sheet, Strip and Plate. 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. 0CR - 1. This specification is for a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. The balance of these elements makes AMS 6414 a high. DMS 2284. 38-0. 8mm). ASTM E 2422 : 2017 : REDLINE. 4340 Alloy Steel. 302 Foil (Shim) is available in various thicknesses. 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 Systems—Connector Tubes—General Specification and Part Standard: SAE AS 4510 :. 合金鋼 specs: bms 7-26, ams 6257, ams 6417, ams 6419, cps 4911, dms 1935, bms 6414, mil-s-8844, bms 7-28, mil-s-5000, ams 6409, ams 6415, ams 6484, ams-s-5000, ams. Manganese. How to Order; Standards We Provide; Updating, Reporting, Audits. All Grades. 25 . Email：hanjustdoit@gmtc. , 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. HP9-4-30 High Strength Alloy Steel. 9Ti - 0. Document Number. Corrosion resistant alloys. inspection standards of AMS 2301. 4130 ams-s-6758 0. Buy SAE AMS 5853 : 2012 STEEL, CORROSION AND HEAT-RESISTANT, BARS AND WIRE, 15CR - 25. Magnetic materials. Alloy Steel. A108, UNS. Heat treatment. 0000. May 1, 2009. 4340 Alloy Steel. 15 0. 27, 1995. STEEL, BARS, FORGINGS, AND TUBING, 1. Also known as: SAE AMS 5735 SAE MOBILUS. 006B - 0. Scope: This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. Historical. 1. 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]. 43%, manganese ranges from 0. 95 Cr, 0. Inconel X750 ™ Super Alloy in Sheet, Strip and Plate. Status. 33 .