Use our Rapid Response RFQ to request a quote. It provides details, methods, and procedures for these various. 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. E Notice 1 - Notice of cancellation/superseded by SAE AMS 6415. 1) exceptions to the transfer technique, allows a type 1 option (5. Heat treatment. For detailed information and chemical analysis please visit the 4340 (E4340) steel page. 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. New and revised standards are added to the database automatically upon publication, so database subscribers always have access to the most current information. In the early 1990’s, US Secretary of Defense, William J. Steel. E-52100, 52100. , This specification covers electric furnace steel bars and reforging stock of aircraft quality. Carbon. ASTM B117/AMS-STD-753: Method 104: Titanium Clean: ASTM B600: Abrasive/Chemical: NonDestructive TESTING (NDT) Process Specifications Description; Electrical Conductivity: ASTM E1004: Heat Treat Response: Fluorescent Penetrant Inspection: ASTM E 1417 *MIL-STD-6866 *MIL-I-6866: Defect Surface Discontinuities: Magnetic Particle Inspection:MIL-S-5000 Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock. 4340 Alloy Steel. Publication Date. March 1, 2007. 2MO - 2. 3125, . Subscribers can view annotate, and download all of SAE's content. tw; Taipei Branch Office. AMS 4109 7175-T736 Superseded by AMS 4149: WS 3. December, 2007, and has been superseded by AMS 2430, Shot Peening. 3) 6al-6v-2sn: ams 4918, ams 4936, ams 4937, ams 4971, ams 4978, ams 4979, mil-t-9046, mil-t-9047, uns 56620 6Al-6V-2Sn Titanium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. amrstndz@army. AMS 6265 Alloy Steel. 250 DIA. All Grades. 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. Steel Carburizing and Nitriding, Processes for. Qualified to SAE-AS81820 BODY BALL RACEDocument Number. qq-s-763 ams-s-7720 mil-s-5059 mil-s-7720: astm a240 / asme sa240 astm a167 / asme sa167 astm a666 astm a276 / asme sa276 astm a479 / asme a479 astm a484 / asme sa484 astm f138 astm a320 grd b8m astm a193 grd b8m cl1: bs 970; 316s31 / 316s12 en 58j: ws 1. 19, 1998. 8 word “end ”added before items 5. Heat treatment. 1 E300 Zinc Clear Zinc Zinc w/ Yellow Chromate QQ-P-325B Type I Clear Type II Yellow Class 1,2,3 ASTM B633 Type I Clear Type II Yellow PHONE: 210. STANDARD Steel Tubing, Seamless 0. AMSS5000. 6Zn 2. 01/714323 DC : DRAFT OCT 2001. It is not a coating and does not change any part’s dimensions. of MIL-S ( steel)MIL-S-5000E-4340 AEROSPACE. Rationale: AMS-QQ-S-763D stabilizes this document because this document is no longer state of the art and other documents contain similar but not necessarily equivalent requirements. Revision A, March 2007. All Grades. Revision Level. Grinding of Chromium Plate - Landing gear parts 275 KSI or above. 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. Technical Data Sheet. Use our Rapid Response RFQ to. 6 - 5005: 5052. AMS 6414 Alloy Steel. Tensile strength. 7. 7225 42CrMo4 EN10083-1: UNS G41400 SCM 440: 4330 Mod VM N&T: AMS 6411 AMS 6427 MIL-S-8699 AMS 2300. MIL-T-9047G Amendment 2 was cancelled, and superseded by SAE (Society of Automotive Engineers). We speak metal!302 mil-s-7720, ams-s-7720 astm-a-276, astm-a-479, asme-sa-479. Steel Sheets. 93 - 1. Due to E-4340's high alloy content it obtains a uniformed hardness by heat treatment. Alloy Steel MAT 137 . SAE AMS-S-5000. MIL-S-5000 | Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock (Superseded by SAE AMS-S-5000) | Document Center, Inc. Kalama, W98625 USA PH: 877-AEROVAC (877-237-6822) FX: 360-673-0100 sales@aerovacalloyforge. Steel covered by this specification is. Alloy 7050. Superseded. Alloy 4130 (AISI 4130) is a chromium molybdenum alloy steel being a widely used Aircraft Steel due to its weldability, ease of fabrication and mild hardenability. AMS-S-6758 has excellent physical properties. Superseded. This specification covers electric furnace steel bars and reforging stock of aircraft quality. Coatings, colorants, and finishes. , This specification covers premium quality, multiple vacuum melted, low alloy steel bars, reforging stock, and mechanical tubing intended for use at. Issuing Committee: AMS E Carbon and Low Alloy Steels Committee Publisher: SAE International. AMS 6414 Alloy Steel. BMS-7-26 Boeing Spec Alloy Steel. 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. 3). 9510-00-580-5486, BAR,METAL. 1. link] was cancelled and superseded by AMS2700 [affil link], which has a class 4 which is. Status. 2 Classification: The steel bars and reforging stock shall be as follows:. Enter code: Category Controls & Processes. 15 0. 00, 2. Use our Rapid Response RFQ to request a quote. Revision Level. SAE AMS-S-5000, Revision A, March 2007 - Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock. This alloy is known for its excellent mechanical properties, corrosion, and heat resistance. July 1, 1998 Steel, Chrome-Molybdenum (4130) Bars and Reforging Stock (Aircraft Quality) 1. 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. 55C (SAE 1050) from SAI Global. Alternate References are: 005805486,9510005805486,00-580-5486,SAE AMS 6415,AMS-S-5000,MIL-S-5000,SAEAMS6415,MIL-S-5000,AMS-S-5000GOLDEN WIN STEEL INDUSTRIAL CORP. 1. 1. Download File - 165. Its chromium content provides good hardness penetration, and the molybdenum imparts uniformity of hardness and high. , 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. , This specification covers chrome-molybdenum (4130) steel bars and forging stock of aircraft quality. All Grades. Document Number. MIL-S-13165C, MILITARY SPECIFICATION: SHOT PEENING OF METAL PARTS (07 JUN 1989) [S/S BY SAE-AMS-S-13165]. 25, 1. Titanium alloys. Our discussion here is driven by the fact that several end-users continue to use the original MIL specification for their peening operations. Buy SAE AMS 2175 : 2010 - non-destructive testing methods, sampling frequency, & acceptance criteria for the inspection of metal castings from SAE International. This combination of alloy and heat treat level. Steel covered by this specification is intended for use in the manufacture of highly stressed aircraft parts requiring high hardenability. , 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. 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. , This specification covers the requirements for heat-treatment of four classes of steel (see 1. (Copies of this document are available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001. Related Topics: Aluminum alloys. 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. 📝 Amendments Available. ASTM E 2422 : 2017 : REDLINE. 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. MIL-S-5000 | Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock (Superseded by SAE AMS-S-5000) | Document Center, Inc. Alloy Steel AMS 6409 . 17-4 (PH) Stainless Steel in Sheet, Strip and Plate. Customer Reviews - What Customers Say About Us! "Just wanted to say thanks for your efforts and updates" "I always try you as you often keep stock that can't be found elsewhere"superseded by MIL-A-8625) AMS-C-27725 D Coating, Corrosion Preventative, for Aircraft Integral Fuel Tanks, for Use to 250 °F (121 °C) AMS-H-6875 C Heat Treatment of Steel Raw Materials (Supersedes MIL-H-6875) AMS-H-6088 C Heat Treatment of Aluminum Alloys (This specification has been cancelled and has been. Having a lower carbon content improves weldability. To those users, I hope to provide a MIL-H-6875 H NOTICE 1 - NOTICE OF CANCELLATION FUTURE ACQUISITIONS FOR THIS ITEM SHOULD REFER TO SAE-AMS-H-6875, "HEAT TREATMENT OF STEEL RAW MATERIALS" Document Type: Standard: ISBN: Pages: Published: Publisher: US Military Specs/Standards/Handbooks : Status: Superseded: Superseded By: PIA H 6875 : 1997 ; Supersedes: MIL H 006875 : LATEST HARD COAT (S/S BY AMS 2469). 60 . This product is not available online at this time. . 5V (0. ; For our AISI 4130 (E4130) aircraft quality steel products please visit the 4130 (E4130) steel section. 95 Cr, 0. Minimum Mechanical Properties required property by ASTM A240 and ASME SA 240. Different grades of steel are achieved by adding other alloying elements, such as manganese, nickel, chromium, titanium and molybdenum to the basic mix. 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. Our extensive product offerings include alloy, stainless, nickel, aluminum, titanium, carbon and cast iron. This mil-spec covers the requirements for electrochemically-formed anodic coatings on aluminum and aluminum alloys for non-architectural applications. AMS 4045 7075 Aluminum Alloy, Aluminum Sheets and Aluminum Alloy Plate 5. Classes 202 and 302: Class 302 is intended for use where severe corrosion is. Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock. , constitutes a requirement to conform to the applicable provisions of the documents. 4×10⁷ Ωm, making it a great electrical conductor. We stock and distribute quality alloy steel from the finest. March 1, 2007. March 3, 2010. SAE AMS-S-5000, Revision A, March 2007 - Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock Steel covered by this specification is intended for use in the manufacture of highly stressed aircraft parts requiring high hardenability. 40. 5NI - 1. 28 - 0. 5Mg 0. 4. Revision Level ADOPT WITHDRAWN Status Superseded Publication Date March 3, 2010 Page Count 1 page AMS-S-5000 Steel, Chrome-Nickel-Molybdenum (E4340) Bars &. 20Mo (0. AMS2750F is typically communicated via industry standards such as SAE/AMS specifications as well as customer purchase orders and part prints. Steel covered by this specification is intended for use in the manufacture of highly stressed aircraft parts requiring high hardenability. TITANIUM AND TITANIUM ALLOY BARS (ROLLED OR FORGED) AND REFORGING STOCK, AIRCRAFT QUALITY (S/S BY SAE-AMS-T-9047) SAE AMS-S-8802. Manufacturing processes. ALLOY ROD/BAR HEX 4340 AMS-S-5000 1. is a world wide supplier of quality alloy steel metals. Material UNS ASTM SAE/AISI AMS SAE EN FED JIS DIN BS O. 11,. Historical Revision Information. SAE International. 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. 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. 1), and results from a Five-Year Review and update of this specification. AMS 6370 Bar AMS 6371 Tube MIL-S-6758 MIL-S-18729 MIL-T-67366: AISI 4130 ASTM A322 ASTM A331: S534 S535 : UNS G41300: 4340 E4340: AMS 6359 Sheet / strip / plate AMS 6409 Bars / Forgings N&T AMS 6414 Vac Melt Bars / Forgings AMS 6415 Bars / Forgings AMS 6484 Bars / Forgings N&T AMS-S-5000 MIL-S-8844 Cl1: ASTM A322 ASTM A331 AISI E4340 : BMS-7-28. 48 - 0. Use our Rapid RFQ to request a quote. Title: Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock (S/S by SAE-AMS6415 and SAE-AMS6484) Scope: This specification covers electric furnace steel bars and reforging stock of aircraft quality. Available Forms: Popular Industry Specifications. Issuing Committee: AMS F Corrosion and Heat Resistant Alloys Committee Publisher: SAE International. 1 Inspection, Ultrasonic, Wrought Metals, Process SUPERSEDED BY AMS2175 Fusion Welding for Aerospace Application Superseded by SAE-AMS-6360,6361,6362 Tape and Sheet, Adhesive, Rubber and Cork Composition Tubing, Steel, Corrosion-Resistant S30400 1/8 H Tube, Alum. AMS 6414 Alloy Steel. AMS 5605. 000 HEX. 75, 2. AMS 5571 Seamless tube. AMS 4045 7075 Aluminum Alloy, Aluminum Sheets and Aluminum Alloy Plate 5. 40/. 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). How to Order; Standards We Provide; Updating, Reporting, Audits;United Aluminum’s Sales Department and talented metallurgy staff are available to assist you with any questions you may have on specifications applicable to aluminum coil and aluminum strip. 20 Mo. ALLOY ROD/BAR HEX 4340 AMS-S-5000 1. It has a density of 0. 420 qqs-763, ams-5621, astm-a-276. Alloy 4140 is the most widely used alloy for oil patch applications. 625, . 4340 Alloy Steel. 649. Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard. MIL-S-5000 Revision E:1982 : Similar to: Standards Referenced By This Book - (Show below) - (Hide below) SAE AMS STD 2154 : 2017-05 : INSPECTION, ULTRASONIC, WROUGHT METALS, PROCESS. Titanium alloys. S. Sorta. 1950. . 95 Cr, 0. 43 0. . Revision Level. MIL-S-5000 | Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock (Superseded by SAE AMS-S-5000) | Document Center, Inc. mil-a-5540. 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]. 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. 60Mn (2024-T3) (2024-T351) Solution Heat Treated QQ-A-250/4. 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. Aeronautical Design Standard (ADS) Documents. 1. Page Count. QUALITY MANAGEMENT SYSTEMS - REQUIREMENTS FOR AVIATION, SPACE AND DEFENSE DISTRIBUTORS. Document Number. 32 KB. Buy SAE AMS 2251 : 2013 TOLERANCES, LOW-ALLOY STEEL BARS from SAI Global. SAE revised the scope of paragraph 1. HP9-4-20 High Strength Alloy Steel. Status. 80/1. 36% to 0. mil-a-13881 mil-a-13883 mil-a-21366 mil-a-22010-s/s by astm-d2564 mil-a-22895 mil-a-23941 mil. 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;. 80 Cr, 1. 6 - 5005: 5052. 4Cu 1. 9510-00-993-5760, BAR,METAL. TOLERANCES, CORROSION AND HEAT-RESISTANT STEEL TUBING. Version: F. A-286 Stainless Steel. Materials are available in sheets, plates and hex, square, flat and round bars. MIL-S-6758 › Steel, Chrome-Molybdenum (4130) Bars and Reforging Stock (Aircraft Quality) (Superseded by SAE AMS-S-6758) MIL-S-6758 - REV B CANCELLATION 1 - CANCELLED -- See the following: AMS-S-6758 Show Complete Document History. 1 for heat treatment of steel parts (see 8. All Grades. Created Date: 8/24/2022 10:15:41 AMBuy SAE AMS 2485 : 2016 COATING, BLACK OXIDE from SAI Global. George VI had undergone a lung operation in September 1951 from which he never fully recovered. 3. HP9-4-30 High Strength Alloy Steel. Find Standards By. Defense industry. Heat treatment. Talk To Us About the Alloys You Need Most. 1, 3. Claudia's Notes: Originally, the AMS-QQ-P-35 was just a reprint of the QQ-P-35C. SAE AMS-S-8802. It has a density of 0. Document History. 455 Stainless Steel. S. K, France, Singapore, and Shanghai. 0. E. In September 1999, MIL-T. 50: si: stk:. The displayed colour will depend on your monitor and browser and pearl or metallic colours. 69 in addtion to MIL-C-5056:. 8. 8 Ni, 0. All Grades. If you require technical assistance or would like to receive a quote, please call our Customer Service team TOLL FREE at (866) 610-1660. 95Cr - 0. Superseded By: Currently Viewing. The alloy’s melting point stands at approximately 2,800°F, and its coefficient of thermal expansion is 6. forgings: ams 6414 ams 6415 astm a646. ADS-10D-SP: Air vehicle technical description (Superseded by DI-SESS-82291) ADS-13F-HDBK: Air Vehicle Materials and Processes; ADS-20F-HDBK: Armament and Fire Control. Related Topics: Manufacturing processes. Having a lower carbon content improves weldability. MIL S-5000: AMS 6409 Specifications. Rationale: AMS5517M revises Composition analysis standards (3. Many contracts still call out MIL-T-9047 and AMS. 4401 ws 1. si ni cr mo cu max. , 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. Peening. MIL-S-6758 Specification 4130 Alloy Steel (AMS Spec here) Steel Bars. Talk To Us About the Alloys You Need Most. C Si Mn P S Cr Mo Ni Cu Cu Min 0. 4404 ws 1. 1. , Da-Kang Village, Kuei-Sun, Taoyuan County. MIL S-5000 SAE J1397 (4340) SAE J404 (4340) SAE J412 (4340) UNS G43400: Chemistry Data. SAE AMS-QQ-S-763. Tensile strength. Talk To Us About the Alloys You Need Most. AMS 2700. ¼ Hard MIL-S-5059 AMS 5907 MMPDS Section 2. sheet/strip/plate: ams 6359 astm a505. 35 0. Related Topics: Heat resistant materials. Chemicals. 8Ni - 0. View all product details. 595A colour chart. 5MO (316), SOLUTION HEAT TREATED from SAI Global. A. 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,. Buy SAE AMS H 6875 : 2010, the susperseded specifications for heat-treatment of four classes of steel, from SAE International. 6al/4v Alpha/Beta Titanium Alloy. Home; Why Us? Alloys. 1 for sufficient time to produce the specified depth of case. Available format(s): Hardcopy, PDF. EN ISO 13533:2002. 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. Grinding of Chromium Plate - Landing gear parts 275 KSI or above. BMS-7-26 Boeing Spec Alloy Steel. SAE MOBILUS. The alloy’s melting point stands at approximately 2,800°F, and its coefficient of thermal expansion is 6. 4330M Alloy Steel. AMS 5512 Sheet / strip / plate (steel, corrosion and heat resistant, sheet, strip and plate 18Cr 10. Alloy: Specification: Thickness (inches) 2024-T351: AMS QQ A 250/4 AMS 4037 ASTM B 209. ROD AND BAR. 33C) (SAE 4130) 125 ksi (862 MPa) Tensile Strength. tube/pipe: ams 6414 ams 6415 astm a519. We carry, process and forge MISC United States Federal GSA Specification QQ-S-766. This specification covers the specific requirements for 2024 aluminum alloy alclad plate and sheet; the general requirements are covered in AMS-QQ-A-250. 5000: 15-5ph ams5862 . AMS Specifications; SPEC Description UNS Number Alloy Quote Request; AMS 2241: Tolerances Heat Resistant Bars: RFQ:. Condition A AMS 5648 Not in MMPDS. 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. HARD COAT (S/S BY AMS 2469)4340 Alloy Steel. 2 Classification: Material shall be. Materials properties. 5V (0. 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. 13 Cr, 8. AMS-S-5000 Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock 2. 4340 Alloy Steel. Product availability:AMS2750F has been released for approximately 7 months now. Superseded By. 80Cr - 1. 1) per SAE AMS 6414, and both are heat treated to 260 to 280 ksi (pounds per square inch ×1000). MIL-S-8784. titanium. Dec. 7004 State Route 123 Franklin, OH 45005 . 35 . 30 2. 43C) (SAE 4340) Special Aircraft Quality Cleanliness Normalized and Tempered AMS6409MIL-S-5626 (superseded by AMS 6382 and AMS 6349) 4140 Alloy Steel, Bars, Rods, and Forging Stock C or later MIL-S-6758 (Superseded by AMS-S-6758) Steel, Chrome-Molybdenum (4130) Bars And Reforging Stock (Aircraft Quality) B or later MIL-S-81733, MIL-PRF-81733 Sealing and Coating Compound D or later . Titanium alloys. 4330M Alloy Steel. 00: in: stk: 302/304 wire . Publication Date. 4340 air melt bms 7˜28, mil˜s˜5000, dms 1555 gr. MIL-S-5000 Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock. Example product meeting this military specification: CS3204 Class A & B. Steel, Chrome-Nickel-Molybdenum (E4340) Bars & Reforging Stock. Castle Metals stocks Alloy 4340 plate through our global distribution network. 316L Condition A Sheet, Strip, Plate QQ-S-766 AMS 5507 Not in MMPDS. S. 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. 43%, manganese ranges from 0. AMS 6411 AMS 6427 MIL-S-8699 AMS 2300 AMS 6411 Bar Stock List: ASTM A646 : UNS K23080 BMS 7-122 BMS 7-27 CE-0906 EMS-96242 FMS-1012 GM-1010: 4340 E4340: AMS 6359 Sheet / strip / plate AMS 6409 Bars / Forgings N&T AMS 6414 Vac Melt Bars / Forgings AMS 6415 Bars / Forgings AMS 6484 Bars / Forgings N&T AMS-S-5000 MIL-S. 2) and the requirements for furnace equipment, test procedures and information for heat-treating procedures, heat-treating temperatures and material (See. MIL-S-5000E (NOTICE 2), MILITARY SPECIFICATION: STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS, AND FORGING STOCK (11 AUG 2000) [S/S BY SAE. 4340 RD BAR COND C 2. Noncurrent. Revision Level. 0. Historical. BMS-7-26 Boeing Spec Alloy Steel. HP9-4-30 High Strength Alloy Steel. Specifications. The carbon content ranges from 0. 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. Max. <br/>Your support ID is. 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. 38-0. February 1998 and replaced by AMS-S-13165. Showing 1 to 25 of 88 entries. Skip to content - Show main menu navigation below - Close main menu navigation below. This specification. mil-a-3316 mil-a-3920. We carry, process and forge MISC Lockheed Martin Corporation Spec STM05-602 Grade 13-8Mo Stainless Steel. 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. Revised. 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. 4340 Alloy Steel. SAE AMS 6484 : 2016. Publication Date. MIL-T-6845D, MILITARY SPECIFICATION: TUBING, STEEL, CORROSION-RESISTANT (S30400), AEROSPACE VEHICLE HYDRAULIC SYSTEM 1/8 HARD CONDITION (26-APR-1985) [S/S BY SAE-AMS-T-6845]. This specification covers a carbon steel in the form of sheet, strip, and plate. Superseded By. , This. Document Number. 00%, and the remaining elements comprise the rest of AMS 6414’s composition. Status. Alternate References are: 005558374,9510005558374,00-555-8374,AMS 6415,AMS-S-5000,MILS5000,AMS6415,AMS-S-5000,MILS5000MIL-S-6090 › Steels Used in Aircraft Carburizing and Nitriding, Process for (Superseded by SAE AMS-S-6090) MIL-S-6090 - REV A CANCELLATION 3 - CANCELLED -- See the following: AMS-S-6090 Show Complete Document History. Description / Abstract: SAE AMS-QQ-P-35, Revision A, February 2005 - Passivation Treatments for Corrosion-Resistant Steel. SAE AMS-S-5000. 1 page 455 Stainless Steel. Document Number. mil-a-8576-s/s by sae-ams-a-8576 mil-a-8623-s/s by mmm-a-134 mil-a-9117. 5MG - 0. 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. Alternate References are: 002289735,9510002289735,00-228-9735,AMS-S-5000,MILS5000,AMS 6484,AMS-S-5000,MILS5000,AMS6484This reference table lists some of the specs available.