BMS-7-26 Boeing Spec Alloy Steel. Tensile strength. 5000 Series Aluminum Sheet; 6000 Series Aluminum Sheet; 7000 Series Aluminum Sheet; Aluminum Checker / Tread / Diamond Plate; Aluminum Wire. AMS 4045 7075 Aluminum Alloy, Aluminum Sheets and Aluminum Alloy Plate 5. AMS-S-13165 was made redundant by AMS 2430 and AMS 2432. I recommend you purchase the AMS for your quotation. The alloy has a good combination of ductility, toughness and strength along with high hardenability and better depth of hardening than chrome-moly 4140 type alloys. MIL-S-5000. 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. , This specification covers electric furnace steel bars and reforging stock of aircraft quality. 20 Mo. val e4130 ams 6370 normalized rounds, squares and flats mil-6758 condition d1-d4 (mil-s 6758 superseded by ams-s-6758)ASTM S 8844 CL l, AMS 6414 AMS S 8814 CL 3, AMS 6417, AMS 6419 AMS 6487 AMS 6265 AMS 6370, AMS 6348, AMS-S-6758 AMS 6382, AMS-S-5626, AMS 6415, AMS-S-5000 AMS-S-6049, AMS 6322 AMS 6260 AMS 6440, AMS-S-7420 (Less Par. Steel Sheets. 6al/4v Alpha/Beta Titanium Alloy. PETROLEUM AND NATURAL GAS INDUSTRIES - DRILLING AND PRODUCTION EQUIPMENT - DRILL-THROUGH EQUIPMENT. com I pierce-spafford. This specification. 3. November 1, 2002. TITANIUM AND TITANIUM ALLOY BARS (ROLLED OR FORGED) AND REFORGING STOCK, AIRCRAFT QUALITY (S/S BY SAE-AMS-T-9047) SAE AMS-S-8802. , Canada, Mexico, U. Pages: 22. 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to say thanks for your efforts and updates" "I always try you as you often keep stock that can't be found elsewhere"superseded by MIL-A-8625) AMS-C-27725 D Coating, Corrosion Preventative, for Aircraft Integral Fuel Tanks, for Use to 250 °F (121 °C) AMS-H-6875 C Heat Treatment of Steel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. ADS-10D-SP: Air vehicle technical description (Superseded by DI-SESS-82291) ADS-13F-HDBK: Air Vehicle Materials and Processes; ADS-20F-HDBK: Armament and Fire Control. 38 - 0. 1. Passivation is a process of making stainless steel more stainless (rust-resistant) than it would be if left alone. 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. Talk To Us About the Alloys You Need Most. 25, 1. BMS-7-26 Boeing Spec Alloy Steel. 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. Status. Status. 2), deletes noise note in Table 6, and adds notes of explanation for Figure 12. 316L Condition A Sheet, Strip, Plate QQ-S-766 AMS 5507 Not in MMPDS. MIL-S-5000 | Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock (Superseded by SAE AMS-S-5000) | Document Center, Inc. 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. The hardenability and weldability of Alloy 4130 are considered equivalent to 8630 (MIL-S-6250) . 1 MIL-H-81200 replaced by AMS-H-81200. Alloy E 4340 is a widely used deep-hardening constructional steel. mil-a-13881 mil-a-13883 mil-a-21366 mil-a-22010-s/s by astm-d2564 mil-a-22895 mil-a-23941. 00, 1. forging: ams 6382 astm a 646. 70 0. K, France, Singapore, and Shanghai. 0. 1. Steel Bars. ”. Status. 60 . E Notice 1 - Notice of cancellation/superseded by SAE AMS 6415. REV E CANCELLATION 2. 40TI (SAE 30321), SOLUTION. Historical. We now reference and conform to AMS 2430 and AMS 2432. The heat treatment of parts fabricated from the steels. Alternate References are: 005057354,9510005057354,00-505-7354,AMS-S-5000,MIL-S-5000,AMS-S-5000,MIL-S-5000Buy SAE AMS S 5000 : 2007 STEEL, CHROME-NICKEL-MOLYBDENUM (E4340) BARS AND REFORGING STOCK from NSAIproduct forms rod & bar plate sheet coil strip tube ingot billet Los Angeles, California 1-877-727-6073 E-MAIL [email protected] psd: 1-1, 9-3 d6-5000 bv d8-5000 p d8-5000 psd: 8-57 dms1786 p dms1786 030-mc dms2433 b. astm-d5363 mil-a-101-s/s by mmm-a-250. How to Order; Standards We Provide; Updating, Reporting, Audits. Passivate Clear Passivate MIL-S-5002 QQ-P-35 AMS-QQ-P-35 AMS-2700 Types: II;VI;VII;VIII ASTM A380 Codes F thru M And ASTM A967 5. The heat treatment of. 60 Si, 0. It has a density of 0. SAE AMS 2243 : 2013. 4. Cancelled. Different grades of steel are achieved by adding other alloying elements, such as manganese, nickel, chromium, titanium and molybdenum to the basic mix. 7. 8 Ni, 0. 2002-11-21. 69 in addtion to MIL-C-5056: S391: PS18021: DFL:. AMSS5000A. AMS 6414 Alloy Steel. AMS-S-6758 has excellent physical properties. 750"dia: 72. BMS-7-26 Boeing Spec Alloy Steel. Alloy Steel MAT 137 . Page Count. 1. Standard Digital Reference Images for Inspection of Aluminum Castings. Find the right standards and certifications for your needs with SAE. AMS-S-5000. 455 Stainless Steel. Status. Popular Metal Specs. Enter code: Category Controls & Processes. 1 for sufficient time to produce the specified depth of case. 69 in addtion to MIL-C-5056:. Publication Date. Tensile strength. 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. EN ISO 15156-2 - PETROLEUM AND NATURAL GAS INDUSTRIES - MATERIALS FOR USE IN H [2]S CONTAINING ENVIRONMENTS IN. 92. 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. 35 5. Document Number. AMS 6265 Alloy Steel. This specification covers the requirements for heat-treatment of four classes of steel (See 1. Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock. 000 HEX - 74978. 43C) (SAE 4340); or, AMS 6484, Steel Bars, Forgings, and Tubing, 0. Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock AMSS5000. Sulfuric Acid Anodizing. Aug. Page Count. 2 Timothy 1:7 . mil-a-907. Find Standards By. mil-s-6090a (amendment-1), military specification: steels used in aircraft carburizing and nitriding, process for (20 jul 1972) [s/s by sae-ams-s-6090]SAE AMS2430, "Shot Peening, Automatic", supersedes SAE-AMS-S-13165. HP9-4-20 High Strength Alloy Steel. Aeronautical Design Standard (ADS) Documents. Steel Reforging Stock. Materials are available in sheets, plates and hex, square, flat and round bars. Previous Next GRADES COVERED BY MIL-S-7720 302. Withdrawn. 1) by users or their vendors or subcontractors. Superseded. SAE AMS-S-8802. 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 . , 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. 1) exceptions to the transfer technique, allows a type 1 option (5. 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. Document Number. Cancelled. BRS-110103. Qualified to SAE-AS81820 BODY BALL RACEDocument Number. Revision A, March 2007. Users may refer to SAE-AMS-S-6090, "Steel Carburizing and Nitriding,. 4441 ws 1. 1. STEEL SHEET AND STRIP 0. DISCLAIMER: The use of this information should be considered strictly voluntary. AMS 6415 - AISI 4340 (E4340) Round Bar Hot Rolled Size Table. mil-a-5540. 1998-04-01. Compression Molding of Reinforced Thermoplastic Materials (QPL) No Nadcap Commodity Code. DMS 2284. Steel covered by this specification is. , 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. 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. 25 Mo, 0. We carry, process and forge MISC United States Federal GSA Specification QQ-S-764 Grade 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. 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. E Notice 2 - Notice of cancellation/superseded by. 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 . 23Cr (7075-T6) (7075-T651)Solution and Precipitation Heat Treated ASTM B209. Metallurgy. 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. ; For our AISI 4130 (E4130) aircraft quality steel products please visit the 4130 (E4130) steel section. Titanium Industries Inc. 5Mg 0. The balance of these elements makes AMS 6414 a high. Customers calling us for 4340 plate a lot of times are. 347 / 347H. , This. tube/pipe: ams 6361 ams 6362 ams 63711. AMS-S-5000A was issued to cancel and supersede AMS-S-5000 with current, technically equivalent specifications. 38-0. This specification is applicable only to the heat treatment of raw material. , 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. REVISION C. HP9-4-30 High Strength Alloy Steel. 749mm) to 7. 0CR - 1. Please enable JavaScript to view the page content. ¼ Hard MIL-S-5059 AMS 5907 MMPDS Section 2. QQ-P-35C/AMS-QQ-P-35A SPECIFICATIONS Passivation Types Type I – Withdrawn Type II – 20-25 v% Nitric, 2-2. Buy SAE AMS 5557 : 2012 STEEL, CORROSION AND HEAT RESISTANT, SEAMLESS OR WELDED HYDRAULIC TUBING, 18. 6al/4v Alpha/Beta Titanium Alloy. sae ams s 6090 : 2006 : steel carburizing and nitriding, processes for: sae as 5944 : 1999 :. Our extensive product offerings include alloy, stainless, nickel, aluminum, titanium, carbon and cast iron. 60MN (CLAD ONE SIDE 2024-O), ANNEALED from SAI Global. MIL-T-9047 Military (Department of Defense) Specification MilSpec 6al/4v Alpha/Beta Titanium Alloy. 43C) Buy SAE AMS S 6090 : 2006 STEEL CARBURIZING AND NITRIDING, PROCESSES FOR from SAI Global. tw; Taipei Branch Office. Although I don't know for certain, it's very likely that the AMS has diverged from the MIL. 284 lb/in³, a thermal conductivity of 24 Btu/ (hr/ft²/°F), and a specific heat of 0. 38 - 0. 56C (SAE 1050) AMS5085 – available for purchase at $40. In the evening of. 4130 bars generally meet several AMS specifications, but the most common are AMS-S-6758 and AMS- 6348, but several others may also apply. AMS5085. 5Ni) AMS 5556 Seamless/ welded tube. AMS 6414 Alloy Steel. AMS2750F is typically communicated via industry standards such as SAE/AMS specifications as well as customer purchase orders and part prints. 4340 Alloy Steel (AMS-S-5000) Heat Treated Cadmium Plated 440C Stainless Steel (AMS 5630) Heat Treated Hard Chrome Plated (AMS-QQ-C-320, Class 2) 17-4 PH Stainless Steel (AMS 5643) Heat Treated AT 3200 Bearing Liner, Permanently Bonded to Race I. 2μm/m °C and a thermal conductivity of 14W/m°C. Steel Forgings. Steel covered by this specification is intended for use in the manufacture of highly stressed aircraft parts requiring high hardenability. MIL-S-7420, AMS-6440, AMS-2301, AMS-6440, AMS-6444. 2) and the requirements for furnace equipment, test procedures and information for heat-treating. 📝 Amendments Available. Claudia's Notes: Originally, the AMS-QQ-P-35 was just a reprint of the QQ-P-35C. Corrosion. Metal finishing. Superseded date: 04-11-2012. 625, . Corrosion. 20 1. BC Ferry: Washington - Bellingham - Victoria - British Columbia Travel and Adventure Vacations. We carry, process and forge MIL-S-5626 Military Specification MilSpec 4140 Alloy Steel. Revised. Chromic Acid Anodizing - Class 5. AMS 4109 7175-T736 Superseded by AMS 4149: WS 3. Test procedures. mil-a-5090-s/s by mmm-a-132 mil-a-5092-s/s by mmm-a-1617. 38-0. March 3, 2010. 00. Document Number. The alloy’s melting point stands at approximately 2,800°F, and its coefficient of thermal expansion is 6. Status. 2002-11-21. All Grades. A-286 Stainless Steel. 36% to 0. AMS-C-27725 Grove, OK Boeing: Etch - Cres AMS-C-81769 Grove, OK: Boeing Passivation: AMS-QQ-P-35 Grove, OK Boeing: Shot Peen AMS-S-13165 Grove, OK: Boeing Passivation: ASTM A380/A380M / AMS QQ-P-35 A Grove, OK Boeing: Salt Spray Testing ASTM B117 Grove, OK: Boeing Penetrant Inspection: ASTM-E-1417 Grove, OK. The furnace or retort should be purged with inert gas before opening. MIL-S-5000E, MILITARY SPECIFICATION: STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS, AND FORGING STOCK (12-NOV-1982) [S/S BY SAE-AMS-S-5000]. 0 Ni, 2. AMS 6414 Alloy Steel. AMS-S-5000. Find the right standards and certifications for your needs with SAE. 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. 90 0. 5. The requirements of the individual specification applicable to the form required shall be fulfilled whenever reference is made to this specification. “This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. 375, . Rationale: AMS-S-7720B stabilizes this document because equivalent technical requirements are contained in other specifications. SAE AMS-S-5000. Multi - user online standards collection: secure, flexibile and cost effective. Alloy Steel MIL-S-83030 . Buy SAE AMS 2251 : 2013 TOLERANCES, LOW-ALLOY STEEL BARS from SAI Global. 1. This product is not available online at this time. 9 KHB 1700. March 1, 2007. AMS 2700 Method 1 is the nitric baths, essentially unchanged from QQ-P-35. A-286 Stainless Steel. March 1, 1999. Alloy Steel AMS 6359 . Superseded. AMS 6931 6al/4v Titanium Alloy. 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). Talk To Us About the Alloys You Need Most. 47-0. E. This combination of alloy and heat treat level. AMS-S-5000. Max Tens MIL-N-14411 Comp 3 (4750) Cap. mil-a-5090-s/s by mmm-a-132 mil-a-5092-s/s by mmm-a-1617. 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. Revision Level. 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. Product Forms: Steel, Chrome-Molybdenum Bars and Re-Forging Stock (Aircraft Quality) Scope: This specification covers chrome-molybdenum (4130) steel bars and forging stock of aircraft quality. MIL-S-13165. 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. 2 Classification: Material shall be. Many contracts still call out MIL-T-9047 and AMS. 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. Issuing Committee: AMS E Carbon and Low Alloy Steels Committee Publisher: SAE International. Superseded. REPLACED BY AMS-S-6758. mil-a-907. MIL-S-6758. AMS-7727 : Kovar® Rod : For God gave us a spirit not of fear but of power and love and self-control. Description / Abstract: SAE AMS-S-6090, Revision B, May 2006 - Steel Carburizing and Nitriding, Processes for. 5Mg 0. Revision Level. 1. 661. Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock. AMS 6414 sheet is an alloy steel that consists of carbon, manganese, chromium, molybdenum, vanadium, and nickel. Alloy 302. 85g/cm³ and a melting point of 1450°C. Grinding of Chromium Plate - Landing gear parts 275 KSI or above. 8. Durability. Use our Rapid Response RFQ to request a quote. The specifications for this alloy include AMS 6414, AMS 6409, AMS 6415, AMS 6484, AMS-S-5000, DMS 1555 Gr A, BMS 7-28, BPS 299-947-055, SS 9702, PWA LCS F-17, MIL-S-8844 CL1, and MIL-S-5000. AMS 5571 Seamless tube. MIL MIL-S-5000E STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS, AND FORGING STOCK (S/S BY SAE-AMS6415P AND SAE-AMS-S-5000) (SUPERSEDING. Country: USA: Britain: Britain: Japan: Standard: ASTM A29: EN 10250: BS 970: JIS G4103: Grades: 4340:. AMSS5000. Buy SAE AS 6279B : 2019, the superseded version of standard practice for production, distribution & procurement of metal stock for AMS, from SAE International. Alloy 4130 is also vacuum degassed to meet the magnetic particle. 3 This test method specifies the use of air melted SAE 4340 steel (Grade A, see 7. Condition: Special Aircraft Quality Cleanliness Normalized and Tempered. 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]. SAE AMS-S-6758. T. Related Topics: Test procedures. l), ASTM-A295 AMS 6304 ASTM F1537 titanium. 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. 6511: EN24/817M40: SNCM 439/SNCM8: AMS 6415 Uses. 12, 1967. 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. September 1, 1997 Steel, Corrosion-Resistant (18-8) Bars, Wire and Forging Stock (Aircraft Quality) 1. redstone. HP9-4-30 High Strength Alloy Steel. This product is not available online at this time. MIL-S-5000 Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock. 60Mn (2024-T3) (2024-T351) Solution Heat Treated QQ-A-250/4. AMS-S-13165 was made redundant by AMS 2430 and AMS 2432. 2 Classification: The steel bars and reforging stock shall be as follows:. View DetailsCalifornia Metal & Supply, Inc. Classes 202 and 302: Class 302 is intended for use where severe corrosion is. 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). No. I. George VI had undergone a lung operation in September 1951 from which he never fully recovered. Document History. Document History. Alloy Steel AMS 6304 (17-22A) Alloy Steel MIL-S-5000 . 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. July 1,. Tensile strength. 6Cu 0. ADOPT WITHDRAWN. All Grades. , Canada, Mexico, U. SAE AMS-QQ-A-225/8 : Aluminum Alloy 6061, Bar, Rod, Wire, and Special Shapes; Rolled, Drawn, or Cold Finished. com . 6000 - Magnesium / Silicon - good machinability, corrosion resistance, moderate strength. 4130 Alloy Steel in AMS-S-6758 per SAE International: “This specification covers chrome-molybdenum (4130) steel bars and forging stock of. As aviation enthusiasts we are pleased to serve all of your aircraft alloy needs. Use our Rapid Response RFQ to request a quote. 080 x 60. Steel Tubing. 23Cr (7075-T6) (7075-T651)Solution and Precipitation Heat Treated ASTM B209. Mo. The plate and sheet covered by this specification shall be an integral composite product consisting of a heat-treatable aluminum alloy 2024 core with thin layers of an aluminum alloy 1230 (99. Alloy 4340 is known for its toughness and capability of. SAE AMS-S-5000. 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. 00: in: stk: 302/304 wire . 4340 Alloy Steel. Pages: 7. Buy SAE AMS 5853 : 2012 STEEL, CORROSION AND HEAT-RESISTANT, BARS AND WIRE, 15CR - 25. 2MO - 2. We carry, process and forge MISC Lockheed Martin Corporation Spec STM05-602 Grade 13-8Mo Stainless Steel. Document History. HP9-4-20 High Strength Alloy Steel. Steel Sheets. Publication Date. BMS-7-26 Boeing Spec Alloy Steel. AMS-S-5000 - ADOPT WITHDRAWN - SUPERSEDED -- See the following: AMS-6415 AMS-6484 Show Complete 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. AMS 6414 Alloy Steel. 00: in: stk: 4130 rnd 1. Aircraft Alloys. 00%, and the remaining elements comprise the rest of AMS 6414’s composition. 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. ams 6351 astm a505 mil-s-18729. This mil-spec covers the requirements for electrochemically-formed anodic coatings on aluminum and aluminum alloys for non-architectural applications. All Grades. Enter code: Categories 300M & 4340M Alloy Steel, Alloy Steel, DMS, Grades, McDonnell Douglas Specifications, Specifications. 2) and the requirements for furnace equipment, test procedures and information for heat-treating procedures, heat-treating temperatures and material (See. 6al/4v Alpha/Beta Titanium Alloy. One of the most versatile stainless steel alloys is AMS-S-5000. Heat Treatment of Steel Raw Materials. com PRINT FORM Equivalent Standard(s) Relationship: SAE AMS 6484 : 2016 : Similar to: SAE AMS S 5000 : 1999 : Similar to: SAE AMS 6415 : 2016 : Similar to: SAE AMS 6409E : 2016 : Similar to: SAE MAM 6415 : 1998 : Similar to Document Number. (s/s by sae ams-h-6875) h amm2 mil-p-23377 (superseded by mil-prf-23377) f mil-p-85582 (superseded byBuy MIL-S-5000 Revision E:1982 STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS AND REFORGING STOCK from SAI GlobalAMSS6090A. Buy SAE AMS 2175 : 2010 - non-destructive testing methods, sampling frequency, & acceptance criteria for the inspection of metal castings from SAE International. 2) and the requirements for furnace equipment, test procedures and information for heat-treating procedures, heat-treating temperatures and material (See 6. 4571 afnor z6cnd17-11 afnor. 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,. 3, 3. 3) test procedures. 5MG - 0. This combination of alloy and heat treat level. Use our Rapid Response RFQ. 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. Materials properties. 1954-05-01. MIL-S-5000E (NOTICE 1), MILITARY SPECIFICATION: STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS, AND FORGING STOCK (27 SEP 1995) [S/S BY SAE. Aluminum alloys.