2 Mo, 1. AMS 5735 is a sub-type specification of Stainless Steel A286, a precipitation-hardenable super-alloy that possesses many favorable properties. Grade Description Specification; 1010: ROD AND BAR: AMS 5062: SHEET: AMS 5040: 1018: ROD AND BAR: ASTM-A-108: 135 MOD: ROD, BAR & FORGINGS: AMS 6470, AMS 6471, MIL-S. The high fatigue strength makes E4340 ideal for highly stress parts as it maintains it's strength and hardness at elevated temperatures. MIL-S-5000. MIL-S-5000 Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock. Click here to view the AMS Std. Buy MIL S 5000 : E STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS AND REFORGING STOCK from NSAIStandard Reference Radiographs for Tin Bronze Castings. Chemicals. 4Cu 1. 1. Bars, and Forging Stock (Superseded by SAE AMS-S-5000) To find similar documents by Federal Supply Class Code: FSC 9510 (Bars and Rods) ORDER.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 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. Product Forms: Steel Bars, Forgings, and Tubing. Document Number. Buy SAE AMS 2251 : 2013 TOLERANCES, LOW-ALLOY STEEL BARS from SAI Global. 8 Ni, 0. 3. Talk To Us About the Alloys You Need Most. Grinding of Chromium Plate - Landing gear parts 275 KSI or above. AMS 6414 Alloy Steel. mil-a-5540. Various Bar / Wire/ Forgings QQ-S-763 AMS-QQ-S-763 Should not be specified for AMS S 8802 standardizes the specifications for temperature-resistant, two-component synthetic rubber compounds of the polysulfide type. 347 / 347H. Rationale: AMS5517M revises Composition analysis standards (3. link] was cancelled and superseded by AMS2700 [affil link], which has a class 4 which is. This specification. 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. Document Number. Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock AMSS5000. S. Steel, Chrome-Nickel-Molybdenum (E4340) Bars & Reforging Stock. 9510-00-228-9735, BAR,METAL. Aircraft Alloys. A-286; 13-8MO; 15-5PH; 17-4PH; 316; 321; 400; 455; 300M/4340M;. Material may also meet specs ASTM-A331, ASTM-A304, ASTM-A108, AMS-2301, AMS-S-5000 (replaced MIL-S-5000), EN10204. 595A colour chart. Identification numbers. MIL-H-5606 petroleum base hydraulic fluid for military aircraft (inactive for new designs. No. Inconel 625 ™ Super Alloy in Sheet, Strip and Plate. Heat treatment. 3. March 1, 2007. Revision A, March 2007. Multi - user online standards collection: secure, flexibile and cost effective. 43%, manganese ranges from 0. What is alloy 4140 steel? Alloy 4140 is an oil-hardening steel of relatively high hardenability. This specification is superseded by a series of individual specifications covering specific forms of this material. , constitutes a requirement to conform to the applicable provisions of the documents. Aluminum. AMS 6414 Alloy Steel. STEEL BARS, FORGINGS, AND TUBING 0. Popular Metal Grades. Titanium alloys. , This specification covers the requirements for heat-treatment of four classes of steel (see 1. This combination of alloy and heat treat level. Subscribers can view annotate, and download all of SAE's content. Heat treatment. 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. SCOPE: 1. Steel. Coatings, colorants, and finishes. Withdrawal Date:MIL-H-6875H HEAT TREATMENT OF STEEL was superseded 2 Feb 1999 by AMS-H-6875 Heat Treatment of Steel Raw Materials ($59 from SAE). 3MO - 0. 40TI (SAE 30321), SOLUTION. AMS-STD-2154E includes revision to transducer size (5. We carry, process and forge ASTM A575 Specification Steel. 40-0. Metallurgy and specifications. Hardness)AMS-77273 KovarMILITARY SPECS(Commonly Requested for Military Hardware)MIL-I-23011 CL 1 3(Kovar)MIL-N (Nickel)MIL-N-6710 600 Nickel Alloy Exc. of MIL-S ( steel)MIL-S-5000E-4340 AEROSPACE. AMS 6414 Alloy Steel. 4435 ws 1. 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. This change spawned a great deal of controversy in the heat treating industry which continues to this day. 4340 E4 MILS-5000 1. 4340 Alloy Steel. , AMS 2759/3 Heat Treatment Precipitation-Hardening Corrosion. 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. Feb. Manufacturing processes. Heat treatment. AMS-S-5000. 4130 Alloy Steel. 749mm) to 7. Steel, Corrosion Resistant, Bars, Wire, Shapes, and Forgings. AMS-S-13165. Classes 202 and 302: Class 302 is intended for use where severe corrosion is. The military paid to have its old specs hosted by commercial standard companies so we can claim we use commercial standards. Related Topics: Heat resistant materials. american aircraft quality alloy steel bar-analysis cmnpmax. 4340 air melt bms 7˜28, mil˜s˜5000, dms 1555 gr. Hendrickson Dr. MIL-S-6758 MilSpec Military Grade Alloy Steel. Qualified to SAE-AS81820 BODY BALL RACEDocument Number. The alloy has a significant amount of nickel and molybdenum, making. A. 1950. We carry, process and forge AMS 4078 Specification 7075 Aluminum Alloy. 250 DIA. 9510-00-505-7354, BAR,METAL. 6al/4v Alpha/Beta Titanium Alloy. SAE AS 9120 : 2016. 3. 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). For detailed information and chemical analysis please visit the 4340 (E4340) steel page. AMS-S-13165 was made redundant by AMS 2430 and AMS 2432. AMS5085. Distributor of alloy steel AMS-S-5000 for aerospace, food service, metalworking, industrial, chemical and petrochemical applications. REV E CANCELLATION 2. 20 1. . Page. 1. Critical updates of standards and customisable alerts and notifications. Buy SAE AMS S 5000 : 2007 STEEL, CHROME-NICKEL-MOLYBDENUM (E4340) BARS AND REFORGING STOCK from SAI Global. Buy SAE AMS 5085 : 2017 STEEL SHEET, STRIP, AND PLATE, 0. Chromic Acid Anodizing - Class 5. SAE AMS-S-5000. SAE AMS-S-6090. HP9-4-30 High Strength Alloy Steel. SAE AMS 6484 : 2016. Titanium Industries Inc. SPECIFICATIONS: Avion Alloys services Blue Chip customers worldwide with prime top-quality metals like AH 36 bars procured exclusively from United States Mills. 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. This specification applies to manufacturers and suppliers who heat treat aerospace material. MIL-S-13165. SCOPE: 1. The carbon content ranges from 0. 455 Stainless Steel. AMS-7727 : Kovar® Rod : For God gave us a spirit not of fear but of power and love and self-control. 0. 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. astm-d5363 mil-a-101-s/s by mmm-a-250. Infostore. The insurance estimator will help personal customers understand what the upcoming premium savings will mean to them. If you require technical assistance or would like to receive a quote, please call our Customer Service team TOLL FREE at (866) 610-1660. December, 2007, and has been superseded by AMS 2430, Shot Peening. March 3, 2010. Buy SAE AMS S 5000 : 1999 STEEL, CHROME-NICKEL-MOLYBDENUM (E4340) BARS AND REFORGING STOCK from SAI Global. AMS-S-5000 has a density of 7. 8. 4340 Alloy Steel. Showing 1 to 25 of 88 entries. 43C) Buy SAE AMS S 6090 : 2006 STEEL CARBURIZING AND NITRIDING, PROCESSES FOR from SAI Global. As part of the hosting, they converted the old MS designated part numbers to AMS, NAS, SAE, etc. This specification covers electric furnace steel bars and reforging stock of aircraft quality. Steel. 40 Mo, 0. Canceled and inac ve MIL-T and AMS specifica ons are referenced for replacement purposes and should not be specified for new designs. Materials properties. MIL-S-5000E (NOTICE 2), MILITARY SPECIFICATION: STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS, AND FORGING STOCK (11 AUG 2000) [S/S BY SAE. Tensile strength. 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. 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. 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. The heat treatment of parts fabricated from the steels. 5Ni) AMS 5556 Seamless/ welded tube. Proposed changes to the standard by DoD activities must be submitted to the DoD Adopting Activity at Defense Standardization Program Office, 8725 John J. MIL-T-9047 Military (Department of Defense) Specification MilSpec 6al/4v Alpha/Beta Titanium Alloy. 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. 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. 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. Different grades of steel are achieved by adding other alloying elements, such as manganese, nickel, chromium, titanium and molybdenum to the basic mix. F18;CTG;CHEM FILM (SUPERSEDED BY MIL-C-5541) Buy SAE AMS S 5000 : 2007 STEEL, CHROME-NICKEL-MOLYBDENUM (E4340) BARS AND REFORGING STOCK from SAI Global 4340 Alloy Steel. 4×10⁷ Ωm, making it a great electrical conductor. Revision Level ADOPT WITHDRAWN Status Superseded Publication Date March 3, 2010 Page Count 1 page AMS-S-5000 Steel, Chrome-Nickel-Molybdenum (E4340) Bars &. 12, 1967. 4330M Alloy Steel. Email：hanjustdoit@gmtc. Superseded. AMS 5575 Welded tube. 0000. Perry, was at the forefront of military specification reform. 33C) (SAE 4130) 125 ksi (862 MPa) Tensile Strength. Effective January 1, 2009, the requirements of the latest issue of AMS 2430 shall be fulfilled whenever reference is made to the cancelled. 05C) (SAE 52100), PREMIUM AIRCRAFT-QUALITY, CONSUMABLE ELECTRODE VACUUM REMELTED. MIL-S-5000 - Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock (Superseded by SAE AMS-S-5000) MIL-S-5626 - Steel, Chrome-Molybdenum (4140). MIL-S-7420, AMS-6440, AMS-2301, AMS-6440, AMS-6444. AMS 6409/14/15/84, SAE 4340, AMS-S-5000, BMS 7-28, NCT 10-123-21/2MD, MTL 1101 0. 250, . SAE AMS-QQ-S-763. Its chromium content provides good hardness penetration, and the molybdenum imparts uniformity of hardness and high. 1998-04-01. superseded a superseded standard is one,. SPECIFICATIONS: AISI4340, ASTM A 829 / A6 SAE J404, AMS 2252/ 2301/6359 SAE J404. Description / Abstract: SAE AMS-QQ-P-35, Revision A, February 2005 - Passivation Treatments for Corrosion-Resistant Steel. We carry, process and forge MISC Specification MTL-1201 Grade 300M / 4340M Alloy Steel. mil-a-1058 . Corrosion. A-286 Stainless Steel. AMS 4109 7175-T736 Superseded by AMS 4149: WS 3. Status. No. 00, 1. 43 C. AMS 6931 6al/4v Titanium Alloy. Type 321 is used where resistance to intergranular corrosion is required and where the parts are subjected to sustained heating or cooling. , This specification presents requirements for thin-walled (inside diameter greater than four times the wall thickness and outside diameter 1/4 inch. “This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. 85g/cm³ and a melting point of 1450°C. AMS Specifications; SPEC Description UNS Number Alloy Quote Request; AMS 2241: Tolerances Heat Resistant Bars: RFQ:. 1. Your Message. All Grades. ¼ Hard MIL-S-5059 AMS 5907 MMPDS Section 2. 80 Cr, 1. Talk To Us About the Alloys You Need Most. 6. Subscribers can view annotate, and download all of SAE's content. Related Topics: Manufacturing processes. Although I don't know for certain, it's very likely that the AMS has diverged from the MIL. 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. 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. Use our Rapid Response RFQ to request a quote. Version: F. , This specification covers chrome-molybdenum (4140) steel bars, rods, and forging stock of aircraft quality. Chromium. 80Cr. SAE MOBILUS. 000 HEX. 40 0. BMS-7-26 Boeing Spec Alloy Steel. 5Mg 0. Rockwell Collins is offering a dual AMS-5000 system a two-year warranty and will replace or update required line replaceable units (LRUs). This combination of alloy and heat treat level has been used for many years and a large database has been accumulated in the aerospace industry on its. Vacuum induction and consumable. Metals. 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 e4340 E4 MILS-5000 1. 38 - 0. SAE AMS-S-7720. 1 Al. TITANIUM AND TITANIUM ALLOY BARS (ROLLED OR FORGED) AND REFORGING STOCK, AIRCRAFT QUALITY (S/S BY SAE-AMS-T-9047) SAE AMS-S-8802. , This specification covers chrome-molybdenum (4130) steel bars and forging stock of aircraft quality. AMS 6265 Alloy Steel. 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. This is a standard used by the aerospace industry to describe and control the passivation of stainless steel. Country: USA: Britain: Britain: Japan: Standard: ASTM A29: EN 10250: BS 970: JIS G4103: Grades: 4340: 36CrNiMo4/ 1. Steel. 4), adds (5. 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. 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. In many cases, nothing has. 36% to 0. Claudia's Notes: Originally, the AMS-QQ-P-35 was just a reprint of the QQ-P-35C. ”. Page Count. EN ISO 13533:2002. MIL S-5000: AMS 6415 Specifications. titanium. Aero-Vac Alloys & Forge is the metal buyer's trusted resource - we speak metal! Skip to navigation Skip to content. 750"dia: 72. AnAlySiS P S ni c Mn Max. AMS2750F is typically communicated via industry standards such as SAE/AMS specifications as well as customer purchase orders and part prints. 4441 ws 1. Talk To Us About the Alloys You Need Most. ; For our AISI 4130 (E4130) aircraft quality steel products please visit the 4130 (E4130) steel section. Publication Date. CAUTION: The supersession information is valid as of the date of this notice and may be superseded by subsequent revisions of the superseding document. HP9-4-20 High Strength Alloy Steel. Talk To Us About the Alloys You Need Most. 38 - 0. AMS 6415 material’s unique combination of properties makes it ideal for various high-stress engineering applications. 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. Related Topics: Heat resistant materials. Buy SAE AMS 6415 : 2016, the current standard for premium aircraft-quality, low-alloy steel bars, forgings & tubing. 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. 50: si: stk:. 420 qqs-763, ams-5621, astm-a-276. This product is not available online at this time. 20 Mo. Page Count. Mo. Sept. Available Forms: Popular Industry Specifications. Historical. Due to E-4340's high alloy content it obtains a uniformed hardness by heat treatment. 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. Steel Forgings. 15. Classes 202, 302, and 305: When sensitization cannot be tolerated classes 202, 302 and 305 are not recommended for use. F18;CTG;CHEM FILM (SUPERSEDED BY MIL-C-5541). 4340 air melt bms 7˜28, mil˜s˜5000, dms 1555 gr. 5000: 15-5ph ams5862 . 6415, AMS. G43406. Status. 2μm/m °C and a thermal conductivity of 14W/m°C. Condition: Special Aircraft Quality Cleanliness Normalized and Tempered. 80/1. Heat treatment. Specifications. The heat treatment of parts fabricated. MIL-STD-2154 Military (Department of Defense) Specification MilSpec Alloy Inspection MilSpec Ultrasonic Inspection. Nickel INVAR 36 . Publication Date. Heat Treatment of Steel Raw Materials. AMS 6278: Steel, Bars, Forgings and Tubing: K91231: CBS-50NIL: RFQ: AMS-DTL-22499: Shim Stock Laminated: RFQ: ASK US A. BMS-7-26 Boeing Spec Alloy Steel. March 3, 2010. Quality assurance. Use our Rapid Response RFQ to request a quote. 60 Si, 0. FSC Code: 9510 - Bars and Rods, Iron and Steel. QQ-P-35, Type VI: AMS 2700, Method 1, Type 6. 10 pages SAE AMS 6485 : 1989. DMS 2284. Superseded. AMS 6414 Alloy Steel. Country: USA: Britain: Britain: Japan: Standard: ASTM A29: EN 10250: BS 970: JIS G4103: Grades: 4340:. AMS 6414 Alloy Steel. Steel Forgings. 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. AMS 5598. , Canada, Mexico, U. 1), ASTM-A295 17-22 AMS 6304 COBALT ALLOYS 28CR-6Mo ASTM F1537. 4427 ws 1. Pages: 7. Document Number. Our discussion here is driven by the fact that several end-users continue to use the original MIL specification for their peening operations. 11 Btu/ (lb/°F). 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. SAE AMS-S-5000. Rationale: AMS-S-6758B has been declared Stabilized as it has been replaced by technically equivalent specifications. Nickel Kovar . 1 for sufficient time to produce the specified depth of case. 20 Mo. A108, UNS. ROD AND BAR. AMS-S-5000A was issued to cancel and supersede AMS-S-5000 with current, technically equivalent specifications. Dec. 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]. AMS-S-5000. com . Corrosion. 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. 85 0. 19, 1998. Revision Level. Use our Rapid Response RFQ to request a quote. 0000 x 144. Rationale: AMS-S-7720B stabilizes this document because equivalent technical requirements are contained in other specifications. We carry, process and forge MISC Lockheed Martin Corporation Spec STM05-602 Grade 13-8Mo Stainless Steel. This grade of the alloy should be forged between 1950 and 2250 degrees F (or about 1066 to 1232 degrees C). All Grades. EN ISO 15156-2 - PETROLEUM AND NATURAL GAS INDUSTRIES - MATERIALS FOR USE IN H [2]S CONTAINING ENVIRONMENTS IN. Steel Carburizing and Nitriding, Processes for. Issuing Committee: AMS E Carbon and Low Alloy Steels Committee Publisher: SAE International. 38 - 0. 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. As aviation enthusiasts we are pleased to serve all of your aircraft alloy needs. 4. 4130 Alloy Steel, Alloy Steel, DMS, Grades, McDonnell Douglas Specifications, Specifications. is a world wide supplier of quality alloy steel metals. 00, 2. Electroless nickel plating is an process that codeposits a nickel-phosphorous alloy without need for an externally applied electrical current. S. Tensile strength. mil-a-8576-s/s by sae-ams-a-8576 mil-a-8623-s/s by mmm-a-134 mil-a-9117. , Da-Kang Village, Kuei-Sun, Taoyuan County. Material may also meet specs ASTM-A322, ASTM-A304, ASTM-A108, AMS-2301, AMS-S-5000 (replaced MIL-S-5000), EN10204. Dec. 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. Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard. Users may refer to SAE-AMS-S-6090, "Steel Carburizing and Nitriding,. MIL-S-5000. MIL-S-6758. AMS-S-6758. 12, 1967. This Standard has been added successfully to your. Here's a link to the history of the MIL, and here's a link to the history of the AMS. 0 Ni, 2. 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). Steel covered by this specification is intended for use in the manufacture of highly stressed aircraft parts requiring high hardenability. 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. This document is available in either Paper or PDF format. si ni cr mo cu max. 1) per SAE AMS 6414, and both are heat treated to 260 to 280 ksi (pounds per square inch ×1000). REV E CANCELLATION 1. Status. Talk To Us About the Alloys You Need Most. 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. This specification covers a carbon steel in the form of sheet, strip, and plate. AMSS5000A. 2738 FAX: 210. ADOPT WITHDRAWN.