Ams-s-5000 superseded by. Revision A, March 2007. Ams-s-5000 superseded by

 
 Revision A, March 2007Ams-s-5000 superseded by Document Number

000" (177. AMS 6414 Alloy Steel. We carry, process and forge MISC United States Federal GSA Specification QQ-S-764 Grade Stainless Steel. plate/sheet/strip: ams 6350. 8Ni - 0. 85g/cm³ and a melting point of 1450°C. Superseded. 33C) (SAE 4130) 125 ksi (862 MPa) Tensile Strength. MIL-S-5000, AMS-S-5000 (Both are canceled and superseded by AMS 6415) MIL-S-8844 299-947-055 Bell Helicopter SS 9702 Sikorsky . Aero-Vac Alloys & Forge is the metal buyer's trusted resource - we speak metal! Skip to navigation Skip to content. MIL-S-5000. Revision Level. 43C) (SAE 4340); or, AMS 6484, Steel Bars, Forgings, and Tubing, 0. AMS 5637, QQS-763, MIL-S-7720. 25 Mo, 0. 010 0. Si cr Max. Available Forms: Popular Industry Specifications. AMS5085. K, France, Singapore, and Shanghai. Status. 40/. Technical Data Sheet. Reference to AMS2759 on a drawing, fabrication order, purchase order, etc. 27, 1995. AMS 5500. Please request a quote below or head over to the general catalog by clicking the "Products" link in the side bar. BMS-7-26 Boeing Spec Alloy Steel. 4340 Alloy Steel. AMS 4091 Superseded by AMS 4081 AMS 4092 Superseded by AMS 4082 AMS 4093 Superseded by AMS 4083 AMS 4113 6061-T6 Extruded shapes AMS 4115 6061-0 Cold finished bars, rod, wireBuy SAE AMS 5620 : 2012, a superseded standard which covers two types of corrosion and heat-resistant steel, from SAE International. 2. This list provides current process documents, and is the. Description / Abstract: SAE AMS-S-6090, Revision B, May 2006 - Steel Carburizing and Nitriding, Processes for. Buy SAE AMS H 6875 : 2010, the susperseded specifications for heat-treatment of four classes of steel, from SAE International. Steel covered by this specification is intended for use in the manufacture of highly stressed aircraft parts requiring high hardenability. 3) in accordance with this standard. Perry, was at the forefront of military specification reform. AMS 6931 6al/4v Titanium Alloy. astm-d5363 mil-a-101-s/s by mmm-a-250. Page Count. 4340 Alloy Steel. 80Cr. Page Count. 4130 Alloy Steel, Alloy Steel, DMS, Grades, McDonnell Douglas Specifications, Specifications. Enter code: Categories 300M & 4340M Alloy Steel, Alloy Steel, DMS, Grades, McDonnell Douglas Specifications, Specifications. Condition A AMS 5648 Not in MMPDS. AMS 6257 Specification 300M/4340M Low Alloy Steel. Noncurrent. Document History. Our service centers are located throughout the U. How to Order; Standards We Provide; Updating, Reporting, Audits. 28 - 0. HP9-4-30 High Strength Alloy Steel. Various Bar / Wire/ Forgings QQ-S-763 AMS-QQ-S-763 Should not be. Pages: 22. Status. 0000. Inconel 706 ™ Super Alloy in Sheet, Strip and Plate. 3, 3. Effective January 1, 2009, the requirements of the latest issue of AMS 2430 shall be fulfilled whenever reference is made to the cancelled. SAE AMS-H-6875. STEEL BARS, FORGINGS, AND TUBING 0. , Canada, Mexico, U. Status. Also known as: SAE AMS 3651 SAE MOBILUS. Publication Date. Max. 6Zn 2. 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. 40-0. All Grades. MIL-S-5000 | Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock (Superseded by SAE AMS-S-5000) | Document Center, Inc. Classes 202 and 302: Class 302 is intended for use where severe corrosion is. To request the addition of new colors, please send a paint sample (on an acceptable substrate) to the SAE contact below. Buy SAE AMS 5853 : 2012 STEEL, CORROSION AND HEAT-RESISTANT, BARS AND WIRE, 15CR - 25. Multi - user online standards collection: secure, flexibile and cost effective. 6al/4v Alpha/Beta Titanium Alloy. 15 0. 25Mo (0. This specification is for a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. Publication Date. AMS 4037 2024 Aluminum Alloy, Aluminum Sheets and Aluminum Alloy Plate 4. 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. Metallurgy and specifications. K, France, Singapore, and Shanghai. 5000 Series Aluminum Sheet; 6000 Series Aluminum Sheet; 7000 Series Aluminum Sheet; Aluminum Checker / Tread / Diamond Plate; Aluminum Wire. S. AMS 6414 sheet is an alloy steel that consists of carbon, manganese, chromium, molybdenum, vanadium, and nickel. November 1, 2002. Related Topics: Coatings, colorants, and finishes. We speak metal!SAE AMS-S-7720: 1997: Steel, Corrosion-Resistant (18-8) Bars, Wire and Forging Stock (Aircraft Quality) /2/ SAE J 217: 1994: Stainless Steel 17-7 Ph Spring Wire and Springs /1/ SAE J 230: 1994: Stainless Steel, SAE 30302, Spring Wire and Springs /1/ SAE J 405: 1998: Chemical Compositions of SAE Wrought Stainless SteelsGrade Specification Temper; 4130: MIL-S-18729, AMS6350, AMS6345: Annealed, Normalised: 4340: AMS6359: Annealed, Normalised: 4140: ASTM-A829 : S514/5: BS 2S515 (BS. Superseded. Revision Level. Revised. 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. 4. Magnetic materials. Steel Bars. 23Cr (7075-T6) (7075-T651)Solution and Precipitation Heat Treated ASTM B209. March 1, 2007. 25, 2. 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 the requirements for heat-treatment of four classes of steel (See 1. mil-b-11595 e - mil-b-11595e (w/amendment 1), military specification: bar, metal and blanks, steel (under 2 inches in diameter) for barrels of small arms weapons (26 jul 2004) mil-s-5000, ams-s-5000, mil-s-8844, ams-s-8844: plate: ams 6359: 52-100: rod and bar: ams 6440, ams 6444, mil-s-7420: 6150: rod and bar: ams 6448, mil-s-8503: 8620: What are the two aircraft that replaced the AMS 6415? 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 . 2) and the requirements for furnace equipment, test procedures and information for heat-treating. Document Number. heavy duty, metallic reinforced, 400 degree f, 5000 psi hydraulic and pneumatic: sae as 5420 : 2017 : hose assembly, heated, 125 psig, lined. DOD ADOPTION. mil-a-1058 . 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. Simple online access to standards, technical information and regulations. Material may also meet specs ASTM-A331, ASTM-A304, ASTM-A108, AMS-2301, AMS-S-5000 (replaced MIL-S-5000), EN10204. E Notice 1 - Notice of cancellation/superseded by SAE AMS 6415. AMS 6265 Alloy Steel. 2) and the requirements for furnace equipment, test procedures and information for heat-treating procedures, heat-treating temperatures and material (See 6. 38 - 0. It has a density of 0. 455 Stainless Steel. STEEL BARS AND FORGINGS, 5. Noncurrent. Technical Data Sheet. 75% to 1. Find the right standards and certifications for your needs with SAE. redstone. 4340 Alloy Steel. ; For our AISI 4130 (E4130) aircraft quality steel products please visit the 4130 (E4130) steel section. All Grades. MIL-S-13165 – Shot Peening of Metal Parts AMS 2430 - Shot Peening AMS 2432 – Shot Peening, Computer Monitored None 1-13-00buy sae ams 5570 : 2013 steel, corrosion and heat-resistant, seamless tubing 18cr - 11ni - 0. 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,. Alloy 7050. SAE AMS 6444 : 2015. Mo. Talk To Us About the Alloys You Need Most. Use our Rapid Response RFQ to request a quote. Page Count. The balance of these elements makes AMS 6414 a high. SAE AMS-H-6875. It is recommended that preheating or. ams 6348 mil-s-6758 ams 2301 astm a322 astm a331 qq-s-624. 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. SAE AMS-QQ-S-763. The carbon content ranges from 0. A-286 Stainless Steel. AMS 5654 Bars (aircraft quality)MIL-H-6875H, MILITARY SPECIFICATION HEAT TREATMENT OF STEEL, PROCESS FOR (1 MAR 1989) [S/S BY SAE-AMS-H-6875]. Historical. Page. Overview. STEEL BARS AND FORGINGS, 5. 376. All Grades. HP9-4-20 High Strength Alloy Steel. As aviation enthusiasts we are pleased to serve all of your aircraft alloy needs. Metallurgy. Heat treatment. In the early 1990’s, US Secretary of Defense, William J. 35 5. MIL-S-5626C, MILITARY SPECIFICATION: STEEL, CHROME-MOLYBDENUM (4140) BARS, RODS, AND FORGING STOCK (FOR AIRCRAFT APPLICATION) (17 JUL 1968) [S/S BY SAE-AMS6382, AND SAE-AMS6349]. REV C CANCELLATION 1. 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]. VIEW CART · CONTACT · HOME. 1 316 Various Bar, Wire, Forgings QQ-S-763 AMS-QQ-S-763 Should not be specified for new design. MIL-H-5606 petroleum base hydraulic fluid for military aircraft (inactive for new designs. Processes: This specification presents requirements for the carburizing and nitriding of carbon and alloy steels to produce the mechanical properties specified by drawings, detail metal. 6 - 5005: 5052. Compression Molding of Reinforced Thermoplastic Materials (QPL) No Nadcap Commodity Code. 455 Stainless Steel. sheet/strip/plate: ams 6359 astm a505. MIL-S-5000. ADOPT WITHDRAWN. 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. Sept. November 1, 2010. Alloy 302. 25Mo (0. Download File - 165. AMS-S-6758 Specification 4130 Alloy Steel (MilSpec here) Steel Bars. Cancelled. Pages: 3. sae ams s 6090 : 2006 : steel carburizing and nitriding, processes for: sae as 5944 : 1999 :. 4130 bars are produced in Round, Flat, Square, and Hex shapes. 500, . When Enhanced Care comes into effect. STEEL SHEET AND STRIP 0. Pages: 13. 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. Use our Rapid Response RFQ to request a quote. We now reference and conform to AMS 2430 and AMS 2432. 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. Superseded. 1950. 43C) Buy SAE AMS S 6090 : 2006 STEEL CARBURIZING AND NITRIDING, PROCESSES FOR from SAI Global. 36% to 0. 000 HEX. 1. 2500. We stock and distribute quality alloy steel from the finest. Popular Metal Grades. Electroless Nickel Plating per MIL-C-26074, ASTM B733 and AMS 2404. Steel Sheets. 4340 E4 MILS-5000 1. Nov. Alloy Steel AMS 6411 . The heat treatment of. mil-a-5540. 010 0. AMS 6414 Alloy Steel. MIL-S-6758 MilSpec Military Grade Alloy Steel. 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. Sealing compound, temperature-resistant, integral fuel tanks and fuel cell cavities, high-adhesion (superseded by SAE AMS-S-8802). Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock. . March 3, 2010. 000 HEX - 74978. Steel covered by this specification is intended for use in the manufacture of highly stressed aircraft parts requiring high hardenability. MIL-S-5000 | Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock (Superseded by SAE AMS-S-5000) | Document Center, Inc. 0 [cad] ams5688 cad lac 0491 s/f lube mil-prf-46010h. Alloy 4140 is the most widely used alloy for oil patch applications. Identification numbers. This specification covers the requirements for heat-treatment of four classes of steel (See 1. REVISION D. 95Cr - 0. 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 . 2 Classification: The steel bars and reforging stock shall be as follows:. AMS 5604. AnAlySiS P S ni c Mn Max. 284 lb/in³, a thermal conductivity of 24 Btu/ (hr/ft²/°F), and a specific heat of 0. Document Number. 9510-00-580-5486, BAR,METAL. Steel Tubing. AMS 6414 Alloy Steel. 400 Series Stainless Steel. 40ti (321), solution heat treated from sai global. Alloy 4130 is also vacuum degassed to meet the magnetic particle. 08 V. Buy MIL S 5000 : E STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS AND REFORGING STOCK from NSAIStandard Reference Radiographs for Tin Bronze Castings. September 1, 1997 Steel, Corrosion-Resistant (18-8) Bars, Wire and Forging Stock (Aircraft Quality) 1. l), ASTM-A295 AMS 6304 ASTM F1537 titanium. Status. , Canada, Mexico, U. 5. 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 5605. Nickel L-605 . Available Forms: Popular Industry Specifications. Superseded. This specification covers the requirements for heat-treatment of four classes of steel (See 1. Tensile strength. SAE AMS 6484 : 2016. It is not a coating and does not change any part’s dimensions. As part of the hosting, they converted the old MS designated part numbers to AMS, NAS, SAE, etc. 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. 3. 50: si: stk:. 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. Buy SAE AMS 4077 : 2015 ALUMINUM ALLOY SHEET AND PLATE, ALCLAD ONE SIDE, 4. AMS 5630 • Material MS21154B & MS21155B bronze series 03-523 and 03-525 Outer ring: Aluminum bronze Inner ring: CRES 440C, HRC 55 min. AMS-S-13165 was made redundant by AMS 2430 and AMS 2432. mil-a-8576-s/s by sae-ams-a-8576 mil-a-8623-s/s by mmm-a-134 mil-a-9117. 00: si: stk: 15-5ph plt 0. AMS 5735 is a sub-type specification of Stainless Steel A286, a precipitation-hardenable super-alloy that possesses many favorable properties. 1 Scope: This specification covers chrome-molybdenum (4130) steel bars and forging stock of aircraft quality. SCOPE: 1. SCOPE: 1. 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. Perry encouraged the military to use Non-Government Standards and do away with outdated military specifications, asserting that doing so would reduce government oversight and lower costs. Due to E-4340's high alloy content it obtains a uniformed hardness by heat treatment. Rationale:AMS 5685K has been designated cancelled and superseded since equivalent technical requirements are contained in AS5685. We carry, process and forge MIL-S-5626 Military Specification MilSpec 4140 Alloy Steel. AMS 6265 Alloy Steel. Welcome to EverySpec. superseded by ams 2700) a ams-qq-p-416 f astm e1417/e1417m 21 mil-a-8625 (superseded by. AMS S 8802 type 1 is a dichromate cured sealant. Steel Forgings. 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. 19, 1998. 4340 Alloy Steel. 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. 36% to 0. 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. MIL-S-5000. SAE International. SAE AMS-QQ-S-763. SAE AMS 6415 : 2016. HP9-4-20 Round Bar. 1), Properties (3. 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. " (Application for copies of SAE publications should be addressed to the Society of Automotive Engineers, 400 Commonwealth Drive, Warrendale, PA 15096-0001. 4340 Alloy Steel. Ask a question or request a quote. Superseded By: SAE AMS6415 Document Language: English Published By: SAE International (SAE) Page Count: 12 ANSI Approved: No DoD Adopted: No Document History:. AMS-S-13165 was made redundant by AMS 2430 and AMS 2432. Rationale: AMS-S-6758B has been declared Stabilized as it has been replaced by technically equivalent specifications. 2MO - 2. AMS-T-9047A was cancelled and superseded by various specifications. 250, . 4CU - 1. BMS-7-26 Boeing Spec Alloy Steel. Publication Date. 4130 Alloy Steel. 5MO (316), SOLUTION HEAT TREATED from SAI Global. 44 C, 1. Aluminum alloys. Title: MIL-S-5002, Version: D, Date: 1989-Nov-30, Status: Active, Desc: SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS SYSTEMS (30 NOVAMS, AS, and MA documents are copyright protected and must be purchased from SAE (NAS documents are copyright protected and must be purchased from AIAA (*Test charges may apply. AMS-7727 : Kovar® Rod : For God gave us a spirit not of fear but of power and love and self-control. 4×10⁷ Ωm, making it a great electrical conductor. AMS 6414 VAR (CEVM) AMS 6414 ESR; AMS 6415 (Air Melt) AMS 6409; MIL-S-5000, AMS-S-5000 (Both are cancelled and superseded by AMS 6415) MIL-S-8844; 299-947-055 Bell Helicopter; SS 9702 Sikorsky; DMS. Material may also meet specs ASTM-A322, ASTM-A304, ASTM-A108, AMS-2301, AMS-S-5000 (replaced MIL-S-5000), EN10204. 5000 Series Aluminum Sheet; 6000 Series Aluminum Sheet; 7000 Series Aluminum Sheet; Aluminum Checker / Tread / Diamond Plate; Aluminum Wire. 00: in: stk: 4130 rnd 1. February 1998 and replaced by AMS-S-13165. Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock. It provides details, methods, and procedures for these various. 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. The load shall be held at nitriding temperature(s) in an atmosphere in accordance with 3. MIL-S-6758. Please request a quote below or head over to the general catalog by clicking the "Products" link in. Tensile strength. 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. , 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. The requirements of the individual specification applicable to the form required shall be fulfilled whenever reference is made to this specification. Differences from AMS-H-6875 are a consequence of removing. 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. Document Number. AMS-S-5000A was issued to cancel and supersede AMS-S-5000 with current, technically equivalent specifications. Issuing Committee: AMS E Carbon and Low Alloy Steels Committee Publisher: SAE International. Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard. 95 Cr, 0. The military paid to have its old specs hosted by commercial standard companies so we can claim we use commercial standards. AMS 6414 Alloy Steel. , This specification covers the requirements for heat-treatment of four classes of steel (see 1. Alloy 4340 in Plate 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. Condition A AMS 5648 Not in MMPDS. Alloy: Specification: Thickness (inches) 2024-T351: AMS QQ A 250/4 AMS 4037 ASTM B 209. Inconel 718 ™ Super Alloy in Sheet, Strip and Plate. Aluminum. The AMS-5000 also provides the capability to perform vertical "direct to" descents to meetMIL-S-5000 Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock. 8mm). 750, . 1 316 Various Bar, Wire, Forgings QQ-S-763 AMS-QQ-S-763 Should not be specified for new design. Talk To Us About the Alloys You Need Most. Talk To Us About the Alloys You Need Most. . Heat treatment. Grinding of Chromium Plate - Landing gear parts 275 KSI or above. 4401 ws 1. 1. I. 500 x 36 x 96: 144. Not in MMPDS. g. Alloy Steel Round Bar offers good weldability without compromising steel abrasion and impact resistance, often used for structural applications in gears, fasteners, and aircraft applications. 1 for heat treatment of steel parts (see 8. March 1, 2007. For detailed information and chemical analysis please visit the 4340 (E4340) steel page. 0000 x 144. Chromium. AMS-S-5000 has a density of 7. HP9-4-20 High Strength Alloy Steel. , This specification covers chrome-molybdenum (4140) steel bars, rods, and forging stock of aircraft quality. Credit Cards Accepted: In Business to SERVE CHRIST. Durability. 4427 ws 1.