A-286 Stainless Steel. Read less…. MIL-S-5000. 0000. mil-a-5090-s/s by mmm-a-132 mil-a-5092-s/s by mmm-a-1617. MIL-S-18729 Military (Department of Defense) Specification MilSpec 4130 Alloy Steel. Dec. . SAE AMS-QQ-S-763. Subscribers can view annotate, and download all of SAE's content. Related Topics: Heat treatment. February 1, 2003. 00, 2. Our discussion here is driven by the fact that several end-users continue to use the original MIL specification for their peening operations. This specification is superseded by a series of individual specifications covering specific forms of this material. 40. Steel Sheets. . Test procedures. Publication Date. Infostore. Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard. Steel Tubing. 1 for sufficient time to produce the specified depth of case. Pages: 7. Subscribers can. Technical Data Sheet. BMS-7-26 Boeing Spec Alloy Steel. Victoria San Juan Cruises sails May through October between Bellingham,. 30V, CONSUMABLE ELECTRODE MELTED 1800 DEGREES F (982 DEGREES C) SOLUTION TREATED AND WORK-STRENGTHENED, 160 KSI (1103 MPA) TENSILE STRENGTH from SAI Global. 2) and the requirements for furnace equipment, test procedures and information for heat-treating procedures, heat-treating temperatures and material (See. Issuing Committee: AMS F Corrosion and Heat Resistant Alloys Committee Publisher: SAE International. Test procedures. Heat Treatment of Steel Raw Materials (STABILIZED Sep 2020) AMSH6875C. 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;. Consumable electrode vacuum remelted, normalized. Showing all 14 results. How to Order; Standards We Provide; Updating, Reporting, Audits. 3 Military and Federal Standards and Commercial Item Descriptions:4MIL-S-7720A, MILITARY SPECIFICATION, STEEL, CORROSION,RESISTANT (18-8) BARS, WIRE AND FORGING STOCK (AIRCRAFT QUALITY) (25 OCT 1967) [S/S BY SAE-AMS-S-7720] MIL-S-7720A, MILITARY SPECIFICATION, STEEL, CORROSION,RESISTANT (18-8) BARS, WIRE AND FORGING STOCK (AIRCRAFT. 7004 State Route 123 Franklin, OH 45005 . 5000 Series Aluminum Sheet; 6000 Series Aluminum Sheet; 7000 Series Aluminum Sheet; Aluminum Checker / Tread / Diamond Plate; Aluminum Wire. 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. Magnesium. S. 8 Ni, 0. 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. 2 Classification: Material shall be. 3. How to Order; Standards We Provide; Updating, Reporting, Audits;. Max Tens MIL-N-14411 Comp 3 (4750) Cap. 80 S150 – – – MSRR 6591/2/5/6/7, 6603/31, 6902/19,Superseded by AWS D17. 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. 8 Ni, 0. This specification covers a carbon steel in the form of sheet, strip, and plate. Magnesium alloys. 3), Reports (4. AMS-S-5000 Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock 2. AMS 5646 Bars / wire / forging. Corrosion. Superseded By: Currently Viewing. Cancelled. Copper. 750"dia: 72. Steel covered by this specification is intended for use in the manufacture of highly stressed aircraft parts requiring high hardenability. Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock. Noncurrent. 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. 26/32 qqs-763c cond h, qqs-764b cond t, astm-a-582 cond t, mil-w-52263. MIL-S-7420, AMS-6440, AMS-2301, AMS-6440, AMS-6444. As aviation enthusiasts we are pleased to serve all of your aircraft alloy needs. 9510-00-993-5760, BAR,METAL. 4571 afnor z6cnd17-11 afnor. AMS-S-6758. SAE ARP 4058 : 2017. 90 0. Use our Rapid Response RFQ to request a quote. 3125, . AMS 6265 Alloy Steel. Use our Rapid Response RFQ to request a quote. Feb. The carbon content ranges from 0. Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock. 1 page 455 Stainless Steel. SAE revised the scope of paragraph 1. 000 HEX - 74978. 000 HEX. This specification covers the specific requirements for 2024 aluminum alloy alclad plate and sheet; the general requirements are covered in AMS-QQ-A-250. 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. Redstone Arsenal, AL 35898-5000 or e-mailed to: usarmy. 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. 10 . Defense industry. Its chromium content provides good hardness penetration, and the molybdenum imparts uniformity of hardness and high. 4130 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 Bar 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]. 080 x 60. SAE AMS 6444 : 2015. plate/sheet/strip: ams 6350. Our service centers are located throughout the U. forging: ams 6382 astm a 646. Service Steel Aerospace stocks Premium Aircraft Quality produced double melted in an. March 1, 2007. Defense industry. , MIL-S-6090A, dated 4 June 1971, and Amendment 2 dated 20 July 1972, is hereby canceled. AMS S 8802 type 1 is a dichromate cured sealant. How to Order; Standards We Provide; Updating, Reporting, Audits. 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 Buy MIL-S-5000 Revision E:1982 STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS AND REFORGING STOCK from SAI Global 5. 4340 Alloy Steel. AMS 5637, QQS-763, MIL-S-7720. Your support ID is: 1013750275635199346. Revision Level. All Grades. Call us. S-5000 COND C4, AMS. 5NI - 1. ams 6348 mil-s-6758 ams 2301 astm a322 astm a331 qq-s-624. AMS 5735 is a sub-type specification of Stainless Steel A286, a precipitation-hardenable super-alloy that possesses many favorable properties. Specifications. Revision Level. AMS 5571 Seamless tube. AMS 5575 Welded tube. 80/1. Alloy Steel Round Bar diameter sizes range from 0. Subscribers can view annotate, and download all of SAE's content. Test procedures. SAE AMS 6484 : 2016. We speak metal!302 mil-s-7720, ams-s-7720 astm-a-276, astm-a-479, asme-sa-479. 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. All Grades. It has a density of 0. Related Topics: Heat resistant materials. THE METAL BUYERS’ TRUSTED RESOURCE. 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. 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. 284 lb/in³, a thermal conductivity of 24 Btu/ (hr/ft²/°F), and a specific heat of 0. mil-a-3316 mil-a-3920. Sorta. 3 ConditionAMS-6532 Aermet 100 AMS-77184750 (Exc. 1 Scope: This specification covers the requirements for compositions of corrosion-resistant (18-8) steel bars, rods, wire and forging stock. However, it appears to me that SAE split out the heat treatments of 4 classes of finished steel parts into 4 more specs. AMS-S-5000. ADOPT WITHDRAWN. AMS-S-13165 was made redundant by AMS 2430 and AMS 2432. Multi - user online standards collection: secure, flexibile and cost effective. Historical. 4340 RD BAR COND C 2. 1 pageMIL-A-8625 Aluminum Anodic Coatings MIL-A-8625 is the military specification for Anodic Coatings for Aluminum and Aluminum Alloys. 4441 ws 1. Corrosion resistant alloys. Material may also meet specs ASTM-A331, ASTM-A304, ASTM-A108, AMS-2301, AMS-S-5000 (replaced MIL-S-5000), EN10204. 2500. HARD COAT (S/S BY AMS 2469)4340 Alloy Steel. It is considered similar but not equivalent, as it does not cover parts (refer to AMS2759). AMS 5604. ”. 48, 160 Lane, Da Hoo Rd. Grinding of Chromium Plate - Landing gear parts 275 KSI or above. Status. , This specification presents requirements for the carburizing and nitriding of carbon and allow steels to produce the mechanical properties specified by drawings, detail specifications,. 5V (0. Revision Level. 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. 1 for heat treatment of steel parts (see 8. 1998-04-01. 0000 x 144. 15-5ph plt 0. 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). Steel. (Copies of this document are available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001. View DetailsCalifornia Metal & Supply, Inc. Rationale: AMS-S-7720B stabilizes this document because equivalent technical requirements are contained in other specifications. 1), Properties (3. MIL-S-6090A, MILITARY SPECIFICATION: STEELS USED IN AIRCRAFT CARBURIZING AND NITRIDING, PROCESS FOR (4 JUN 1971) [S/S BY SAE-AMS-S-6090]. MIL-S-6758 MilSpec Military Grade Alloy Steel. 1954-05-01. Page Count. 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. 32 KB. Alloy Designation: UK Specifications: US Specifications: US Federal Specifications: European Specifications: Other: 5005: BS N41 5005 : A-G0. This mil-spec covers the requirements for electrochemically-formed anodic coatings on aluminum and aluminum alloys for non-architectural applications. <br/>Your support ID is. SAE AMS 6484 and SAE AMS S 5000. AMS 6414 Alloy Steel. AMS5085. mil-a-907. MIL-T-9047G Amendment 2 was cancelled, and superseded by SAE (Society of Automotive Engineers). com. T. 10 pages SAE AMS 6485 : 1989. 5Mg 1. AMS 6414, AMS 6415, AMS 6484, AMS 6409, AMS-S-5000, BMS7-28, SS 9702: 4340 Plate and Sheet: AMS 6454 (VAR PLATE), AMS 6359: For more information on 4340 steel, call Aero-Vac at 877-237-6822. Outer ring: Alloy steel, AMS-S-5000, AMS-S-6758 or AMS-S-6050 Inner ring: CRES 440C, HRC 55 min. 0. Condition A AMS 5648 Not in MMPDS. 376. March 1, 2007. 0000. ADOPT WITHDRAWN. c. 5000: 15-5ph ams5862 . LAMINATED SHEET. MIL-S-5000 | Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock (Superseded by SAE AMS-S-5000) | Document Center, Inc. Showing 1 to 25 of 88 entries. Historical. Publication Date. All Grades. Learn More ». 010 0. Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock. com materials stocked Reliance Aerospace Solutions STAINLESS STEEL SPECIFICATIONS 13-8 PH AMS 5629, DMS 2100, STO160LB0013, ASTM-A-564 (XM-13)Specs: AISI. mil-a-3316 mil-a-3920. 19, 1998. Available Forms: Popular Industry Specifications. 69 in addtion to MIL-C-5056:. 316L Condition A Sheet, Strip, Plate QQ-S-766 AMS 5507 Not in MMPDS. Publication Date. The hardenability and weldability of Alloy 4130 are considered equivalent to 8630 (MIL-S-6250) . 01/714323 DC : DRAFT OCT 2001. BAC 5019. 35 5. S. Nickel. 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. AMS 2700. 6415, AMS. Aluminium Welding Wire;. QQ-P-35, Type VI: AMS 2700, Method 1, Type 6. AMS 6931 6al/4v Titanium Alloy. astm-d2564. Sealing compound, low adhesion, for removable panels and fuel tank inspection plates (superseded by SAE AMS-3284). George VI had undergone a lung operation in September 1951 from which he never fully recovered. 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. All Grades. 0CR - 1. 6al/4v Alpha/Beta Titanium Alloy. MIL-S-6758. 1), ASTM-A295 17-22 AMS 6304 COBALT ALLOYS 28CR-6Mo ASTM F1537. MIL-S-5000E (NOTICE 2), MILITARY SPECIFICATION: STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS, AND FORGING STOCK (11 AUG 2000) [S/S BY SAE. MIL-S-5000E, MILITARY SPECIFICATION: STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS, AND FORGING STOCK (12-NOV-1982) [S/S BY SAE-AMS-S-5000]. 455 Stainless Steel. Our extensive product offerings include alloy, stainless, nickel, aluminum, titanium, carbon and cast iron. 85g/cm³ and a melting point of 1450°C. ›. Kalama, W98625 USA PH: 877-AEROVAC (877-237-6822) FX: 360-673-0100 sales@aerovacalloyforge. 303 sul mill-s-7720, mil-w-52263 ams-5640 type 1, qqs-763c, qqs-764b, astm-a-582 astm-a-320 grd b8f. Revision Level ADOPT WITHDRAWN Status Superseded Publication Date March 3, 2010 Page Count 1 page AMS-S-5000 Steel, Chrome-Nickel-Molybdenum (E4340) Bars &. 4130 Alloy Steel. AMS 6415 - AISI 4340 (E4340) Round Bar Hot Rolled Size Table. , Canada, Mexico, U. 1. com Performance metal solutions ISO 9001: 2008, AS9100: 2009 Revision CThis document is intended to replace MIL-H-6875 (cancelled) and AMS-H-6875 (stabilized) for new design or when approved by the Cognizant Engineering Organization (CEO) on existing design. 6 - 5005: 5052. Type 321's general corrosion is less than Type 302 . heavy duty, metallic reinforced, 400 degree f, 5000 psi hydraulic and pneumatic: sae as 5420 : 2017 : hose assembly, heated, 125 psig, lined. 3. Use our Rapid Response RFQ to request a quote. Identification numbers. Standard Digital Reference Images for Inspection of Aluminum Castings. Different grades of steel are achieved by adding other alloying elements, such as manganese, nickel, chromium, titanium and molybdenum to the basic mix. Nickel INVAR 36 . QQ-P-35 was superseded by AMS-QQ-P-35 for aerospace products and AMSQQP35 [canceled, affil. Publication Date. Status. Manganese. AMS-S-5000 - ADOPT WITHDRAWN - SUPERSEDED -- See the following: AMS-6415 AMS-6484 Show Complete Document History. 6Cu 0. Per D8-5000 Finish Code VF-1. AMS-S-5000 Specification 4340 High Tensile Steel (MilSpec here) Steel Bars. Also known as: SAE AMS 5735 SAE MOBILUS. 1 Al. Material may also meet specs ASTM-A322, ASTM-A304, ASTM-A108, AMS-2301, AMS-S-5000 (replaced MIL-S-5000), EN10204. The carbon content ranges from 0. Use our Rapid Response RFQ to request a quote. This alloy is known for its excellent mechanical properties, corrosion, and heat resistance. 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. 1. Enter code: Category Controls & Processes. 32 KB. 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. Buy SAE AMS S 5000 : 2007 STEEL, CHROME-NICKEL-MOLYBDENUM (E4340) BARS AND REFORGING STOCK from SAI GlobalMIL S. 38-0. Find Standards By. 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. 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. AMS6361G. 15/. ¼ Hard MIL-S-5059 AMS 5907 MMPDS Section 2. 1, 3. Carbon. The military paid to have its old specs hosted by commercial standard companies so we can claim we use commercial standards. 38 - 0. Steel, Corrosion Resistant, Sheet and Strip 18Cr - 8Ni Cold Rolled, 150 ksi (1034 MPa) Tensile Strength AMS5518NAMS 6414. became AMS-F 7190). 0 Ni, 2. 2. 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. SAE AMS-S-5000. Credit Cards Accepted: In Business to SERVE CHRIST. Classes 202 and 302: Class 302 is intended for use where severe corrosion is. AMS 6414 Alloy Steel. 17-4 (PH) Stainless Steel in Sheet, Strip and Plate. As part of the hosting, they converted the old MS designated part numbers to AMS, NAS, SAE, etc. 1. Also known as: SAE AMS 3651 SAE MOBILUS. 7. MIL-STD-2175A, MILITARY STANDARD: CASTINGS, CLASSIFICATION AND INSPECTION OF (25 AUG 1993) [S/S BY SAE-AMS-STD-2175]. 4427 ws 1. 1 pageRationale: AMS-QQ-A-250/11 has been designated Cancelled and Superseded because equivalent technical requirements are provided by other specifications. 7 Cooling The load shall be cooled from the nitriding temperature in a suitable atmosphere to 300 °F (149 °C) or below. Inconel 718 ™ Super Alloy in Sheet, Strip and Plate. HP9-4-20 High Strength Alloy Steel. This document is available in either Paper or PDF format. Titanium alloys. 6×10^-6 in/ (in·°F). SAE-AMS-H-6088, WITHDRAWAL OF ADOPTION NOTICE: HEAT TREATMENT OF ALUMINUM ALLOYS (27-JAN-2010) [SUPERSEDES MIL-H-6088H] [NO S/S DOCUMENT]. Superseded date: 04-11-2012. 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. MIL-STD-2154 Military (Department of Defense) Specification MilSpec Alloy Inspection MilSpec Ultrasonic Inspection. AMS 6257 Specification 300M/4340M Low Alloy Steel. Sealing compound, temperature-resistant, integral fuel tanks and fuel cell cavities, high-adhesion (superseded by SAE AMS-S-8802). 3. We carry, process and forge MISC United States Federal GSA Specification QQ-S-764 Grade Stainless Steel. 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). Round Bar, Flat Bar, Plate. 1950. MIL-S-5000 | Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock (Superseded by SAE AMS-S-5000) | Document Center, Inc. 1) per SAE AMS 6415 (formerly SAE AMS-S-5000 and formerly MIL-S-5000) or an alternative VAR (Vacuum Arc Remelt) SAE 4340 steel (Grade B, see 7. 5Mg 0. Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock AMSS5000. Revision Level. This specification covers the requirements for heat-treatment of four classes of steel (See 1. 13 Cr, 8. Document Number. MIL-S-7124 › Sealing Compound, Polysulfide, Accelerator Required, for Aircraft Structures (Superseded by SAE AMS-S-7124) MIL-S-7124 - REV B CANCELLATION 2 - SUPERSEDED -- See the following: AMS-S-7124 Show Complete Document History. 0. Find the right standards and certifications for your needs with SAE. If you require technical assistance or would like to receive a quote, please call our Customer Service team TOLL FREE at (866) 610-1660. 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. 8Ni - 0. mil-s-5000e (notice 1), military specification: steel, chrome-nickel-molybdenum (4340) bars, and forging stock (27 sep 1995) [s/s by sae-ams-s-5000] Future acquisitions for this material should refer to AMS 6415, Bars, Forgings, and Tubing, 0. Revised. 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. 3, 3. 75-110. AMS ASME; 1050: Aluminum Coil: Aluminum Strip: Aluminum Plate: 1060: Aluminum Coil: ASTM-B209: Aluminum Strip. 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. 2MO - 2. 302 Foil (Shim) is available in various thicknesses. 4340 E4 MILS-5000 1. 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. Created Date: 8/24/2022 10:15:41 AMBuy SAE AMS 2485 : 2016 COATING, BLACK OXIDE from SAI Global. 85 0. 38 - 0. is a world wide supplier of quality alloy steel metals. The heat treatment of parts fabricated. 40-0. , constitutes a requirement to conform to the applicable provisions of the documents. Rationale: AMS-S-13165 has been designated Cancelled and Superseded because equivalent technical requirements are provided by AMS 2430. 6 - 5005: 5052. GENERAL SPECIFICATION GUIDE FOR MECHANICAL GEARED ROTARY ACTUATORS. 3. , This specification covers premium quality, multiple vacuum melted, low alloy steel bars, reforging stock, and mechanical tubing intended for use at. We carry, process and forge AMS 5604 Specification 17-4PH Stainless Steel. Revision A, March 2007. superseded a superseded standard is one,. 28/. Use our Rapid Response RFQ. Steel Carburizing and Nitriding, Processes for.