HP9-4-20 High Strength Alloy Steel. Read more…. plate/sheet/strip: ams 6350. The balance of these elements makes AMS 6414 a high. 56C (SAE 1050) AMS5085 – available for purchase at $40. SCOPE: 1. Nickel. Heat treatment. S-5000 COND C4, AMS. 60Mn (2024-T3) (2024-T351) Solution Heat Treated QQ-A-250/4. AMS 5558 Welded /thin wall tube. 4571 afnor z6cnd17-11 afnor. Rationale: AMS-QQ-S-763D stabilizes this document because this document is no longer state of the art and other documents contain similar but not necessarily equivalent requirements. 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. tw; Taipei Branch Office. MIL-STD-2175A, MILITARY STANDARD: CASTINGS, CLASSIFICATION AND INSPECTION OF (25 AUG 1993) [S/S BY SAE-AMS-STD-2175]. Classes 202, 302, and 305: When sensitization cannot be tolerated classes 202, 302 and 305 are not recommended for use. 4340 High Tensile Steel in AMSS5000 Specification, per SAE International: “This specification covers electric furnace steel bars and reforging stock of. Country: USA: Britain: Britain: Japan: Standard: ASTM A29: EN 10250: BS 970: JIS G4103: Grades: 4340:. Steel, Corrosion Resistant, Sheet and Strip 18Cr - 8Ni Cold Rolled, 150 ksi (1034 MPa) Tensile Strength AMS5518NAMS 6414. MIL-S-7720 is a Military Specification for 300 Series Stainless Steel MIL-S-7720A (AMENDMENT 2), MILITARY SPECIFICATION, STEEL, CORROSION,RESISTANT (18-8) BARS, WIRE AND FORGING STOCK (AIRCRAFT QUALITY) (26 JUL 1974) [S/S BY SAE-AMS-S-7720]. Status. Document Number. D. Aeronautical Design Standard (ADS) Documents. Condition A AMS 5648 Not in MMPDS. , This specification covers premium quality, multiple vacuum melted, low alloy steel bars, reforging stock, and mechanical tubing intended for use at tensile strength levels of 260,000 psi (1795 MPa) and above. Steel Extrusions. AMS 6265 Alloy Steel. 20 Mo. 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. Alloy Steel Grade: AISI 4340. 40ti (321), solution heat treated from sai global. Round Bar, Flat Bar, Plate. We carry, process and forge MISC United States Federal GSA Specification QQ-S-766. Grinding of Chromium Plate - Landing gear parts 275 KSI or above. Steel. com. QUALITY MANAGEMENT SYSTEMS - REQUIREMENTS FOR AVIATION, SPACE AND DEFENSE DISTRIBUTORS. Changed AMS I-6875 to AMS-H-6875. 28 - 0. I. 4. 2% offset 1000 psi (MPa) 30 (207) min Elongation % 35% min Hardness. 43C) Buy SAE AMS S 6090 : 2006 STEEL CARBURIZING AND NITRIDING, PROCESSES FOR from SAI Global. Heat treatment. This specification covers electric furnace steel bars and reforging stock of aircraft quality. Alloy E 4340 is a widely used deep-hardening constructional steel. REVISION C. 7M Pub Date 01/2015 >oupled Multiwaypoint VNAV – The C AMS-5000 calculates one vertical path through multiple lateral upgrade your Beechjet waypoints, enabling a fully stabilized descent or approach. 2500. Type 321's general corrosion is less than Type 302 . 6Cu 0. Durability. Issuing Committee: AMS G Titanium and Refractory Metals Committee Publisher: SAE International. 3. 4130 bars generally meet several AMS specifications, but the most common are AMS-S-6758 and AMS- 6348, but several others may also apply. com materials stocked Reliance Aerospace Solutions STAINLESS STEEL SPECIFICATIONS 13-8 PH AMS 5629, DMS 2100, STO160LB0013, ASTM-A-564 (XM-13)Specs: AISI. 1954-05-01. BMS-7-26 Boeing Spec Alloy Steel. AMS 6278: Steel, Bars, Forgings and Tubing: K91231: CBS-50NIL: RFQ: AMS-DTL-22499: Shim Stock Laminated: RFQ: ASK US A. LAMINATED SHEET. SAE AMS-S-7720. Canceled and inac ve MIL-T and AMS specifica ons are referenced for replacement purposes and should not be specified for new designs. Proposed changes to the standard by DoD activities must be submitted to the DoD Adopting Activity at Defense Standardization Program Office, 8725 John J. Buy SAE AMS S 5000 : 2007 STEEL, CHROME-NICKEL-MOLYBDENUM (E4340) BARS AND. 4340 VAR AMS 6414 is a low alloy Chromium-Nickel-Molybdenum steel capable of being heat treated to high strength levels. 302 Foil (Shim) is available in various thicknesses. The heat treatment of parts fabricated. , This specification covers premium quality, multiple vacuum melted, low alloy steel bars, reforging stock, and mechanical tubing intended for use at. 4130 Alloy Steel in AMS-S-6758 per SAE International: “This specification covers chrome-molybdenum (4130) steel bars and forging stock of. MIL-S-5000. Materials are available in sheets, plates and hex, square, flat and round bars. Applications: Aircraft Landing Gear:ÐÏ à¡± á> þÿ ã þÿÿÿ d å f ç h é j ë l. SAE AMS-S-5000. AMS 5564, AMS 5566, AMS 5569 (AMS-T-6845 noncurrent, MIL-T-6845D canceled) 304/LAMS 6484 Bars / Forgings N&T AMS-S-5000 MIL-S-8844 Cl1 ASTM A322 ASTM A331 AISI E4340 BMS-7-28 BPS-299-947-055 BPS-299-949-055. Steel Forgings. SAE AMS-H-6875. 302 stainless steel is available in Sheet, Strip, Plate, Angles, Bars (Round, Hexagon, Squares, Flats). MIL-T-6845D, MILITARY SPECIFICATION: TUBING, STEEL, CORROSION-RESISTANT (S30400), AEROSPACE VEHICLE HYDRAULIC SYSTEM 1/8 HARD CONDITION (26-APR-1985) [S/S BY SAE-AMS-T-6845]. 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). Hendrickson Dr. Rationale: AMS-S-13165 has been designated Cancelled and Superseded because equivalent technical requirements are provided by AMS 2430. 750, . Hydraulic…SAE AMS S 13165 : 1997. 455 Stainless Steel. 7225 42CrMo4 EN10083-1: UNS G41400 SCM 440: 4330 Mod VM N&T: AMS 6411 AMS 6427 MIL-S-8699 AMS 2300. Standard Digital Reference Images for Inspection of Aluminum Castings. 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. July 1,. Revision Level ADOPT WITHDRAWN Status Superseded Publication Date March 3, 2010 Page Count 1 page AMS-S-5000 Steel, Chrome-Nickel-Molybdenum (E4340) Bars &. Materials properties. 1), and results from a Five-Year Review and update of this specification. 40/. AMS-S-5000. BAC 5019. 6×10^-6 in/ (in·°F). Status. No. AMS5085. Document Number. 1) per SAE AMS 6414, and both are heat treated to 260 to 280 ksi (pounds per square inch ×1000). 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]. Chromium. AMS-S-6758 has excellent physical properties. Test procedures. This alloy has a coefficient of thermal expansion of 17. Publication Date. 1) by users or their vendors or subcontractors. 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. 48, 160 Lane, Da Hoo Rd. November 1, 2002. 625, . 3). HP9-4-30 High Strength Alloy Steel. Si cr Max. These include high strength at elevated temperatures, good high-temperature corrosion resistance up to 1300 °F (700 °C), and excellent low-temperature non-magnetic strength, down to -320 °F (-196 °C). Nickel INVAR 36 . Document Number. 00, 1. Steel Reforging Stock. 4401 ws 1. 26/32 qqs-763c cond h, qqs-764b cond t, astm-a-582 cond t, mil-w-52263. 2 Mo, 1. g. 90 0. MIL-S-13165. c. 4130 Alloy Steel in Department of Defense Military MilSpec Specification MIL-S-6758 per SAE International’s AMS Standard: “This specification covers chrome-molybdenum (4130) steel bars and forging stock of aircraft quality. E. SAE revised the scope of paragraph 1. It is considered similar but not equivalent, as it does not cover parts (refer to AMS2759). Perry, was at the forefront of military specification reform. All Grades. 30 2. Page Count. 20Mo (0. 7 added Interim C 07-20-2007 Interim Revision (General Revision—Document Completely Rewritten) AMS 4037 2024 Aluminum Alloy, Aluminum Sheets and Aluminum Alloy Plate 4. 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. 45CR (0. customer’s supply chain. 00. Subscribers can view annotate, and download all of SAE's content. 6al/4v Alpha/Beta Titanium Alloy. 010 0. Buy MIL S 5000 : E STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS AND REFORGING STOCK from NSAIStandard Reference Radiographs for Tin Bronze Castings. Per D8-5000 Finish Code VF-1. Related Topics: Test procedures. 250 DIA. Metals. 4340 E4 MILS-5000 1. Stainless Steel Bar Specifications UNS = Unified Numbering System TYPE = Commonly used grade name AMS = Aerospace Society for Testing and Materials ASTM = American Society for Testing and Materials FEDERAL = Federal specifications UNS TYPE AMS ASTM FEDERAL CHARACTERISTICS STOCK CHECK S13800 13-8 PH 5629 A-564 –. Titanium alloys. 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 . 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. 4340 High Tensile Steel in AMSS5000 Specification, per SAE International: “This specification. Status. Publication Date. MIL-S-6090A (NOTICE-3), MILITARY SPECIFICATION: STEELS USED IN AIRCRAFT CARBURIZING AND NITRIDING, PROCESS FOR (20 AUG 1998) [S/S BY SAE-AMS-S-6090]. We carry, process and forge MIL-S-5000 Military Specification MilSpec 4340 High Tensile Steel. This specification covers electric furnace steel bars and reforging stock of aircraft quality. 4364: ABS 5064: 7175: AMS 4148 7175-T6 Die Forgings: IPS03-02-000/0008-03: 7175:. This Standard has been added successfully to your. 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. 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. What is alloy 4140 steel? Alloy 4140 is an oil-hardening steel of relatively high hardenability. 3 This test method specifies the use of air melted SAE 4340 steel (Grade A, see 7. March 1, 2007. I recommend you purchase the AMS for your quotation. 1. 6415, AMS. 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. sheet/strip/plate: ams 6359 astm a505. Superseded. AMS 6931 6al/4v Titanium Alloy. Steel, Corrosion Resistant, Bars, Wire, Shapes, and Forgings. Use our Rapid Response RFQ to request a quote. Distributor of alloy steel AMS-S-5000 for aerospace, food service, metalworking, industrial, chemical and petrochemical applications. Please enable JavaScript to view the page content. December, 2007, and has been superseded by AMS 2430, Shot Peening. Related Topics: Heat resistant materials. February 1998 and replaced by AMS-S-13165. Steel covered by this specification is. 95 Cr, 0. Not in MMPDS. We speak metal!Future acquisition of this item should refer to SAE-AMS-S-6758, "Steel, Chrome-Molybdenum (4130) Bars and Reforging Stock (Aircraft Quality). Since the material usually comes in the annealed condition, additional heat treatments (oil quenching and tempering, or normalizing and tempering) can produce parts with even higher strength and fatigue resistance. Inconel X750 ™ Super Alloy in Sheet, Strip and Plate. 3Mo - 1. Alloy Designation: UK Specifications: US Specifications: US Federal Specifications: European Specifications: Other: 5005: BS N41 5005 : A-G0. This specification is superseded by a series of individual specifications covering specific forms of this material. 8. MIL-S-5000. MIL-S-5000E (NOTICE 2), MILITARY SPECIFICATION: STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS, AND FORGING STOCK (11 AUG 2000) [S/S BY SAE. , Canada, Mexico, U. Call us. All Grades. 32 KB. of MIL-S ( steel)MIL-S-5000E-4340 AEROSPACE. Condition A AMS 5648 Not in MMPDS. Issued. 5000 ht: 15-5ph ams5862 plate cond h1150: 136. became AMS-F 7190). Manufacturing processes. 50: si: stk:. 187" (4. Report Problem (email) Status: Cancelled. Revision Level. Version: F. REVISION E. 1) exceptions to the transfer technique, allows a type 1 option (5. K, France, Singapore, and Shanghai. Status. Related Topics: Heat treatment. Max Tens MIL-N-14411 Comp 3 (4750) Cap. QQ-P-35C/AMS-QQ-P-35A SPECIFICATIONS Passivation Types Type I – Withdrawn Type II – 20-25 v% Nitric, 2-2. 6Cu 0. SAE AMS 6485 : 1989. Our service centers are located throughout the U. This specification covers the specific requirements for 2024 aluminum alloy alclad plate and sheet; the general requirements are covered in AMS-QQ-A-250. Aero-Vac Alloys & Forge is the metal buyer's trusted resource!scope: This specification establishes general requirements for the processes listed in 3. Our extensive product offerings include alloy, stainless, nickel, aluminum, titanium, carbon and cast iron. 2 Classification: The steel bars and reforging stock shall be as follows:. Max. Document Number. 80Cr - 1. ”. Historical. Manufacturing processes. 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. Vacuum induction and consumable. 35 5. 93 - 1. 38-0. Reactions: Eredhel. Pages: 3. 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. AMS-S-5000 Specification 4340 High Tensile Steel (MilSpec here) Steel Bars. 38 - 0. AMS 6265 Alloy Steel. 080 x 60. 661. 5000 Series Aluminum Sheet; 6000 Series Aluminum Sheet; 7000 Series Aluminum Sheet; Aluminum Checker / Tread / Diamond Plate; Aluminum Wire. Rationale: AMS-S-6758B has been declared Stabilized as it has been replaced by technically equivalent specifications. 📝 Amendments Available. SAE AMS-S-5000 ( Complete Document ) Superseded By: 1999 Edition, March 1999. 6511: EN24/817M40: SNCM 439/SNCM8: AMS 6415 Uses. REVISION D. Technical Data Sheet. SAE AMS-QQ-S-763. Issuing Committee: AMS F Corrosion and Heat Resistant Alloys Committee Publisher: SAE International. 1 MIL-H-81200 replaced by AMS-H-81200. 47-0. Status. 376. 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. REVISION C. Revision Level. 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. QQ-P-35, Type VI: AMS 2700, Method 1, Type 6. However, it appears to me that SAE split out the heat treatments of 4 classes of finished steel parts into 4 more specs. com I pierce-spafford. 0. Alloy Steel AMS 6409 . SAE-AMS-S-5000 Scroll down to access document images. BC Ferry: Washington - Bellingham - Victoria - British Columbia Travel and Adventure Vacations. 4130 Alloy Steel. 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. Report Problem (email) Status: Cancelled. It has a density of 0. Feb. This is a standard used by the aerospace industry to describe and control the passivation of stainless steel. Publication Date. <br/>Your support ID is. 455 Stainless Steel. Buy SAE AMS H 6875 : 2010, the susperseded specifications for heat-treatment of four classes of steel, from SAE International. Material UNS ASTM SAE/AISI AMS SAE EN FED JIS DIN BS O. 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. 4435 ws 1. mil-a-5090-s/s by mmm-a-132 mil-a-5092-s/s by mmm-a-1617. inspection standards of AMS 2301. superseded by ams 2700) a ams-qq-p-416 f astm e1417/e1417m 21 mil-a-8625 (superseded by. BMS-7-26 Boeing Spec Alloy Steel. 08 V. SAE AMS-S-5000, Revision A, March 2007 - Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock Steel covered by this specification is intended for use in the manufacture of highly stressed aircraft parts requiring high hardenability. The balance of these elements makes AMS 6414 a high. Status. 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. MIL-S-5000 Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock. 7004 State Route 123 Franklin, OH 45005 . AMS 6411 AMS 6427 MIL-S-8699 AMS 2300 AMS 6411 Bar Stock List: ASTM A646 : UNS K23080 BMS 7-122 BMS 7-27 CE-0906 EMS-96242 FMS-1012 GM-1010: 4340 E4340: AMS 6359 Sheet / strip / plate AMS 6409 Bars / Forgings N&T AMS 6414 Vac Melt Bars / Forgings AMS 6415 Bars / Forgings AMS 6484 Bars / Forgings N&T AMS-S-5000 MIL-S. We speak metal!302 mil-s-7720, ams-s-7720 astm-a-276, astm-a-479, asme-sa-479. 60 Si, 0. MIL-T-9047G Amendment 2 was cancelled, and superseded by SAE (Society of Automotive Engineers). SAE AMS-S-5000. HP9-4-30 High Strength Alloy Steel. This specification. 36% to 0. Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard. american aircraft quality alloy steel bar-analysis cmnpmax. (s/s by sae ams-h-6875) h amm2 mil-p-23377 (superseded by mil-prf-23377) f mil-p-85582 (superseded byAMS 6359 AMS 6409 AMS 6414 AMS 6415 AMS 6454 ASTM A29 (4340) ASTM A320 (L43) ASTM A322 (4340) ASTM A331 (4340) ASTM A506 (4340) ASTM A519 (4340) ASTM A646 (4340-7) ASTM A711 ASTM A752 (4340) ASTM A829 MIL S-5000 SAE J1397 (4340) SAE J404 (4340) SAE J412 (4340) UNS G43400: Chemistry Data. This document comes with our free Notification Service, good for the life of the document. SAE MOBILUS. AMS 6414 Alloy Steel. Buy SAE AMS S 5000 : 2007 STEEL, CHROME-NICKEL-MOLYBDENUM (E4340) BARS AND REFORGING STOCK from SAI Global. 4340 Alloy Steel. Inconel 706 ™ Super Alloy in Sheet, Strip and Plate. STANDARD Steel Tubing, Seamless 0. Issuing Committee: AMS E Carbon and Low Alloy Steels Committee Publisher: SAE International. 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. (Copies of this document are available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001. Document Number. AMS-S-6758. TITANIUM AND TITANIUM ALLOY BARS (ROLLED OR FORGED) AND REFORGING STOCK, AIRCRAFT QUALITY (S/S BY SAE-AMS-T-9047)Buy SAE AMS S 5000 : 2007 STEEL, CHROME-NICKEL-MOLYBDENUM (E4340) BARS AND REFORGING STOCK from SAI GlobalBoeing Helicopter support only, Per D8-5000 Finish Code VF-1. 2. Use our Rapid Response RFQ to request a quote. Find the right standards and certifications for your needs with SAE. Use our Rapid Response RFQ to request a quote. Corrosion. This specification covers a carbon steel in the form of sheet, strip, and plate. 4340 E4 MILS-5000 1. Tensile strength. 40. Federal Standard 595C from 2008 has now been cancelled and has been superseded by AMS Standard 595A from 2016 and adminstered by SAE®. 75, 2. 7 Cooling The load shall be cooled from the nitriding temperature in a suitable atmosphere to 300 °F (149 °C) or below. Pages: 7. 4Cu 1. AMS5085. Effective January 1, 2009, the requirements of the latest issue of AMS 2430 shall be fulfilled whenever reference is made to the cancelled. 6Zn 2. AMS 6265 Alloy Steel. 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. HP9-4-20 High Strength Alloy Steel. 3. 1 pageRationale: AMS-QQ-A-250/11 has been designated Cancelled and Superseded because equivalent technical requirements are provided by other specifications. AMS 4109 7175-T736 Superseded by AMS 4149: WS 3. 5Mg 1. All Grades. This product is not available online at this time. 875, 1. 4Cu 1. HP9-4-20 High Strength Alloy Steel. SAE AS 9120 : 2016. 3 Military and Federal Standards and Commercial Item Descriptions:4SEAL, BONDED, ALUMINUM ALLOY 6061-T6, AMS4027, MOLD IN GROOVE, NBR RUBBER, AMS-P-5315: SAE AS 85052 : 2015 : CLAMP ASSEMBLY, LOOP TYPE, CUSHIONED, GENERAL SPECIFICATION FOR: SAE J 24714 : 2001 : Fluid Systems—Connector Tubes—General Specification and Part Standard: SAE AS 4510 :. 5Ni) AMS 5556 Seamless/ welded tube. 6000 - Magnesium / Silicon - good machinability, corrosion resistance, moderate strength. , This specification covers chrome-molybdenum (4130) steel bars and forging stock of aircraft quality. 5, 1973. Alloy Steel. 3) test procedures. The heat treatment of. Alloy 302. Peening. HP9-4-20 Round Bar. 69 in addtion to MIL-C-5056:. Talk To Us About the Alloys You Need Most. 3V AMS5735 – available for purchase at $48. Email：hanjustdoit@gmtc. Alloy 4130 (AISI 4130) is a chromium molybdenum alloy steel being a widely used Aircraft Steel due to its weldability, ease of fabrication and mild hardenability. ams 6351 astm a505 mil-s-18729. AMS 6931 6al/4v Titanium Alloy. Skip to content - Show main menu navigation below - Close main menu navigation below. 010 0. Country: USA: Britain: Britain: Japan: Standard: ASTM A29: EN 10250: BS 970: JIS G4103: Grades: 4340: 36CrNiMo4/ 1. HP9-4-20 High Strength Alloy Steel. mil-a-13881 mil-a-13883 mil-a-21366 mil-a-22010-s/s by astm-d2564 mil-a-22895 mil-a-23941 mil. This comprehensive database includes thousands of current aerospace material specifications issued by SAE’s aerospace materials committees. Historical. The insurance estimator will help personal customers understand what the upcoming premium savings will mean to them. HP9-4-30 High Strength Alloy Steel. All Grades. BMS-7-26 Boeing Spec Alloy Steel. Alloy Steel AMS 6359 . Cancelled. HP9-4-20 High Strength Alloy Steel. Steel Sheets.