Customer Reviews - What Customers Say About Us! "Just wanted to say thanks for your efforts and updates" "I always try you as you often keep stock that can't be found elsewhere"superseded by MIL-A-8625) AMS-C-27725 D Coating, Corrosion Preventative, for Aircraft Integral Fuel Tanks, for Use to 250 °F (121 °C) AMS-H-6875 C Heat Treatment of Steel Raw Materials (Supersedes MIL-H-6875) AMS-H-6088 C Heat Treatment of Aluminum Alloys (This specification has been cancelled and has been. SAE ARP 4058 : 2017. 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. Publication Date. Cancelled. With that roman numeral type reccomendation from QQ-P-35 in hand, you can make a corresponding AMS 2700 (Method 1) callout by changing the roman numberal to the corresponding arabic numneral as shown below: QQ-P-35, Type II: AMS 2700, Method 1, Type 2. Page Count. This alloy has a coefficient of thermal expansion of 17. Minimum Mechanical Properties required property by ASTM A240 and ASME SA 240. 0. 1 Inspection, Ultrasonic, Wrought Metals, Process SUPERSEDED BY AMS2175 Fusion Welding for Aerospace Application Superseded by SAE-AMS-6360,6361,6362 Tape and Sheet, Adhesive, Rubber and Cork Composition Tubing, Steel, Corrosion-Resistant S30400 1/8 H Tube, Alum. AMS 4045 7075 Aluminum Alloy, Aluminum Sheets and Aluminum Alloy Plate 5. 4404 ws 1. HP9-4-20 High Strength Alloy Steel. AMS2750F is typically communicated via industry standards such as SAE/AMS specifications as well as customer purchase orders and part prints. 90 0. 36% to 0. 5CR - 10. Our service centers are located throughout the U. AMS 5605. Superseded. 1 Scope: This specification covers chrome-molybdenum (4130) steel bars and forging stock of aircraft quality. The insurance estimator will help personal customers understand what the upcoming premium savings will mean to them. All Grades. Redstone Arsenal, AL 35898-5000 or e-mailed to: usarmy. MIL-S-40046D (NOTICE 1), MILITARY SPECIFICATION: SLING, FLAGSTAFF (08-JAN-1999) MIL-S-9479C (NOTICE-1), MILITARY SPECIFICATION: SEAT SYSTEM, UPWARD. Nickel Hex Bar . D. 3 This test method specifies the use of air melted SAE 4340 steel (Grade A, see 7. Also known as: SAE AMS 3651 SAE MOBILUS. MIL-S-5000, AMS-S-5000 (Both are canceled and superseded by AMS 6415) MIL-S-8844 299-947-055 Bell Helicopter SS 9702 Sikorsky DMS 1555 Boeing (Previously McDonnell. 00. 2000 Series 3000 Series 4000 Series 5000 Series 6000 Series DTL Series. 4340 VAR AMS 6414 is a low alloy Chromium-Nickel-Molybdenum steel capable of being heat treated to high strength levels. 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. mil-a-1058 . 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. , This specification covers electric furnace steel bars and reforging stock of aircraft quality. 5MO (316), SOLUTION HEAT TREATED from SAI Global. 000 HEX. 0. 1 316 Various Bar, Wire, Forgings QQ-S-763 AMS-QQ-S-763 Should not be specified for new design. 43C) Buy SAE AMS S 6090 : 2006 STEEL CARBURIZING AND NITRIDING, PROCESSES FOR from SAI Global. 17-22a: uns k14675 specs: ams-6304, ams-6305 17-22a(s) uns k23015 specs: ams-6302 4130: uns g41300 specs: ams-6345, ams-6348, ams-6350, ams-6370, ams-s-6758, atm-a-322, mil-s-18729 4140: uns g41400 specs: ams-6382, ams-s-5626 4330 mod vac melt: uns k23080 specs: ams-6411, ams-6427, bms-7-122, bms-7-27, gm-1010,. 284 lb/in³, a thermal conductivity of 24 Btu/ (hr/ft²/°F), and a specific heat of 0. Many contracts still call out MIL-T-9047 and AMS. Sulfuric Acid Anodizing. ”. SAE AMS-S-6090. AMS-S-5000; AMS-S-6758; Other Military Grade Alloys & Steels; View All Alloys & Metals by Grade. 65 0. Read less…. 56C (SAE 1050) AMS5085 – available for purchase at $40. mil-a-8576-s/s by sae-ams-a-8576 mil-a-8623-s/s by mmm-a-134 mil-a-9117. Specification Supersedence : Table I lists process standards and specifications that have been superseded by military, federal, industry, and the Boeing Company. c. Status. All Grades. Revision Level. 25Mo (0. Alloy Steel MIL-S-83030 . Alloy Steel AMS 6411 . Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock. 0000. Find the right standards and certifications for your needs with SAE. 6al/4v Alpha/Beta Titanium Alloy. 00. How to Order; Standards We Provide; Updating, Reporting, Audits. Prior to that date, processors may perform shot peening in accordance with AMS-S-13165 or AMS 2430. How to Order; Standards We Provide; Updating, Reporting, Audits. 4330M Alloy Steel. 36% to 0. February 1998 and replaced by AMS-S-13165. AMS 5646 Bars / wire / forging. Talk To Us About the Alloys You Need Most. mil-a-8576-s/s by sae-ams-a-8576 mil-a-8623-s/s by mmm-a-134 mil-a-9117. superseded a superseded standard is one,. Alloy, Seamless. AMS6361G. Applications: Aircraft Landing Gear:ÐÏ à¡± á> þÿ ã þÿÿÿ d å f ç h é j ë l. Page Count. Description / Abstract: SAE AMS-QQ-P-35, Revision A, February 2005 - Passivation Treatments for Corrosion-Resistant Steel. AMS 6265 Alloy Steel. 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]. November 1, 2010. Steel Rings. Customers calling us for 4340 plate a lot of times are. Superseded. 3) in accordance with this standard. AMS-S-6758. Aeronautical Design Standard (ADS) Documents. AMS5085. May 1, 2009. Alloy 302. 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). DISCLAIMER: The use of this information should be considered strictly voluntary. A-286 Stainless Steel. Sealing compound, temperature-resistant, integral fuel tanks and fuel cell cavities, high-adhesion (superseded by SAE AMS-S-8802). 455 Stainless Steel. Tensile strength. 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. REVISION D. We carry, process and forge AMS 5604 Specification 17-4PH Stainless Steel. 50: si: stk:. 625, . Use our Rapid Response RFQ to request a quote. HP9-4-20 High Strength Alloy Steel. HP9-4-30 High Strength Alloy Steel. 4401 ws 1. astm-d2564. AMS 5512 Sheet / strip / plate (steel, corrosion and heat resistant, sheet, strip and plate 18Cr 10. 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. 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. 25 1. Classes 202, 302, and 305: When sensitization cannot be tolerated classes 202, 302 and 305 are not recommended for use. AMS 6931 6al/4v Titanium Alloy. Effective January 1, 2009, the requirements of the latest issue of AMS 2430 shall be fulfilled whenever reference is made to the cancelled AMS-S-13165. mil-a-5540. 4340 steel is produced by the consumable electrode vacuum arc. 400 Series Stainless Steel. Description / Abstract: MIL-S-5000, Revision E, November 12, 1982 - STEEL, CHROME-NICKEL-MOLYODENUM (4340) BARS, AND FORGING STOCK. 50, 1. 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]. 40ti (321), solution heat treated from sai global. 25Mo (0. The military paid to have its old specs hosted by commercial standard companies so we can claim we use commercial standards. . Historical. AMS Specifications; SPEC Description UNS Number Alloy Quote Request; AMS 2241: Tolerances Heat Resistant Bars: RFQ:. Country: USA: Britain: Britain: Japan: Standard: ASTM A29: EN 10250: BS 970: JIS G4103: Grades: 4340:. 15 0. The alloy’s melting point stands at approximately 2,800°F, and its coefficient of thermal expansion is 6. Steel Extrusions. We are a pre-eminent alloy steel distributor who has proudly serviced the needs for over 30 years as metal and alloy suppliers to the world’s major Aerospace and Aero-Engine Manufacturers. 0 [cad] ams5688 cad lac 0491 s/f lube mil-prf-46010h. l), ASTM-A295 AMS 6304 ASTM F1537 titanium. K, France, Singapore, and Shanghai. 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. Previous Next GRADES COVERED BY MIL-S-7720 302. AMS 6415: 3 - Design Control Reference: 1 - Incomplete Part Number: SOCIETY OF AUTOMOTIVE ENGINEERS INC 81343 ; AMS-S-5000: 5 - Replaced / Discontinued: 9 - No Longer Used: SOCIETY OF AUTOMOTIVE ENGINEERS INC 81343 ; MIL-S-5000: 5 - Replaced / Discontinued: 9 - No Longer Used: MILITARY SPECIFICATIONS 81349AMS 5515, AMS 5516, MIL-S-5059. 4340 RD BAR COND C 2. titanium. com . AMSS5000A. 80Cr - 1. STEEL BARS AND FORGINGS, 5. , This specification presents requirements for the carburizing and nitriding of carbon and allow steels to produce the mechanical properties specified by drawings, detail specifications,. 000 HEX - 74978. The alloy’s melting point stands at approximately 2,800°F, and its coefficient of thermal expansion is 6. This specification is superseded by a series of individual specifications covering specific forms of this material. Related Topics: Aluminum alloys. Skip to content - Show main menu navigation below - Close main menu navigation below. AMS-S-5000 Steel, Chrome-Nickel-Molybdenum (E4340) Bars & Reforging Stock Document Center. MIL-S-18729 Military (Department of Defense) Specification MilSpec 4130 Alloy Steel. sae ams s 6090 : 2006 : steel carburizing and nitriding, processes for: sae as 5944 : 1999 :Buy MIL-S-5000 Revision E:1982 STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS AND REFORGING STOCK from SAI GlobalDescription: 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. 43 0. of MIL-S ( steel)MIL-S-5000E-4340 AEROSPACE. 3. I recommend you purchase the AMS for your quotation. 4130 Alloy Steel. )ULTRASONIC INSPECTION, THIN WALL METAL TUBING. Specifications: AMS 6359, AMS 6409, AMS 6414, AMS 6415, AMS 6454, ASTM A29, ASTM A322, ASTM A331, ASTM A506,ASTM A519, ASTM A646, ASTM A752, ASTM A829, MIL-S-5000, UNS G43400 . 2301, ASTM. 12, 1982. 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. SAE AMS S 6090 : 2006 : STEEL CARBURIZING AND NITRIDING, PROCESSES FOR: MIL-B-9946 Revision E:1987 : BIT, SCREWDRIVER, GENERAL SPECIFICATION FOR:4340 Alloy Steel. 00, 1. 85g/cm³ and a melting point of 1450°C. 6 Peening intensity: Unless otherwise specified on the drawing or in the contract, the. 3 ConditionAMS-6532 Aermet 100 AMS-77184750 (Exc. 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. . Product availability:AMS2750F has been released for approximately 7 months now. Revision Level. 4340 Alloy Steel. (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. superseded a superseded standard is one,. 4441 ws 1. Rationale: AMS5517M revises Composition analysis standards (3. Related Topics: Manufacturing processes. 6Zn 2. SPECIFICATIONS: AISI4340, ASTM A 829 / A6 SAE J404, AMS 2252/ 2301/6359 SAE J404. All Grades. AMS S 8802 type 1 is a dichromate cured sealant. 43%, manganese ranges from 0. Alternate References are: 005558374,9510005558374,00-555-8374,AMS 6415,AMS-S-5000,MILS5000,AMS6415,AMS-S-5000,MILS5000MIL-S-6090 › Steels Used in Aircraft Carburizing and Nitriding, Process for (Superseded by SAE AMS-S-6090) MIL-S-6090 - REV A CANCELLATION 3 - CANCELLED -- See the following: AMS-S-6090 Show Complete Document History. How to Order; Standards We Provide; Updating, Reporting, Audits;. Enter code: Categories 300M & 4340M Alloy Steel, Alloy Steel, DMS, Grades, McDonnell Douglas Specifications, Specifications. , This specification covers electric furnace steel bars and reforging stock of aircraft quality. , 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. 08 V. 4340 E4 MILS-5000 1. MIL-S-7420, AMS-6440, AMS-2301, AMS-6440, AMS-6444. Our service centers are located throughout the U. Superseded. 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. Buy SAE AMS S 5000 : 2007 STEEL, CHROME-NICKEL-MOLYBDENUM (E4340) BARS AND REFORGING STOCK from SAI GlobalMIL S. Death Sandringham House in Norfolk, where the King died. Also known as: SAE AMSS 5000 SAE MOBILUS. 38 - 0. Superseded. 347 / 347H. MIL-S-6758 Specification 4130 Alloy Steel (AMS Spec here) Steel Bars. 95 Cr, 0. 38-0. This specification covers electric furnace steel bars and reforging stock of aircraft quality. Please enable JavaScript to view the page content. This change spawned a great deal of controversy in the heat treating industry which continues to this day. AMS 6414 Alloy Steel. 4340 E4 MILS-5000 1. 75, 2. LBS/FT:. 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. 10 . Revision Level. Explore our McDonnell Douglas Specifications product category. Superseded By: SAE AMS4115 Document Language: English Published By: SAE International (SAE) Page Count: 6 ANSI Approved: No DoD Adopted: No Document History:. AMS-S-5000. Titanium alloys. current specification revisions revision 122022. Publication Date. 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,. AMS-S-13165 was made redundant by AMS 2430 and AMS 2432. 15/. Buy SAE AMS 5085 : 2017 STEEL SHEET, STRIP, AND PLATE, 0. Aug. We carry, process and forge AMS 5621 Specification 420 Stainless Steel. 2) and the requirements for furnace equipment, test procedures and information for heat-treating. Titanium. Claudia's Notes: Originally, the AMS-QQ-P-35 was just a reprint of the QQ-P-35C. 69 in addtion to MIL-C-5056:. 60 . 3. Buy SAE AS 6279B : 2019, the superseded version of standard practice for production, distribution & procurement of metal stock for AMS, from SAE International. Status: Withdrawn. 38 - 0. March 1, 2007. 15. 25, 2. Also known as: SAE AMS 56854340 VAC-ARC steel is a low alloy, nickel-chromium-molybdenum steel capable of being heat treated to high strength levels. Status. 11 Btu/ (lb/°F). 0000 x 144. The specifications for this alloy include AMS 6414, AMS 6409, AMS 6415, AMS 6484, AMS-S-5000, DMS 1555 Gr A, BMS 7-28, BPS 299-947-055, SS 9702, PWA LCS F-17, MIL-S-8844 CL1, and MIL-S-5000. AMS-S-5000 Specification 4340 High Tensile Steel (MilSpec here) Steel Bars. 2) and the requirements for furnace equipment, test procedures and information for heat-treating procedures, heat-treating. 82 Cr, 1. 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 :. HP9-4-20 High Strength Alloy Steel. This specification covers the requirements for heat-treatment of four classes of steel (See 1. Availability. This blog. 4340 Alloy Steel. 010 0. For our AISI 4130 (E4130) aircraft quality steel products please visit. Talk To Us About the Alloys You Need Most. 11 Btu/ (lb/°F). The hardenability and weldability of Alloy 4130 are considered equivalent to 8630 (MIL-S-6250) . AMS 6414 Alloy Steel. Document Number. SAE-AMS-H-6088, WITHDRAWAL OF ADOPTION NOTICE: HEAT TREATMENT OF ALUMINUM ALLOYS (27-JAN-2010) [SUPERSEDES MIL-H-6088H] [NO S/S DOCUMENT]. Vacuum induction and consumable. 2μm/m °C and a thermal conductivity of 14W/m°C. Status. Eredhel Quality Manager. 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. 7004 State Route 123 Franklin, OH 45005 . Vanadium Valve K15047 A‐232 6150 J132 10270‐2 G3561 2803 SWOCV‐V 735A50 HD Inconel 600 N06600 B‐166 5687 3075/3076 NA14 Inconel X750 N07750 B‐637 5698/5699 Notes:superseded a superseded standard is one,. Superseded. 4130 Alloy Steel, Alloy Steel, DMS, Grades, McDonnell Douglas Specifications, Specifications. 40. 01/714323 DC : DRAFT OCT 2001. mil-a-3316 mil-a-3920. Find the right standards and certifications for your needs with SAE. 6. No. 749mm) to 7. mil-a-5540. QQ-P-35, Type VI: AMS 2700, Method 1, Type 6. REV A AMENDMENT 2. C Si Mn P S Cr Mo Ni Cu Cu Min 0. Pages: 7. HARD COAT (S/S BY AMS 2469)4340 Alloy Steel. Alloy 4140 is the most widely used alloy for oil patch applications. AMS 5637, QQS-763, MIL-S-7720. si ni cr mo cu max. Popular Metal Specs. MIL-S-8784. 12, 1967. Type 321's general corrosion is less than Type 302 . 1 Al. 13-8MO Stainless Steel in AMS 5629 Specification, per SAE International: “This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, flash welded rings, extrusions, and stock for forging, flash welded rings, or extrusion. 5NI - 0. View DetailsCalifornia Metal & Supply, Inc. 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;. . Metallurgy and specifications. MIL-S-6758 › Steel, Chrome-Molybdenum (4130) Bars and Reforging Stock (Aircraft Quality) (Superseded by SAE AMS-S-6758) MIL-S-6758 - REV B CANCELLATION 1 - CANCELLED -- See the following: AMS-S-6758 Show Complete Document History. Pages: 13. 4130 Alloy Steel. Although I don't know for certain, it's very likely that the AMS has diverged from the MIL. All of our alloys steels are fully certified by United States producing mills and are shipped with original mill test reports. SAE AMS 6484 and SAE AMS S 5000. SAE AMS 6415 : 2016. mil-a-13881 mil-a-13883 mil-a-21366 mil-a-22010-s/s by astm-d2564 mil-a-22895 mil-a-23941. Use our Rapid Response RFQ to request a quote. mil-s-5000 mil-s-8844. Steel Tubing. Related Topics: Test procedures. 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. superseded by ams 2700) a ams-qq-p-416 f astm e1417/e1417m 21 mil-a-8625 (superseded by. 1. A-286 Stainless Steel. AMS-S-5000 - BASE - SUPERSEDED -- See the following: AMS-6415 AMS-6484 Show Complete Document History. 1. Please enable JavaScript to view the page content. mil-a-1058 . One of the most versatile stainless steel alloys is AMS-S-5000. AMSS6090A. The Royal Roads University campus sprawls over 260 hectares of lush parkland, where you will find walking, hiking, and biking trails, magnificent examples of. 📝 Amendments Available. 8 Ni, 0. 750"dia: 72. 3V AMS5735 – available for purchase at $48. 38-0. Hydraulic…SAE AMS S 13165 : 1997. MIL-S-6758. Document History. 4340 Alloy Steel. AMS-2769 Rev C Heat Treatment of Parts in Vacuum (07-12-19) AMS-2770 Rev P Heat Treatment of Wrought Aluminum Alloy Parts (04-08-19) ARP-1962 Rev B Training and Approval of Heat Treating. 1 for sufficient time to produce the specified depth of case. We now reference and conform to AMS 2430 and AMS 2432. December, 2007, and has been superseded by AMS 2430, Shot Peening. 2 Classification: Material shall be. forgings: ams 6414 ams 6415 astm a646. E-52100, 52100. 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. 2002-11-21. 500 x 36 x 96: 144. 20Mo (0. Alternate References are: 009935760,9510009935760,00-993-5760,AMS 2806,AMS-S-5000,MIL-S-5000,AMS2806,AMS-S-5000,MIL-S-5000AMS-5000 for the Beechjet 400A Ref. 25 Mo, 0. 5000 Series Aluminum Sheet; 6000 Series Aluminum Sheet; 7000 Series Aluminum Sheet; Aluminum Checker / Tread / Diamond Plate; Aluminum Wire. 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. We carry, process and forge MISC Specification MTL-1201 Grade 300M / 4340M Alloy Steel. MIL S-5000: AMS 6409 Specifications. 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. AMS 6414 Alloy Steel. March 3, 2010. As aviation enthusiasts we are pleased to serve all of your aircraft alloy needs. Heat treatment. , Canada, Mexico, U. 5000 ht: 15-5ph ams5862 plate cond h1150: 136. 006B - 0. 40-0. The carbon content ranges from 0. The furnace or retort should be purged with inert gas before opening. Superseded date: 04-11-2012. Tensile strength. 80 S150 – – – MSRR 6591/2/5/6/7, 6603/31, 6902/19,Superseded by AWS D17. To those users, I hope to provide a 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 HARD COAT (S/S BY AMS 2469). QUALITY MANAGEMENT SYSTEMS - REQUIREMENTS FOR AVIATION, SPACE AND DEFENSE DISTRIBUTORS. The high fatigue strength makes E4340 ideal for highly stress parts as it maintains it's strength and hardness at elevated temperatures. 9510-00-993-5760, BAR,METAL. Defense industry. 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. ¼ Hard MIL-S-5059 AMS 5907 MMPDS Section 2. 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. Publication Date. It has a density of 0. AMS 5558 Welded /thin wall tube. Document Number. The electrical resistivity of AMS-S-5000 is 7. Report Problem (email) Status: Cancelled. E Notice 2 - Notice of cancellation/superseded by. 5000: 15-5ph ams5862 . CAUTION: The supersession information is valid as of the date of this notice and may be superseded by subsequent revisions of the superseding document. Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock. SAE AMS 6415 : 2016. SCOPE: 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 &. 4. Coatings, colorants, and finishes. ams 6351 astm a505 mil-s-18729. 23Cr (7075-T6) (7075-T651)Solution and Precipitation Heat Treated ASTM B209. 4330M Alloy Steel. 4427 ws 1. link] was cancelled and superseded by AMS2700 [affil link], which has a class 4 which is. 5, 1973. Effective January 1, 2009, the requirements of the latest issue of AMS 2430 shall be fulfilled whenever reference is made to the cancelled. Tensile strength.