SCOPE: 1. Publication Date. , This specification covers premium quality, multiple vacuum melted, low alloy steel bars, reforging stock, and mechanical tubing intended for use at. Document Number. 43C) Buy SAE AMS S 6090 : 2006 STEEL CARBURIZING AND NITRIDING, PROCESSES FOR from SAI Global. FSC Code: 9510 - Bars and Rods, Iron and Steel. All Grades. 8. Use our Rapid Response RFQ. This specification covers the requirements for heat-treatment of four classes of steel (See 1. AMS-S-6758 has excellent physical properties. 750, . AMS 6414 Alloy Steel. AMS-S-5000 - ADOPT WITHDRAWN - SUPERSEDED -- See the following: AMS-6415 AMS-6484 Show Complete Document History. 5Mg 0. 60 . 5MO (316), SOLUTION HEAT TREATED from SAI Global. Publication Date. AMS-S-5000 - BASE - SUPERSEDED -- See the following:. 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]. 6 - 5005: 5052. Created Date: 8/24/2022 10:15:41 AMBuy SAE AMS 2485 : 2016 COATING, BLACK OXIDE from SAI Global. Trace-ability is everything in the aviation industry and when you become an aviation client of ours you can rest assured that you are purchasing quality material to. Minimum Mechanical Properties required property by ASTM A240 and ASME SA 240. Document History. Changed AMS I-6875 to AMS-H-6875. 1) per SAE AMS 6414, and both are heat treated to 260 to 280 ksi (pounds per square inch ×1000). MIL-S-7420, AMS-6440, AMS-2301, AMS-6440, AMS-6444. Talk To Us About the Alloys You Need Most. redstone. 3. 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. Different grades of steel are achieved by adding other alloying elements, such as manganese, nickel, chromium, titanium and molybdenum to the basic mix. DOD ADOPTION. AMS S 8802 standardizes the specifications for temperature-resistant, two-component synthetic rubber compounds of the polysulfide type. Grinding of Chromium Plate - Landing gear parts 275 KSI or above. 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. Rationale: AMS5517M revises Composition analysis standards (3. Electroless Nickel Plating per MIL-C-26074, ASTM B733 and AMS 2404. This product is not available online at this time. became AMS-F 7190). Issuing Committee: AMS E Carbon and Low Alloy Steels Committee Publisher: SAE International. Rockwell Collins is offering a dual AMS-5000 system a two-year warranty and will replace or update required line replaceable units (LRUs). DMS 2284. 15/. This product is not available online at this time. , This specification presents requirements for the carburizing and nitriding of carbon and allow steels to produce the mechanical properties specified by drawings, detail specifications,. AMS 6931 6al/4v Titanium Alloy. For detailed information and chemical analysis please visit the 4340 (E4340) steel page. , Canada, Mexico, U. 33 . Customers calling us for 4340 plate a lot of times are frustrated with on-time. BMS-7-26 Boeing Spec Alloy Steel. AMS 5516. Buy SAE AMS 2175 : 2010 - non-destructive testing methods, sampling frequency, & acceptance criteria for the inspection of metal castings from SAE International. 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]. 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. Test procedures. It is not a coating and does not change any part’s dimensions. D. Status. AMS 5637, QQS-763, MIL-S-7720. The electroless nickel plating process occurs from a chemical reduction of the nickel ions within the electroless nickel solution onto. Showing 1 to 25 of 88 entries. Theams 6257 / ams 6419 ams 6417 / bs s155 gm 1012-3 mil-s-qq-8844(class 3) 5: 4340: 10≦Φ≦454: g43400: ams 6409 / ams 6414 ams 6415 / bms 7-28 ams-s-5000 mil-s-8844(class 1) 6: 4330m: 10≦Φ≦454: k23080: ams 6411 / ams 6427 bms 7-122 / bms 7-27 be 0886 / ce 0906 gm 1010: 7: 9310: 10≦Φ≦454: g93106: ams 6265 ams 6260: 8: 4130:. MIL-STD-2175A, MILITARY STANDARD: CASTINGS, CLASSIFICATION AND INSPECTION OF (25 AUG 1993) [S/S BY SAE-AMS-STD-2175]. Alloy Steel. mil-a-1058 . 284 lb/in³, a thermal conductivity of 24 Btu/ (hr/ft²/°F), and a specific heat of 0. si ni cr mo cu max. Page Count. MIL-T-9047G Amendment 2 was cancelled, and superseded by SAE (Society of Automotive Engineers). Buy SAE AMS S 5000 : 2007 STEEL, CHROME-NICKEL-MOLYBDENUM (E4340) BARS AND. T. STEEL BARS AND FORGINGS, 5. This specification covers a carbon steel in the form of sheet, strip, and plate. Condition A AMS 5648 Not in MMPDS. 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. 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,. 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. Alloy E 4340 is a widely used deep-hardening constructional steel. MIL-S-6758 MilSpec Military Grade Alloy Steel. AMS2750F is typically communicated via industry standards such as SAE/AMS specifications as well as customer purchase orders and part prints. 3) in accordance with this standard. 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,. Heat treatment. AMS 6265 Alloy Steel. AMS 4045 7075 Aluminum Alloy, Aluminum Sheets and Aluminum Alloy Plate 5. 5. Description / Abstract: MIL-S-5000, Revision E, November 12, 1982 - STEEL, CHROME-NICKEL-MOLYODENUM (4340) BARS, AND FORGING STOCK. Steel, Chrome-Nickel-Molybdenum (E4340) Bars & Reforging Stock. 12, 1967. Nickel L-605 . MIL-S-5000. HARD COAT (S/S BY AMS 2469)4340 Alloy Steel. Metals. Noncurrent. 4CU - 1. Type 321's general corrosion is less than Type 302 . The plate and sheet covered by this specification shall be an integral composite product consisting of a heat-treatable aluminum alloy 2024 core with thin layers of an aluminum alloy 1230 (99. 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. A. 1. 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). 75, 2. 0000 x 144. STEEL, CORROSION AND HEAT RESISTANT 15Cr - 26Ni - 1. 48 - 0. Issuing Committee: AMS E Carbon and Low Alloy Steels Committee Publisher: SAE International. AMS 6265 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. 50: si: stk:. 60Mn (2024-T3) (2024-T351) Solution Heat Treated QQ-A-250/4. MIL-H-5606 petroleum base hydraulic fluid for military aircraft (inactive for new designs. The alloy has a good combination of ductility, toughness and strength along with high hardenability and better depth of hardening than chrome-moly 4140 type alloys. 12, 1982. 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. 455 Stainless Steel. Pages: 13. 2738 FAX: 210. AMS 6414 sheet is an alloy steel that consists of carbon, manganese, chromium, molybdenum, vanadium, and nickel. MIL-S-46033 - STEEL BARS, CARBON and ALLOY, ROUND, SQUARE, and FLAT (FOR SPRINGS) (Use ASTM-A29/A29M) MIL-S-46042 - Steel, Corrosion and Heat Resistant Bar and Forgings (No Superseding Document) MIL-S-46047 - Steel, Bars and Blanks (1-3/4 Inches and over in Diameter) for Barrels of Small Arms Weapons. DMS 2257. Type 2 is fine for any grade that type 6 or 7 would be used on. 000 HEX. 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. Alloy Steel AMS 6267 . Differences from AMS-H-6875 are a consequence of removing. 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. 5000 - Magnesium - moderate to high strength, resistant to corrosion, used in marine environments. 8Ni - 0. SAE AMS-H-6875. AMS-S-6758 has excellent physical properties. Historical Revision Information. AMS 6414 Alloy Steel. March 1, 2007. Type 321 is a chromium-nickel stainless steel and with the addition of titanium, type 321 is resistant to intergranular corrosion. Effective January 1, 2009, the requirements of the latest issue of AMS 2430 shall be fulfilled whenever reference is made to the cancelled. Please enable JavaScript to view the page content. 56C (SAE 1050) AMS5085 – available for purchase at $40. The displayed colour will depend on your monitor and browser and pearl or metallic colours. Condition A AMS 5648 Not in MMPDS. Pricing based on. 43%, manganese ranges from 0. 13 AMS2770, AMS2771, and AMS2772 replaces AMS-H-6088. 11 Btu/ (lb/°F). July 1,. AMS 6931 6al/4v Titanium Alloy. 649. It has a density of 0. The furnace or retort should be purged with inert gas before opening. AMS-S-5000. Status. 4340 RD BAR COND C 2. Aero-Vac Alloys & Forge is the metal buyer's trusted resource!scope: This specification establishes general requirements for the processes listed in 3. mil-a-5090-s/s by mmm-a-132 mil-a-5092-s/s by mmm-a-1617. MIL-S-40046D (NOTICE 1), MILITARY SPECIFICATION: SLING, FLAGSTAFF (08-JAN-1999) MIL-S-9479C (NOTICE-1), MILITARY SPECIFICATION: SEAT SYSTEM, UPWARD. , Da-Kang Village, Kuei-Sun, Taoyuan County. 1 pageMIL-A-8625 Aluminum Anodic Coatings MIL-A-8625 is the military specification for Anodic Coatings for Aluminum and Aluminum Alloys. K, France, Singapore, and Shanghai. Perry, was at the forefront of military specification reform. View superseded by. d2-5000 psd: 9-1, 9-3 d6-5000 br d8-5000 p d8-5000 psd: 8-57 dms1786 p dms1786 030-mc dms2433 b. How to Order; Standards We Provide; Updating, Reporting, Audits. 2. Nearly all of our 4130 bars are produced as “Cold Finished Normalized,” which is also known as “Condition D4”. QQ-P-35 was superseded by AMS-QQ-P-35 for aerospace products and AMSQQP35 [canceled, affil. BMS-7-26 Boeing Spec Alloy Steel. 4130 Alloy Steel in AMS-S-6758 per SAE International: “This specification covers chrome-molybdenum (4130) steel bars and forging stock of. E. Pages: 3. This alloy is known for its excellent mechanical properties, corrosion, and heat resistance. Simple online access to standards, technical information and regulations. MIL-S-6758 MilSpec Military Grade Alloy Steel. SAE International. , This specification covers electric furnace steel bars and reforging stock of aircraft quality. 0000 x 144. forging: ams 6382 astm a 646. Manufacturing processes. 4340 E4 MILS-5000 1. american aircraft quality alloy steel bar-analysis cmnpmax. SPECIFICATIONS: Avion Alloys services Blue Chip customers worldwide with prime top-quality metals like AH 36 bars procured exclusively from United States Mills. Noncurrent. sae ams-s-5000a-2007 (sae ams-s-5000a-2007) Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock (Cancelled: Mar 2007) This specification covers. 80Cr. Having a lower carbon content improves weldability. Tensile strength. Feb. This specification is applicable only to the heat treatment of raw material. 65 3. Steel covered by this specification is intended for use in the manufacture of highly stressed aircraft parts requiring high hardenability. Alloy, Seamless. 1, 3. 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. HP9-4-20 High Strength Alloy Steel. The high fatigue strength makes E4340 ideal for highly stress parts as it maintains it's strength and hardness at elevated temperatures. 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. 1 pageFAX. 9510-00-580-5486, BAR,METAL. E4340, AMS. MIL-S-5000E (NOTICE 1), MILITARY SPECIFICATION: STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS, AND FORGING STOCK (27 SEP 1995) [S/S BY SAE. HP9-4-20 High Strength Alloy Steel. AMS-S-5000. 1 MIL-H-81200 replaced by AMS-H-81200. 32 KB. REV E CANCELLATION 1. In the early 1990’s, US Secretary of Defense, William J. 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 . AMS-S-5000. 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. When Enhanced Care comes into effect. All Grades. 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. qq-w-423 cond b form 1 superseded by astm-a313: 12,540. Eredhel Quality Manager. 187" (4. Related Topics: Manufacturing processes. (Copies of this document are available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001. MIL-S-5000 - Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock (Superseded by SAE AMS-S-5000) MIL-S-5626 - Steel, Chrome-Molybdenum (4140). MIL-S-5000E, MILITARY SPECIFICATION: STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS, AND FORGING STOCK (12-NOV-1982) [S/S BY SAE-AMS-S-5000]. SAE revised the scope of paragraph 1. 25 Mo, 0. Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock AMSS5000. 2. Aluminum. AMS-S-13165. 69 in addtion to MIL-C-5056: S391: PS18021: DFL:. Status. 4340 High Tensile Steel in AMSS5000 Specification, per SAE International: “This specification. Publication Date. ”. 595A colour chart. Talk To Us About the Alloys You Need Most. Carbon. 3Mo - 1. 3V AMS5735 – available for purchase at $48. (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. 13 Cr, 8. Explore our McDonnell Douglas Specifications product category. 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. link] was cancelled and superseded by AMS2700 [affil link], which has a class 4 which is. Use our Rapid Response RFQ to request a quote. ¼ Hard MIL-S-5059 AMS 5907 MMPDS Section 2. 8 Ni, 0. Various Bar / Wire/ Forgings QQ-S-763 AMS-QQ-S-763 Should not be. Publication Date. 5000 ht: 15-5ph ams5862 plate cond h1150: 136. November 1, 2010. 1. Steel Tubing. 2) and the requirements for furnace equipment, test procedures and information for heat-treating procedures, heat-treating temperatures and material (See 6. Titanium alloys. 6al/4v Alpha/Beta Titanium Alloy. 38-0. Document Number. 4×10⁷ Ωm, making it a great electrical conductor. Superseded date: 04-11-2012. AMS 6265 Alloy Steel. 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. 1. Email：hanjustdoit@gmtc. 5NI - 0. AMS-S-5000 has a density of 7. Superseded By. 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. Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard. 82 Cr, 1. AMS 5512 Sheet / strip / plate (steel, corrosion and heat resistant, sheet, strip and plate 18Cr 10. PETROLEUM AND NATURAL GAS INDUSTRIES - DRILLING AND PRODUCTION EQUIPMENT - DRILL-THROUGH EQUIPMENT. , This specification covers electric furnace steel bars and reforging stock of aircraft quality. tube/pipe: ams 6361 ams 6362 ams 63711. May 1, 2009. 00%, and the remaining elements comprise the rest of AMS 6414’s composition. 4340 Alloy Steel. Test procedures. Alloy E 4340 is a widely used deep-hardening constructional steel. AMS 6931 6al/4v Titanium Alloy. Steel Rings. The balance of these elements makes AMS 6414 a high. 2% offset 1000 psi (MPa) 30 (207) min Elongation % 35% min Hardness. Call us. Buy SAE AMS 5853 : 2012 STEEL, CORROSION AND HEAT-RESISTANT, BARS AND WIRE, 15CR - 25. This Standard has been added successfully to your. 5CR - 10. Use our Rapid RFQ to request a quote. AMS 6414 Alloy Steel. 93 - 1. superseded by ams 2700) a ams-qq-p-416 g astm 2021, e1 . Status. Buy SAE AMS 5085 : 2017 STEEL SHEET, STRIP, AND PLATE, 0. 5, 1973. May 1, 1999 Sealing Compound, Temperature Resistant, Integral Fuel Tanks and Fuel Cell Cavities, High Adhesion ams-s-8802. 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 . Coatings, colorants, and finishes. 304/L Specifications AMS 5565 ( AMS-T-8506 canceled, supersedes MIL-T-8506) AMS 5567 (supersedes MIL-T-8504) Material Type & UNS# 304, 304L / S30400, S30403 Modulus of Elasticity 106 psi (GPa) 29 (200) Tensile Strength 1000 psi (MPa) 100 (689) max Yield Strength 0. Various Bar / Wire/ Forgings QQ-S-763 AMS-QQ-S-763 Should not be specified for AMS S 8802 standardizes the specifications for temperature-resistant, two-component synthetic rubber compounds of the polysulfide type. K, France, Singapore, and Shanghai. 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. 9510-00-505-7354, BAR,METAL. Test procedures. Document Number. 35 . This alloy has a coefficient of thermal expansion of 17. BAC 5019. 0. 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. 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. 25Mo (0. Dec. Classes 202 and 302: Class 302 is intended for use where severe corrosion is. A-286; 13-8MO; 15-5PH; 17-4PH; 316; 321; 400; 455; 300M/4340M;. 1. Aluminum alloys. LAMINATED SHEET. 95Cr - 0. AMS-S-5000 Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock 2. 27, 1995. . Alloy 4140 (AISI 4140) is a low alloy steel containing Chromium and Molybdenum. Revision A, March 2007. Alloy Steel AMS 6409 . No. AMS-C-27725 Grove, OK Boeing: Etch - Cres AMS-C-81769 Grove, OK: Boeing Passivation: AMS-QQ-P-35 Grove, OK Boeing: Shot Peen AMS-S-13165 Grove, OK: Boeing Passivation: ASTM A380/A380M / AMS QQ-P-35 A Grove, OK Boeing: Salt Spray Testing ASTM B117 Grove, OK: Boeing Penetrant Inspection: ASTM-E-1417 Grove, OK. 50, 1. 0. 9510-00-993-5760, BAR,METAL. Enter code: Category Controls & Processes. Pages: 5. Alternate References are: 005805486,9510005805486,00-580-5486,SAE AMS 6415,AMS-S-5000,MIL-S-5000,SAEAMS6415,MIL-S-5000,AMS-S-5000GOLDEN WIN STEEL INDUSTRIAL CORP. It is recommended that preheating or. 4130 Alloy Steel. , This specification covers the requirements for heat-treatment of four classes of steel (see 1. 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. Document History. Related Topics: Test procedures. Round Bar, Flat Bar, Plate. Qualified to SAE-AS81820 BODY BALL RACEDocument Number. current specification revisions revision 122022. 25, 2. For detailed information and chemical analysis please visit the 4340 (E4340) steel page. MIL-S-5000 | Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock (Superseded by SAE AMS-S-5000) | Document Center, Inc. 4. 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. Nov. How to Order; Standards We Provide; Updating, Reporting, Audits. All Grades. Pages: 22. of MIL-S ( steel)MIL-S-5000E-4340 AEROSPACE. 1 316 Various Bar, Wire, Forgings QQ-S-763 AMS-QQ-S-763 Should not be specified for new design. Scope: This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. BMS-7-26 Boeing Spec Alloy Steel. This specification covers the requirements for heat-treatment of four classes of steel (See 1. 6. AMS 6931 6al/4v Titanium Alloy. 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. HP9-4-30 High Strength Alloy Steel. 40ti (321), solution heat treated from sai global. Titanium alloys. E Notice 1 - Notice of cancellation/superseded by SAE AMS 6415. 4330M Alloy Steel. Tensile strength. AMS 6931 6al/4v Titanium Alloy. Hydraulic…SAE AMS S 13165 : 1997. HP9-4-30 High Strength Alloy Steel. Standard Digital Reference Images for Inspection of Aluminum Castings. Publication Date. 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. Corrosion. 5000 Series Aluminum Sheet; 6000 Series Aluminum Sheet; 7000 Series Aluminum Sheet; Aluminum Checker / Tread / Diamond Plate; Aluminum Wire. E. STEEL PLATE, SHEET, AND STRIP, ALLOY, 4130, AIRCRAFT QUALITY (S/S BY SAE-AMS6350, SAE-AMS6351 OR SAE-AMS6345. com materials stocked Reliance Aerospace Solutions STAINLESS STEEL SPECIFICATIONS 13-8 PH AMS 5629, DMS 2100, STO160LB0013, ASTM-A-564 (XM-13)Specs: AISI. Steel Reforging Stock. 30 2. 1 Al. This is a standard used by the aerospace industry to describe and control the passivation of stainless steel. Cancelled. Heat treatment. Product availability:AMS2750F has been released for approximately 7 months now. HP9-4-20 High Strength Alloy Steel. Mo. Please request a quote below or head over to the general catalog by clicking the "Products" link in. 80Cr - 1. Inconel 625 ™ Super Alloy in Sheet, Strip and Plate. Manganese.