43 0. 3 ConditionAMS-6532 Aermet 100 AMS-77184750 (Exc. 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. Aluminum alloys. AMS 5604. 2 Timothy 1:7 . ”. ; For our AISI 4130 (E4130) aircraft quality steel products please visit the 4130 (E4130) steel section. Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard. 75% to 1. 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. Chrome Vanadium Com K15048 A‐231 6150 10270‐2 2803 735A50 HS OT Chr. MIL-S-5000 | Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock (Superseded by SAE AMS-S-5000) | Document Center, Inc. 13-8MO Stainless Steel in AMS 5629 Specification, per SAE International: “This specification covers a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. March 3, 2010. )ULTRASONIC INSPECTION, THIN WALL METAL TUBING. 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. View DetailsCalifornia Metal & Supply, Inc. 3. Victoria San Juan Cruises sails May through October between Bellingham,. SAE AMS-QQ-A-225/8 : Aluminum Alloy 6061, Bar, Rod, Wire, and Special Shapes; Rolled, Drawn, or Cold Finished. This product is not available online at this time. 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. SAE AMS-S-5000. Aug. STEEL BARS AND FORGINGS, 5. We carry, process and forge AMS 5604 Specification 17-4PH Stainless Steel. com . 10 pages SAE AMS 6485 : 1989. Document Number. 43 C. AMS 6414 Composition. Click here to view the AMS Std. 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G3561 2803 SWOCV‐V 735A50 HD Inconel 600 N06600 B‐166 5687 3075/3076 NA14 Inconel X750 N07750 B‐637 5698/5699 Notes:superseded a superseded standard is one,. Alloy Steel AMS 6304 (17-22A) Alloy Steel MIL-S-5000 . forgings: ams 6414 ams 6415 astm a646. MIL-S-5000. MIL-S-5000 Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock. Document History. Alloy 4140 is the most widely used alloy for oil patch applications. MIL S-5000 SAE J1397 (4340) SAE J404 (4340) SAE J412 (4340) UNS G43400: Chemistry Data. Aero-Vac Alloys & Forge is the metal buyer's trusted resource!scope: This specification establishes general requirements for the processes listed in 3. Steel covered by this specification is. astm-d2564. 1, 3. GENERAL SPECIFICATION GUIDE FOR MECHANICAL GEARED ROTARY ACTUATORS. 9 Mil 1984 10-49. 9510-00-993-5760, BAR,METAL. 75-110. Alloy 302. Specifications. July 1,. 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. Heat treatment. Call us. AMS 6265 Alloy Steel. 80Cr. ”. SAE AMS-S-7720. MIL-S-5000. MIL-T-9047 Military (Department of Defense) Specification MilSpec 6al/4v Alpha/Beta Titanium Alloy. AMS-S-13165A SAE AMS-S-13165A - 6 - 3. Chemicals. 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. George VI had undergone a lung operation in September 1951 from which he never fully recovered. טיטניום מפרטים: ams 4928, ams 6931, ams 4911, ams 4965, ams 6930, ams 4967, ams 4920, ams-t-9046, mil-t-9047, bms 7-269, dms 1570, dms 1592, ams 4907. Manganese. Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock. 455 Stainless Steel. AMS-7727 : Kovar® Rod : For God gave us a spirit not of fear but of power and love and self-control. 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. Rationale: AMS-S-5000A was issued to cancel and supersede AMS-S-5000 with current, technically equivalent specifications. si ni cr mo cu max. 316L Condition A Sheet, Strip, Plate QQ-S-766 AMS 5507 Not in MMPDS. 010 0. 302 stainless steel is available in Sheet, Strip, Plate, Angles, Bars (Round, Hexagon, Squares, Flats). 12, 1967. Chromium. Ask a question or request a quote. SAE AMS 6415 : 2016. QQ-S-763 Rev. 2738 FAX: 210. ALLOY ROD/BAR HEX 4340 AMS-S-5000 1. AMS 6931 6al/4v Titanium Alloy. Heat Treatment of Steel Raw Materials. 48 - 0. 1) per SAE AMS 6414, and both are heat treated to 260 to 280 ksi (pounds per square inch ×1000). MIL-S-13165C, MILITARY SPECIFICATION: SHOT PEENING OF METAL PARTS (07 JUN 1989) [S/S BY SAE-AMS-S-13165]. Differences from AMS-H-6875 are a consequence of removing. STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS, AND FORGING STOCK (S/S BY SAE-AMS6415P AND SAE-AMS-S-5000) (SUPERSEDING MIL-S-5000D) standard by Military Specifications and Standards, 11/12/1982. tw; Taipei Branch Office. Test procedures. Related Topics: Manufacturing processes. 1 MIL-H-81200 replaced by AMS-H-81200. 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. 60Mn (2024-T3) (2024-T351) Solution Heat Treated QQ-A-250/4. Title: Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock (S/S by SAE-AMS6415 and SAE-AMS6484) Scope: This specification covers electric furnace steel bars and reforging stock of aircraft quality. , constitutes a requirement to conform to the applicable provisions of the documents. 95Cr - 0. MIL-S-5000E (NOTICE 2), MILITARY SPECIFICATION: STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS, AND FORGING STOCK (11 AUG 2000) [S/S BY SAE. Related Topics: Coatings, colorants, and finishes. Our extensive product offerings include alloy, stainless, nickel, aluminum, titanium, carbon and cast iron. 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. Publication Date. 6. K, France, Singapore, and Shanghai. When Enhanced Care comes into effect. 2), deletes noise note in Table 6, and adds notes of explanation for Figure 12. Condition A AMS 5648 Not in MMPDS. Also known as: SAE AMSS 5000 SAE MOBILUS. ADOPT WITHDRAWN. Talk To Us About the Alloys You Need Most. 3MO - 0. Showing 1 to 25 of 88 entries. March 1, 2007. Type 321 is a chromium-nickel stainless steel and with the addition of titanium, type 321 is resistant to intergranular corrosion. 60MN (CLAD ONE SIDE 2024-O), ANNEALED from SAI Global. mil-a-3316 mil-a-3920. MIL-S-5000 | Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock (Superseded by SAE AMS-S-5000) | Document Center, Inc. Alloy, Seamless. Tensile strength. com PRINT FORM Equivalent Standard(s) Relationship: SAE AMS 6484 : 2016 : Similar to: SAE AMS S 5000 : 1999 : Similar to: SAE AMS 6415 : 2016 : Similar to: SAE AMS 6409E : 2016 : Similar to: SAE MAM 6415 : 1998 : Similar to Document Number. FSC Code: 9510 - Bars and Rods, Iron and Steel. 1950. 5V (0. Report Problem (email) Status: Cancelled. 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. Si cr Max. Use our Rapid Response RFQ. 15. Revised. Available Forms: Popular Industry Specifications. 23Cr (7075-T6) (7075-T651)Solution and Precipitation Heat Treated ASTM B209. 4340 Alloy Steel. amrstndz@army. Steel, Chrome-Nickel-Molybdenum (E4340) Bars & Reforging Stock. The alloy’s melting point stands at approximately 2,800°F, and its coefficient of thermal expansion is 6. 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;. Add to Watchlist. REPLACED BY AMS-S-6758. SAE AMS-S-5000, Revision A, March 2007 - Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock. 4340 Alloy Steel. Material UNS ASTM SAE/AISI AMS SAE EN FED JIS DIN BS O. 0. 00%, and the remaining elements comprise the rest of AMS 6414’s composition. 303 sul mill-s-7720, mil-w-52263 ams-5640 type 1, qqs-763c, qqs-764b, astm-a-582 astm-a-320 grd b8f. 4340 Alloy Steel. 4×10⁷ Ωm, making it a great electrical conductor. AMS-S-5000. Proper es are a func on of tubing diameter and wall thickness, refer to specifica on details. Cancelled. 2 Classification: The steel bars and reforging stock shall be as follows:. March 1, 2007. , This specification covers electric furnace steel bars and reforging stock of aircraft quality. Steel, Chrome-Nickel-Molybdenum (4340) 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. 38 - 0. , MIL-S-6090A, dated 4 June 1971, and Amendment 2 dated 20 July 1972, is hereby canceled. 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 6415 : 2016. 📝 Amendments Available. Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard. AMS5085. Identification numbers. Page Count. 0. 6Cu 0. Mo. Buy SAE AMS 4077 : 2015 ALUMINUM ALLOY SHEET AND PLATE, ALCLAD ONE SIDE, 4. 8 Ni, 0. CANCELLATION NOTICE This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of March 2007 and has been superseded by the applicable AMS specifications listed below. Superseded By. 6Zn 2. This combination of alloy and heat treat level. All Grades. 000 HEX - 74978. Historical Revision Information. The requirements of the individual specification applicable to the form required shall be fulfilled whenever reference is made to this specification. Publication Date. 56C (SAE 1050) AMS5085 – available for purchase at $40. E Notice 2 - Notice of cancellation/superseded by. Search our products, such as 4340 steel, AMS 5643, AMS 5737 or many others, and receive a quote! Aero-Vac’s focus is on value added processing to help its customers reduce their overall costs and exposure. 00 Max 0. Per D8-5000 Finish Code VF-1. 187" (4. superseded by ams 2700) a ams-qq-p-416 g astm 2021, e1 . We carry, process and forge MISC Lockheed Martin Corporation Spec STM05-602 Grade 13-8Mo Stainless Steel. Your Message. Buy SAE AMS 5853 : 2012 STEEL, CORROSION AND HEAT-RESISTANT, BARS AND WIRE, 15CR - 25. Issuing Committee: AMS E Carbon and Low Alloy Steels Committee Publisher: SAE International. Publication Date. D. Your support ID is: 1013750275635199346. Manufacturing processes. In September 1999, MIL-T. mil-a-8576-s/s by sae-ams-a-8576 mil-a-8623-s/s by mmm-a-134 mil-a-9117. We carry, process and forge MISC United States Federal GSA Specification QQ-S-766. Our service centers are located throughout the U. 6 - 5005: 5052. Manganese. Because this revision clarifies changes from revision D, changes for both revisions are maintained. Multi - user online standards collection: secure, flexibile and cost effective. A108, UNS. 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. 00: in: stk: 4130 rnd 1. AMS 4037 2024 Aluminum Alloy, Aluminum Sheets and Aluminum Alloy Plate 4. 5. STEEL BARS, FORGINGS, AND TUBING 0. MIL-S-18729 Military (Department of Defense) Specification MilSpec 4130 Alloy Steel. As part of the hosting, they converted the old MS designated part numbers to AMS, NAS, SAE, etc. Superseded. The military paid to have its old specs hosted by commercial standard companies so we can claim we use commercial standards. Our discussion here is driven by the fact that several end-users continue to use the original MIL specification for their peening operations. SAE AMS-S-5000. 5MO (316), SOLUTION HEAT TREATED from SAI Global. Buy SAE AMS 2251 : 2013 TOLERANCES, LOW-ALLOY STEEL BARS from SAI Global. Steel Blocks. 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. 4Cu 1. We carry, process and forge MIL-S-7720 Military Specification 303 Stainless Steel. 4340 Alloy Steel. Kingman Road, Stop 5100, Fort Belvoir VA 22060. The heat treatment of parts fabricated from the steels. 38 - 0. 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. Aircraft Alloys. 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. 9510-00-555-8374, BAR,METAL. All Grades. MIL-S-5000. Home; Why Us? Alloys. We speak metal!302 mil-s-7720, ams-s-7720 astm-a-276, astm-a-479, asme-sa-479. <br/>Your support ID is. 43C) Buy SAE AMS S 6090 : 2006 STEEL CARBURIZING AND NITRIDING, PROCESSES FOR from SAI Global. Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock. 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]. 90 0. qq-w-423 cond b form 1 superseded by astm-a313: 12,540. Passivate Clear Passivate MIL-S-5002 QQ-P-35 AMS-QQ-P-35 AMS-2700 Types: II;VI;VII;VIII ASTM A380 Codes F thru M And ASTM A967 5. We speak metal!321 Stainless Steel. AISI 4340 is a heat treatable, low alloy steel containing nickel, chromium and molybdenum. BMS-7-26 Boeing Spec Alloy Steel. 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. AMS-S-5000 Steel, Chrome-Nickel-Molybdenum (E4340) Bars & Reforging Stock Document Center. 60 . , Da-Kang Village, Kuei-Sun, Taoyuan County. 75% to 1. E-52100, 52100. We carry, process and forge DMS 1935 McDonnell Douglas Specification 300M Alloy Steel. 8mm). Identification numbers. 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. The displayed colour will depend on your monitor and browser and pearl or metallic colours. 4CU - 1. Compression Molding of Reinforced Thermoplastic Materials (QPL) No Nadcap Commodity Code. MIL-H-5606 petroleum base hydraulic fluid for military aircraft (inactive for new designs. 85 0. 00 0. To those users, I hope to provide a4130 Plate 4130 Sheet 4130 Bar 4130 Rod, 4130 Tube, 4130 Tubing 4130 Pipe, 4130 Noramlized and Heat Treat Aircraft Alloy Round,4130 Bar to AMS 2301, AMS-S-6758, ASTM-A-331,ASTM-A-322 MIL-S-6758, AMS 6346, AMS 6370, AMS 6348 4330 MOD Vacuum Melt Normalized & Tempered Round Barsuperseded a superseded standard is one,. Revision Level. 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:. 3) 6al-6v-2sn: ams 4918, ams 4936, ams 4937, ams 4971, ams 4978, ams 4979, mil-t-9046, mil-t-9047, uns 56620 6Al-6V-2Sn Titanium Alloy is an alpha-beta alloy that can be heat treated to higher strengths and heavier section sizes than titanium alloy 6AL-4V. AMS5085. Feb. 2MO - 2. 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. 3) in accordance with this standard. HARD COAT (S/S BY AMS 2469)4340 Alloy Steel. Rationale: AMS-S-6758B has been declared Stabilized as it has been replaced by technically equivalent specifications. 43 C. 11,. Download File - 165. Steel Reforging Stock. AMS 6414 sheet is an alloy steel that consists of carbon, manganese, chromium, molybdenum, vanadium, and nickel. 3Mo - 1. A-286 Stainless Steel. 40 0. Alloy Steel MIL-S-8699 . 8Ni - 0. Available format(s): Hardcopy, PDF. 25 Mo, 0. All Grades. 4340 Alloy Steel. 3. Titanium alloys. Carbon. Alloy Steel MIL-S-7393 . SCOPE: 1. July 1, 1998 Steel, Chrome-Molybdenum (4130) Bars and Reforging Stock (Aircraft Quality) 1. Classes 202, 302, and 305: When sensitization cannot be tolerated classes 202, 302 and 305 are not recommended for use. 90 0. Condition: Special Aircraft Quality Cleanliness Normalized and Tempered. Superseded. AMS S 8802 type 1 is a dichromate cured sealant. 47-0. 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. We carry, process and forge ASTM A575 Specification Steel. Our discussion here is driven by the fact that several end-users continue to use the original MIL specification for their peening operations. 2500. SAE AMS S 5000 : 1999 : STEEL, CHROME-NICKEL-MOLYBDENUM (E4340) BARS AND REFORGING STOCK: ASTM E 1158 : 2014 : REDLINE : Standard Guide for Material Selection and Fabrication of Reference Blocks for the Pulsed Longitudinal Wave Ultrasonic Testing of Metal and Metal Alloy Production Material: SAE AMS QQ A 200/11 : 2014 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 Boeing: Assembly BAC 5000 Grove, OK. 13 AMS2770, AMS2771, and AMS2772 replaces AMS-H-6088. Revision Level. AMS 5516. SAE AMS 6444 : 2015. Vacuum induction and consumable. (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. 2) and the requirements for furnace equipment, test procedures and information for heat-treating procedures, heat-treating temperatures and material (See. Page. 5 w% Sodium Dichromate, 120-130ºF, 20 minutes minimum Type III – Withdrawn Type IV – Withdrawn Type V – Withdrawn Type VI – 25-45 v% Nitric, 70-90ºF, 30 minutes minimum Type VII – 20-25 v% Nitric, 120-150ºF, 20 minutes minimumSteel, Chrome-Molybdenum (4130) Bars and Reforging Stock (Aircraft Quality) (Superseded by SAE AMS-S-6758) To find similar documents by Federal Supply Class Code: FSC 9510 (Bars and Rods) ORDER. Here's a link to the history of the MIL, and here's a link to the history of the AMS. Alloy Designation: UK Specifications: US Specifications: US Federal Specifications: European Specifications: Other: 5005: BS N41 5005 : A-G0. BMS-7-26 Boeing Spec Alloy Steel. Subscribers can view annotate, and download all of SAE's content. sheet/strip/plate: ams 6359 astm a505. Page Count. 11 Btu/ (lb/°F). 13 Cr, 8. 4340 RD BAR COND C - 25394. AMS-S-5000A was issued to cancel and supersede AMS-S-5000 with current, technically equivalent specifications. Material may also meet specs ASTM-A331, ASTM-A304, ASTM-A108, AMS-2301, AMS-S-5000 (replaced MIL-S-5000), EN10204. S. MIL MIL-S-5000E STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS, AND FORGING STOCK (S/S BY SAE-AMS6415P AND SAE-AMS-S-5000) (SUPERSEDING. In the early 1990’s, US Secretary of Defense, William J. AMS-S-6758. Hendrickson Dr. Having a lower carbon content improves weldability. FSC Code: 9510 - Bars and Rods, Iron and Steel. 4340 Alloy Steel. Magnetic materials. sae ams s 6090 : 2006 : steel carburizing and nitriding, processes for: sae as 5944 : 1999 :. Use our Rapid RFQ to request a quote. 00%, and the remaining elements comprise the rest of AMS 6414’s composition. Castle Metals stocks Alloy 4340 plate through our global distribution network. We carry, process and forge AMS 4078 Specification 7075 Aluminum Alloy. 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. 36-60. QQ-P-35C/AMS-QQ-P-35A SPECIFICATIONS Passivation Types Type I – Withdrawn Type II – 20-25 v% Nitric, 2-2. HP9-4-20 High Strength Alloy Steel. Alloy Steel MIL-S-83030 . 20 Mo. Talk To Us About the Alloys You Need Most. 00: si: stk: 15-5ph plt 0. 00. 010 0. DISCLAIMER: The use of this information should be considered strictly voluntary. This specification applies to manufacturers and suppliers who heat treat aerospace material. Subscribers can view annotate, and download all of SAE's content. 65 0. Alloy Steel AMS 6359 . Steel covered by this specification is intended for use in the manufacture of highly stressed aircraft parts requiring high hardenability. 3MO - 0. AMS 5605. Learn more about its features, benefits and typical uses in this PDF document. Related Topics: Test procedures. 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. Our service centers are located throughout the U. MIL-S-5000. 📝 Amendments Available. Status. 32 KB. mil-a-5090-s/s by mmm-a-132 mil-a-5092-s/s by mmm-a-1617. Heat treatment. Max Tens MIL-N-14411 Comp 3 (4750) Cap. 4340 High Tensile Steel in AMSS5000 Specification, per SAE International: “This specification. Titanium alloys. Grinding of Chromium Plate - Landing gear parts 275 KSI or above. 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. Availability. see AMS-P-83461) MIL-H-5606 Better dynamic performance and longer service life at 257°F than AMS-P-25732 (MS28775). astm-d5363 mil-a-101-s/s by mmm-a-250. 60 Si, 0. 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. DMS 2257. 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. 7. 95 Cr, 0. AMS 6265 Alloy Steel. , This specification presents requirements for thin-walled (inside diameter greater than four times the wall thickness and outside diameter 1/4 inch. Use our Rapid Response RFQ to request a quote. , This specification covers the requirements for heat-treatment of four classes of steel (see 1. , This specification covers electric furnace steel bars and reforging stock of aircraft quality. Users may refer to SAE-AMS-S-6090, "Steel Carburizing and Nitriding,. 15 0. This specification is for a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. 284 lb/in³, a thermal conductivity of 24 Btu/ (hr/ft²/°F), and a specific heat of 0. Explore our McDonnell Douglas Specifications product category. 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. Document Number. Heat treatment. 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. ADOPT WITHDRAWN.