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. 8 word “end ”added before items 5. How to Order; Standards We Provide; Updating, Reporting, Audits. To request the addition of new colors, please send a paint sample (on an acceptable substrate) to the SAE contact below. Outer ring: Alloy steel, AMS-S-5000, AMS-S-6758 or AMS-S-6050 Inner ring: CRES 440C, HRC 55 min. 20 1. It is based on using an acid (nitric or citric. 25Mo (0. Alloy 302. S. 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 –. AMS-S-6758 has excellent physical properties. 69 in addtion to MIL-C-5056: S391: PS18021: DFL:. 4130 bars are produced in Round, Flat, Square, and Hex shapes. 250, . This specification covers the requirements for heat-treatment of four classes of steel (See 1. 32 KB. Steel. Magnetic materials. Steel Sheets. 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]. What is alloy 4140 steel? Alloy 4140 is an oil-hardening steel of relatively high hardenability. qq-w-423 cond b form 1 superseded by astm-a313: 12,540. 6Zn 2. 4427 ws 1. Steel Rings. Publication Date. Condition A AMS 5648 Not in MMPDS. I recommend you purchase the AMS for your quotation. AMS-S-5000 - ADOPT WITHDRAWN - SUPERSEDED -- See the following: AMS-6415 AMS-6484 Show Complete Document History. AMS6361G. Related Topics: Heat resistant materials. SAE AMS-S-5000, Revision A, March 2007 - Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock. All of our alloys steels are fully certified by United States producing mills and are shipped with original mill test reports. MIL-S-5000E, MILITARY SPECIFICATION: STEEL, CHROME-NICKEL-MOLYBDENUM (4340) BARS, AND FORGING STOCK (12-NOV-1982) [S/S BY SAE-AMS-S-5000]. 1) per SAE AMS 6414, and both are heat treated to 260 to 280 ksi (pounds per square inch ×1000). 95 Cr, 0. AMS5085. Nickel L-605 . Aluminium Alloy 5000. HP9-4-20 High Strength Alloy Steel. LAMINATED SHEET. Metallurgy. Superseded. Superseded. BMS-7-26 Boeing Spec Alloy Steel. Round Bar, Flat Bar, Plate. Our discussion here is driven by the fact that several end-users continue to use the original MIL specification for their peening operations. Revision Level. AMS 4045 7075 Aluminum Alloy, Aluminum Sheets and Aluminum Alloy Plate 5. Classes 202, 302, and 305: When sensitization cannot be tolerated classes 202, 302 and 305 are not recommended for use. MIL-S-5000. S. AMS S 8802 type 1 is a dichromate cured sealant. Explore our McDonnell Douglas Specifications product category. 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. 40TI (SAE 30321), SOLUTION. This blog. Subscribers can. mil-a-907. Also known as: SAE AMS 3651 SAE MOBILUS. Also known as: SAE AMS 5735 SAE MOBILUS. 3) test procedures. Historical. 25 . ¼ Hard MIL-S-5059 AMS 5907 MMPDS Section 2. Santa Fe Springs, CA Manufacturer*, Distributor $5 - 9. 7 Cooling The load shall be cooled from the nitriding temperature in a suitable atmosphere to 300 °F (149 °C) or below. 0. Per D8-5000 Finish Code VF-1. 43 0. 30V, CONSUMABLE ELECTRODE MELTED 1800 DEGREES F (982 DEGREES C) SOLUTION TREATED AND WORK-STRENGTHENED, 160 KSI (1103 MPA) TENSILE STRENGTH from SAI Global. 4130 Alloy Steel in AMS-S-6758 per SAE International: “This specification covers chrome-molybdenum (4130) steel bars and forging stock of. 750"dia: 72. December, 2007, and has been superseded by AMS 2430, Shot Peening. AMS-S-5000 Steel, Chrome-Nickel-Molybdenum (E4340) Bars and Reforging Stock 2. E Notice 1 - Notice of cancellation/superseded by SAE AMS 6415. We stock and distribute quality alloy steel from the finest. Qualified to SAE-AS81820 BODY BALL RACEDocument Number. Defense industry. Perry, was at the forefront of military specification reform. Aug. 2738 FAX: 210. 1 for heat treatment of steel parts (see 8. 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. 6415, AMS. ALLOY ROD/BAR ROUND 4340 AMS-S-5000 2. All Grades. 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. All Grades. Steel Bars. Description Description AH 36 Bars. Available format(s): Hardcopy, PDF. Document History. Titanium alloys. 1998-04-01. Metal finishing. Quality assurance. Carbon. 0. 6al/4v Alpha/Beta Titanium Alloy. S. 60MN (CLAD ONE SIDE 2024-O), ANNEALED from SAI Global. 0000 x 144. 43%, manganese ranges from 0. DISCLAIMER: The use of this information should be considered strictly voluntary. Death Sandringham House in Norfolk, where the King died. plate/sheet/strip: ams 6350. AMS 4109 7175-T736 Superseded by AMS 4149: WS 3. ASTM E 2422 : 2017 : REDLINE. The passivation treatments provided by this specification are intended to improve the corrosion resistance of parts made from austenitic, ferritic and martensitic corrosion-resistant steels of the 200, 300 and 400 series. AMS-S-13165. All Grades. american aircraft quality alloy steel bar-analysis cmnpmax. 1. REVISION E. 15. Document History. Tensile strength. mil-s-5000 mil-s-8844. Email：hanjustdoit@gmtc. 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. MIL-S-5000. 1 316 Various Bar, Wire, Forgings QQ-S-763 AMS-QQ-S-763 Should not be specified for new design. Critical updates of standards and customisable alerts and notifications. si ni cr mo cu max. AMSS5000A. Please enable JavaScript to view the page content. 13 Cr, 8. 3), Reports (4. Electroless nickel plating is an process that codeposits a nickel-phosphorous alloy without need for an externally applied electrical current. BC Ferry: Washington - Bellingham - Victoria - British Columbia Travel and Adventure Vacations. 85 0. SCOPE: 1. 302 Foil (Shim) is available in various thicknesses. S. 000" (177. Manganese. 080 x 60. Titanium alloys. Click here to view the AMS Std. 1 Al. Alloy Steel Grade: AISI 4340. 4340 Alloy Steel (AMS-S-5000) Heat Treated Cadmium Plated 440C Stainless Steel (AMS 5630) Heat Treated Hard Chrome Plated (AMS-QQ-C-320, Class 2) 17-4 PH Stainless Steel (AMS 5643) Heat Treated AT 3200 Bearing Liner, Permanently Bonded to Race I. 1), Properties (3. Rationale: AMS-S-5000A was issued to cancel and supersede AMS-S-5000 with current, technically equivalent specifications. Max Tens MIL-N-14411 Comp 3 (4750) Cap. 11 Btu/ (lb/°F). 416 ht r. Revision A actually just issued the cancellation notice, replacing this specification with the AMS-2700 document. 9510-00-555-8374, BAR,METAL. com I pierce-spafford. 43. 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. A-286 Stainless Steel. Reference to AMS2759 on a drawing, fabrication order, purchase order, etc. 43%, manganese ranges from 0. REV E CANCELLATION 1. Test procedures. 📝 Amendments Available. 284 lb/in³, a thermal conductivity of 24 Btu/ (hr/ft²/°F), and a specific heat of 0. MIL-S-5000 › Complete Document History Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock (Superseded by SAE AMS-S-5000) How to Order Standards We ProvideAMS 6414 Alloy Steel. Status. 6 Peening intensity: Unless otherwise specified on the drawing or in the contract, the. 8 Ni, 0. Alternate References are: 002289735,9510002289735,00-228-9735,AMS-S-5000,MILS5000,AMS 6484,AMS-S-5000,MILS5000,AMS6484This reference table lists some of the specs available. The displayed colour will depend on your monitor and browser and pearl or metallic colours. 4. 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. 6al/4v Alpha/Beta Titanium Alloy. Revision Level. Read less…. Status. Status. DOD ADOPTION. Heat Treatment of Steel Raw Materials (STABILIZED Sep 2020) AMSH6875C. Nov. Related Topics: Heat treatment. 38-0. HP9-4-30 High Strength Alloy Steel. Consumable electrode vacuum remelted, normalized. STEEL PLATE, SHEET, AND STRIP, ALLOY, 4130, AIRCRAFT QUALITY (S/S BY SAE-AMS6350, SAE-AMS6351 OR SAE-AMS6345. AMS 6931 6al/4v Titanium Alloy. Chromic Acid Anodizing - Class 5. AMS 5637, QQS-763, MIL-S-7720. Report Problem (email) Status: Cancelled. “This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. 6Cu 0. 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. Test procedures. AMS-S-5000 - BASE - SUPERSEDED -- See the following:. The AMS-5000 installation requires replacing the integrated avionics processing system (IAPS) and associated components to provide the latest technology available for the Pro Line 4 system. MIL-S-5000 Steel, Chrome-Nickel-Molybdenum (4340) Bars, and Forging Stock. SAE AMS-QQ-S-763. Steel covered by this specification is intended for use in the manufacture of highly stressed aircraft parts requiring high hardenability. 1. HP9-4-20 High Strength Alloy Steel. The carbon content ranges from 0. Ask a question or request a quote. 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. SAE AMS-S-5000 ( Complete Document ) Superseded By: 1999 Edition, March 1999. Technical Data Sheet. forging: ams 6382 astm a 646. Status: Withdrawn. 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 electric furnace steel bars and reforging stock of aircraft quality. This specification covers a carbon steel in the form of sheet, strip, and plate. May 1, 2009. Users may refer to SAE-AMS-S-6090, "Steel Carburizing and Nitriding,. 19, 1998. Material may also meet specs ASTM-A322, ASTM-A304, ASTM-A108, AMS-2301, AMS-S-5000 (replaced MIL-S-5000), EN10204. MIL-S-5000 Revision E:1982 : Similar to: Standards Referenced By This Book - (Show below) - (Hide below) SAE AMS STD 2154 : 2017-05 : INSPECTION, ULTRASONIC, WROUGHT METALS, PROCESS. Many contracts still call out MIL-T-9047 and AMS. Grinding of Chromium Plate - Landing gear parts 275 KSI or above. SAE AMS 6485 : 1989. 6. MIL S-5000: AMS 6409 Specifications. Steel Forgings. SPECIFICATIONS: AISI4340, ASTM A 829 / A6 SAE J404, AMS 2252/ 2301/6359 SAE J404. Read more…. SAE revised the scope of paragraph 1. Technical Data Sheet. It has a density of 0. Eredhel Quality Manager. 455 Stainless Steel. tw; Taipei Branch Office. Superseded By: SAE AMS6415 Document Language: English Published By: SAE International (SAE) Page Count: 12 ANSI Approved: No DoD Adopted: No Document History:. 7004 State Route 123 Franklin, OH 45005 . 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. Subscribers can view. AMS ASME; 1050: Aluminum Coil: Aluminum Strip: Aluminum Plate: 1060: Aluminum Coil: ASTM-B209: Aluminum Strip. Status. Use our Rapid Response RFQ to request a quote. Alloy Steel MIL-S-7393 . 1. Alloy E 4340 is a widely used deep-hardening constructional steel. 50, 1. 80Cr - 1. 9 Mil 1984 10-49. K, France, Singapore, and Shanghai. Page. 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,. AMS 6931 6al/4v Titanium Alloy. Pages: 11. 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. 38 - 0. ADOPT WITHDRAWN. 6al/4v Alpha/Beta Titanium Alloy. 05C) (SAE 52100), PREMIUM AIRCRAFT-QUALITY, CONSUMABLE ELECTRODE VACUUM REMELTED. 4130 Alloy Steel. 80 S150 – – – MSRR 6591/2/5/6/7, 6603/31, 6902/19,Superseded by AWS D17. Related Topics: Test procedures. All Grades. Issuing Committee: AMS F Corrosion and Heat Resistant Alloys Committee Publisher: SAE International. Document Number. This specification covers electric furnace steel bars and reforging stock of aircraft quality. 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. 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. 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]. If you require technical assistance or would like to receive a quote, please call our Customer Service team TOLL FREE at (866) 610-1660. View superseded by. 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. E-52100, 52100. HP9-4-20 High Strength Alloy Steel. 5000 Series Aluminum Sheet; 6000 Series Aluminum Sheet; 7000 Series Aluminum Sheet; Aluminum Checker / Tread / Diamond Plate; Aluminum Wire. 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. 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. Find Standards By. 347 / 347H. Revision A, March 2007. 5000 Series Aluminum Sheet; 6000 Series Aluminum Sheet; 7000 Series Aluminum Sheet; Aluminum Checker / Tread / Diamond Plate; Aluminum Wire. Different grades of steel are achieved by adding other alloying elements, such as manganese, nickel, chromium, titanium and molybdenum to the basic mix. Document Number. Use our Rapid RFQ to request a quote. current specification revisions revision 122022. tube/pipe: ams 6414 ams 6415 astm a519. SAE AMS-S-6090. 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. 2 Timothy 1:7 . Alternate References are: 005057354,9510005057354,00-505-7354,AMS-S-5000,MIL-S-5000,AMS-S-5000,MIL-S-5000Buy SAE AMS S 5000 : 2007 STEEL, CHROME-NICKEL-MOLYBDENUM (E4340) BARS AND REFORGING STOCK from NSAIproduct forms rod & bar plate sheet coil strip tube ingot billet Los Angeles, California 1-877-727-6073 E-MAIL [email protected] psd: 1-1, 9-3 d6-5000 bv d8-5000 p d8-5000 psd: 8-57 dms1786 p dms1786 030-mc dms2433 b. Steel, Corrosion Resistant, Bars, Wire, Shapes, and Forgings. 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]. HP9-4-30 High Strength Alloy Steel. Multi - user online standards collection: secure, flexibile and cost effective. Related Topics: Coatings, colorants, and finishes. 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. Perry, was at the forefront of military specification reform. 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. 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. 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. Our discussion here is driven by the fact that several end-users continue to use the original MIL specification for their peening operations. 00: in: stk: 4130 rnd 1. 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. HP9-4-20 High Strength Alloy Steel. AMS 6931 6al/4v Titanium Alloy. This change spawned a great deal of controversy in the heat treating industry which continues to this day. 284 lb/in³, a thermal conductivity of 24 Btu/ (hr/ft²/°F), and a specific heat of 0. 4435 ws 1. 48, 160 Lane, Da Hoo Rd. 40ti (321), solution heat treated from sai global. SAE AMS-S-6758. 1. Publication Date. Feb. 4340 Alloy Steel. MIL-S-6090A, MILITARY SPECIFICATION: STEELS USED IN AIRCRAFT CARBURIZING AND NITRIDING, PROCESS FOR (4 JUN 1971) [S/S BY SAE-AMS-S-6090]. 10 pages SAE AMS 6485 : 1989. The balance of these elements makes AMS 6414 a high. HP9-4-30 High Strength Alloy Steel. see AMS-P-83461) MIL-H-5606 Better dynamic performance and longer service life at 257°F than AMS-P-25732 (MS28775). 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. 30 2. A-286 Stainless Steel. 4140 AMS 6382, AMS-S-5626, 4340 AMS 6415, AMS-S-5000 8740 AMS-S-6049, AMS 6322 9310 AMS 6260 52100 BAR AMS 6440, AMS-S-7420 (Less Par. HP9-4-20 High Strength Alloy Steel. 000 HEX. We carry, process and forge AMS 5604 Specification 17-4PH Stainless Steel. 8. SAE AMS-H-6875. AMS 6414 sheet is an alloy steel that consists of carbon, manganese, chromium, molybdenum, vanadium, and nickel. 32 KB. mil-a-5540. AMS 6414 Composition. 6×10^-6 in/ (in·°F). The alloy’s melting point stands at approximately 2,800°F, and its coefficient of thermal expansion is 6. Materials are available in sheets, plates and hex, square, flat and round bars. Publication Date. Legends Steel Company is a premier metals distributor providing many grades of material from Aluminum, Stainless & Alloy to Titanium bars and plates. 025 . Buy SAE AMS S 5000 : 1999 STEEL, CHROME-NICKEL-MOLYBDENUM (E4340) BARS AND REFORGING STOCK from SAI Global. BAC 5019. Alloy Designation: UK Specifications: US Specifications: US Federal Specifications: European Specifications: Other: 5005: BS N41 5005 : A-G0. 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]. 010 0. This alloy is known for its excellent mechanical properties, corrosion, and heat resistance. 60Mn (2024-T3) (2024-T351) Solution Heat Treated QQ-A-250/4. Revision Level. Issued. AMS-S-5000. 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. 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. 25 Mo, 0. 55C (SAE 1050) from SAI Global. Steel Forgings. Grade Description Specification; C11000: ETP COPPER: AMS 4500, ASTM-B-152: C17200: BERYLLIUM COPPER: AMS 4530, AMS 4533, AMS 4534, AMS 4650, AMS 4651: AMS 4535, QQC. No. Popular Metal Grades. Alloy Steel AMS 6304 (17-22A) Alloy Steel MIL-S-5000 . Not in MMPDS. Page Count. Changed AMS I-6875 to AMS-H-6875. May 1, 1999 Sealing Compound, Temperature Resistant, Integral Fuel Tanks and Fuel Cell Cavities, High Adhesion ams-s-8802. Revised. Chrome Vanadium Com K15048 A‐231 6150 10270‐2 2803 735A50 HS OT Chr. AMS-T-9047A was cancelled and superseded by various specifications. AMS2750F is typically communicated via industry standards such as SAE/AMS specifications as well as customer purchase orders and part prints. DMS 2257. 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. The alloy’s melting point stands at approximately 2,800°F, and its coefficient of thermal expansion is 6. Description / Abstract: SAE AMS-S-6090, Revision B, May 2006 - Steel Carburizing and Nitriding, Processes for. May 1, 1999 Sealing Compound, Temperature Resistant, Integral Fuel Tanks and Fuel Cell Cavities, High Adhesion This specification covers temperature resistant, two component synthetic rubber compounds of the polysulfide type for sealing and repairing integral fuel tanks and fuel cell cavities, for continuous. SAE AMS-S-6090. AMSS6090A. 1954-05-01. 6 - 5005: 5052. " (Application for copies of SAE publications should be addressed to the Society of Automotive Engineers, 400 Commonwealth Drive, Warrendale, PA 15096-0001. 1 Scope: This specification covers chrome-molybdenum (4130) steel bars and forging stock of aircraft quality. mil-a-13881 mil-a-13883 mil-a-21366 mil-a-22010-s/s by astm-d2564 mil-a-22895 mil-a-23941 mil. Subscribers can view annotate, and download all of SAE's content. March 3, 2010. 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. Alloy Steel MIL-S-83030 . STEEL BARS AND FORGINGS, 5. 43C) Buy SAE AMS S 6090 : 2006 STEEL CARBURIZING AND NITRIDING, PROCESSES FOR from SAI Global. Identification numbers. AH 36 Bars Suppliers.