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Missile Hydraulic Pumps and Their Power SourcesAIR560D (Current)
This AIR provides information about the specific requirements for missile hydraulic pumps and their associated power sources.
A-6C4 Power Sources Committee
STUD, STEPPED - 2.5 DIA ENGAGEMENT, PD SHANK, UNS S66286 .3750-24 UNJF-3A X .3125-24 UNJF-3AAS3141C (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - HEXAGON HEAD, DRILLED 6 HOLES, PD SHANK, AMS5731, UNS S66286, .375-24 UNJF-3AAS3117B (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - HEXAGON HEAD, DRILLED 6 HOLES, PD SHANK, UNS S66286, .5625-18 UNJF-3AAS3120B (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - HEXAGON HEAD, DRILLED 6 HOLES, PD SHANK, AMS5731, UNS S66286, .4375-20 UNJF-3AAS3118B (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
STUD, STEPPED - 2.5 DIA ENGAGEMENT, PD SHANK, UNS S66286 .3125-24 UNJF-3A X .2500-28 UNJF-3AAS3140C (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - HEXAGON HEAD, DRILLED 6 HOLES, PD SHANK, CRES (UNS S66286), .5000-20 UNJF-3AAS3119B (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
STUD, STEPPED - 2.5 DIA ENGAGEMENT, PD SHANK, UNS S66286 .2500-28 UNJF-3A X .1900-32 UNJF-3AAS3139C (Current)3/23/2026
E-25 General Standards for Aerospace and Propulsion Systems
Shaft Nut and Keywasher Installation Dimensions forAS1495B (Current)3/20/2026
The purpose of this Standard is to provide installation dimensions for shaft nuts and their companion keywasher. The Standard type typically shown on MS9951 and MS9952, but is also suitable for parts which are dimensionally equivalent.
E-25 General Standards for Aerospace and Propulsion Systems
STUD - STRAIGHT, DRILLED, .2500-20UNS X .2500-28UNF-3AAS128363B (Current)3/20/2026
E-25 General Standards for Aerospace and Propulsion Systems
NUT, SPANNER, AERONAUTICAL, UNS G41400AS172321B (Current)3/20/2026
E-25 General Standards for Aerospace and Propulsion Systems
STUD, LOCKED IN - RING, STRAIGHT, HOLE PREPARATION FORAS1620A (Current)3/20/2026
E-25 General Standards for Aerospace and Propulsion Systems
STUD - STRAIGHT, NECKED, .3750-16UNS X .3750-24UNF-3AAS126881B (Current)3/20/2026
E-25 General Standards for Aerospace and Propulsion Systems
STUD - STRAIGHT, WAISTED, .4375-14 X .4375-20UNF-3AAS127193B (Current)3/20/2026
E-25 General Standards for Aerospace and Propulsion Systems
STUD - STRAIGHT, DRILLED, STEEL (SAE 8740), CADMIUM PLATED, .3750-16UNS X .3750-24UNF-3AAS129293B (Current)3/20/2026
E-25 General Standards for Aerospace and Propulsion Systems
RING, RETAINING-SPIRAL, EXTERNAL, LIGHT DUTY, CRESAS3218C (Current)3/20/2026
E-25 General Standards for Aerospace and Propulsion Systems
RING, RETAINING-SPIRAL, EXTERNAL, HEAVY DUTY, CRES (UNS S30200)AS3216C (Current)3/20/2026
E-25 General Standards for Aerospace and Propulsion Systems
STUD - STRAIGHT, DRILLED, .3125-18UNS X .3125-24UNF-3AAS128687B (Current)3/20/2026
E-25 General Standards for Aerospace and Propulsion Systems
Aluminum Alloy, Plate 5.0Cu - 0.4Mn - 0.5Mg - 0.4Ag (2139-T84) Solution Heat Treated, Cold Worked, and Artificially AgedAMS4468A (Current)10/13/2022
This specification covers an aluminum alloy in the form of plate with nominal thickness from 1.000 to 5.000 inches (25.40 to 127.00 mm), inclusive (see 8.5).
AMS D Nonferrous Alloys Committee
Nickel Alloy, Brazing Filler Metal, 73Ni - 4.5Si - 14Cr - 3.1B - 4.5Fe (Low Carbon), 1790 °F (977 °C) Solidus to 1970 °F (1077 °C) Liquidus RangeAMS4776K (Current)10/16/2023
This specification covers a nickel alloy in the form of wire, rod, strip, foil, and powder and a viscous mixture (paste) of the powder in a suitable binder.
AMS F Corrosion and Heat Resistant Alloys Committee
Aluminum Alloy Sheet and Plate, Alclad 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (Alclad 2219-O) AnnealedAMS4096E (Current)12/1/2021
This specification covers an aluminum alloy in the form of sheet and plate 0.020 to 0.499 inch (0.50 to 12.50 mm), inclusive, in nominal thickness, clad on two sides (see 8.6).
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Plate 4.0Cu - 1.0Li - 0.40Mg - 0.35Ag - 0.13Zr (2195-T34) Solution Heat Treated and Stress RelievedAMS4472B (Current)10/13/2022
This specification covers an aluminum alloy in the form of plate 0.500 to 2.250 inches (12.70 to 57.15 mm), inclusive, in nominal thickness (see 8.6).
AMS D Nonferrous Alloys Committee
Aluminum, Foil and Light Gage Sheet 99.45Al (1145-0) AnnealedAMS4011E (Current)8/5/2022
This specification covers aluminum in the form of foil and light gage sheet.
AMS D Nonferrous Alloys Committee
Plating, Zinc-Nickel AlloyAMS2417K (Current)5/26/2020
This specification covers the requirements for electrodeposition of a zinc-nickel alloy and the properties of the deposit.
AMS B Finishes Processes and Fluids Committee
Steel, Corrosion and Heat-Resistant, Welded and Drawn or Seamless and Drawn Tubing 9.0Mn - 20Cr - 6.5Ni - 0.28N High-Pressure HydraulicAMS5561H (Current)10/12/2021
This specification covers a corrosion and heat-resistant steel in the form of welded and drawn or seamless and drawn tubing.
AMS F Corrosion and Heat Resistant Alloys Committee
Electro-Deposition of ZincAMS03_20A (Current)10/4/2017
This SAE Standard specifies the requirements for the electro-deposition of zinc on non-corrosion resisting steel items for protection against corrosion, and on copper-base alloy items and corrosion resisting steel items for the reduction of contact corrosion of less noble metallic materials. Zinc coatings shall not be used on items which are liable to be subjected to temperatures exceeding 350 °C.
AMS B Finishes Processes and Fluids Committee
Cleaner for Exterior Aircraft Surfaces Gel-Type, Solvent-BaseAMS1533C (Current)1/8/2019
This specification covers a solvent-base cleaner in the form of a gel.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Shot Peening of Metal PartsAMSS13165A (Current)12/17/2007
This specification covers procedure requirements for shot peening of metal parts, to induce residual compressive stresses in specified surfaces, for the purpose of improving resistance to fatigue, stress corrosion cracking, and galling (see 6.1).
AMS B Finishes Processes and Fluids Committee
Coating Material, Fluorocarbon (FKM), Elastomeric, Rain-Erosion Resistant, Color MatchedAMS3138/3C (Current)4/14/2009
This specification has been declared "CANCELLED " by the Aerospace materials Division, SAE, as of April 2009, and has been superseded by AMS3138D. The requirements of the latest issue of AMS3138D shall be fulfilled whenever reference is made to the cancelled AMS3138/1B. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications, noting that it has been superseded by AMS3138D. Cancelled specifications are available from SAE.
AMS G8 Aerospace Organic Coatings Committee
Coating Materials, Fluorocarbon (FKM) ElastomericAMS3138D (Current)12/20/2007
This specification covers fluorocarbon (FKM) elastomeric coating materials for fiber-reinforced-resin composite structures in the form of two-component brushable or sprayable liquids.
AMS G8 Aerospace Organic Coatings Committee
Coating Material, Fluorocarbon (FKM) Elastomeric, Anti-Static Topcoating, WhiteAMS3138/5C (Current)4/14/2009
This specification has been declared "CANCELLED " by the Aerospace materials Division, SAE, as of April 2009, and has been superseded by AMS3138D. The requirements of the latest issue of AMS3138D shall be fulfilled whenever reference is made to the cancelled AMS3138/1B. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications, noting that it has been superseded by AMS3138D. Cancelled specifications are available from SAE.
AMS G8 Aerospace Organic Coatings Committee
Aluminum Alloy 6061, Plate and SheetAMSQQA250/11A (Current)7/15/2008
This specification covers the specific requirements for 6061 aluminum alloy plate and sheet.
AMS D Nonferrous Alloys Committee
Welding, Resistance: Spot and SeamAMSW6858B (Current)11/21/2007
This specification covers requirements for resistance spot and seam welding of the following metals and their alloys. Group 1 - Aluminum and magnesium Group 2 - Iron, nickel, and cobalt Group 3 - Titanium
AMS B Finishes Processes and Fluids Committee
Aluminum Alloy, Alclad 7075 Plate and Sheet, Improved Exfoliation ResistantAMSQQA250/25B (Current)3/23/2009
This specification has been declared "CANCELLED " by the Aerospace Materials Division, SAE, as of March 2009 and has been superseded by AMS4316. The requirements of the latest issue of AMS4316 shall be fulfilled whenever reference is made to the cancelled AMS-QQ-A-250/25. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications, noting that it has been superseded by AMS4316. Cancelled specifications are available from SAE.
AMS D Nonferrous Alloys Committee
Detergent, External Removable Fuel TanksAMSD81956A (Current)2/26/2008
This specification covers a water soluble, oil dispersing nonionic detergent used for cleaning aircraft removable fuel tanks.
AMS J Aircraft Maintenance Chemicals and Materials Committee
Alloy Welding Electrodes, Covered, Corrosion and Heat-Resistant, 75Ni - 15Cr - 1.5 (Cb+Ta) - 1.9Ti - 0.55Al - 5.5FeAMS5779E (Current)3/26/2008
This specification covers a corrosion and heat resistant nickel alloy wire in the form of covered welding electrodes.
AMS F Corrosion and Heat Resistant Alloys Committee
Steel Tubing (Seamless for Machined Parts) .55ni .50cr .25mo (.38 - .43c) Heat-Treated (180,000 Tensile Strength)AMS6285 (Current)12/16/2002
AMS E Carbon and Low Alloy Steels Committee
Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 47.5ni 22cr 1.5co 9.0mo 0.60w 18.5fe, Solution Heat TreatedMAM5536B (Current)3/12/2003
This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate procured in SI (metric) units. AMS 5536 is the inch/pound version of this MAM. These products have been used typically for parts requiring oxidation resistance up to 1205 degrees C and relatively high strength up to 815 degrees C, but usage is not limited to such applications.
AMS F Corrosion and Heat Resistant Alloys Committee
FLUID, DEICING/ANTI-ICING, RUNWAYS AND TAXIWAYS Potassium Acetate BaseAMS1432 (Current)7/23/2002
This specification covers a potassium-acetate base deicing/anti-icing fluid in the form of a concentrated liquid.
G-12RDP Runway Deicing Product Committee
Aluminum Alloy, Sheet and Plate 4.5 Cu - 1.5 Mg - 0.60 Mn (2024-T36) Width Over 48 to 60 In., Incl.AMS4098 (Current)12/16/2002
AMS D Nonferrous Alloys Committee
Tungsten Sheet, Strip, Plate, and Foil, Pressed, Sintered, and WroughtAMS7898D (Current)7/23/2002
This specification covers tungsten in the form of pressed, sintered, and wrought sheet, strip, plate, and foil.
AMS G Titanium and Refractory Metals Committee
Adhesion Promoter for Polysulfide Sealing Compounds Water BasedAMS3100/3A (Current)12/15/2008
This specification has been declared "CANCELLED " by the Aerospace Materials Division, SAE, as of December 2008 and has been superseded by AMS3100B. The requirements of the latest issue of AMS3100B shall be fulfilled whenever reference is made to the cancelled AMS3100/3. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications, noting that it has been superseded by AMS3100B.
AMS G9 Aerospace Sealing Committee
Steel Tubing (Seamless for Machined Parts) .55ni .50cr .25mo (.38-.43c) Heat-Treated (180,000 T.S.)AMS6286 (Current)12/16/2002
AMS E Carbon and Low Alloy Steels Committee
Coating System, Polyurethane, Nonyellowing, White, Rain Erosion Resistant, Thermally ReflectiveAMSC83445A (Current)3/9/2001
This specification covers the requirements for one type of thermally reflective non-yellowing white rain erosion resistant polyurethane coating system.
AMS G8 Aerospace Organic Coatings Committee
Sealing Compound, Polythioether, Ambient Cure or Immediate Heat Cure For Aircraft Structures, Fuel Resistant with Intermittent Use to 400°CF (204°CC)AMS3263A (Current)12/13/2002
this specification covers two classes of a guel resistant polythioether sealing compound supplied as a two-component system.
AMS G9 Aerospace Sealing Committee
Aluminum Alloy, Sheet and Plate 4.5cu 1.5mg 0.60mn (2024-T36) Width Over 30 to 48 In., Incl.AMS4104 (Current)12/16/2002
AMS D Nonferrous Alloys Committee
Steel Plate, Sheet, and Strip, Alloy 4130, Aircraft QualityAMSS18729A (Current)1/24/2002
This specification covers chrome-molybdenum alloy 4130, steel sheet, strip, and plate of thickness to and including 1.50 inches.
AMS E Carbon and Low Alloy Steels Committee
Pressure Testing, Hydraulic, 6895 KpaMAM2620C (Current)11/28/2001
This specification provides requirements and procedures for hydraulic-pressure leak testing of parts.
AMS B Finishes Processes and Fluids Committee
Tin Bronze Castings, Sand and Centrifugal 86.5cu 11.2sn 2.0zn as CastAMS4846B (Current)2/1/2001
This specification has been declared "NONCURRENT" by the Aerospace Materials Division, SAE, as of 10-1-83. It is recommended that this specification not be specified for new designs. See AMS 4845 for a recommended substitute casting alloy.
AMS D Nonferrous Alloys Committee
Aluminum Alloy, Bars, Rods, and Wire 1.0Mg - 0.60Si - 0.30Cu - 0.20Cr (6061-T4) Cold Finished, Solution Heat Treated and Naturally AgedAMS4116K (Current)4/14/2021
This specification covers an aluminum alloy in the form of bars, rods, and wire.
AMS D Nonferrous Alloys Committee
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