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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
RING, RETAINING-SPIRAL, EXTERNAL, HEAVY DUTY, CRES (UNS S30200)AS3216C (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, DRILLED, .3125-18UNS X .3125-24UNF-3AAS128687B (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
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 - 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
STUD, STEPPED - 2.5 DIA ENGAGEMENT, PD SHANK, UNS S66286 .4375-20 UNJF-3A X .3750-24 UNJF-3AAS3142C (Current)3/19/2026
E-25 General Standards for Aerospace and Propulsion Systems
BEARING, BALL, AIRFRAME, ANTIFRICTION, EXTRA LIGHT DUTYAS27646E (Current)3/19/2026
ACBG Rolling Element Bearing Committee
STUD, STEPPED - 2.5 DIA ENGAGEMENT, PD SHANK, UNS S66286 .5000-20 UNJF-3A X .4375-20 UNJF-3AAS3143C (Current)3/19/2026
E-25 General Standards for Aerospace and Propulsion Systems
Application Layer - Generator Sets and IndustrialJ1939/75_202603 (Current)3/19/2026
SAE J1939-75 defines the set of data parameters (SPs) and messages (PGs) for information predominantly associated with monitoring and control generators and driven equipment in electric power generation and industrial applications. The data parameters (SPs) and messages (PGs) previously published within this document are published in SAE J1939DA. Applications using the SAE J1939-75 document must refer to SAE J1939DA for the SAE J1939 parameters and messages for monitoring and controlling the power units, e.g., engines and turbines, that power the generators and driven industrial equipment.
Truck and Bus Control and Communications Network Committee
CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE (FOR MIL-C-81511 SERIES 2 CONNECTORS)AS39029/46C (Current)3/19/2026
AE-8C1 Connectors Committee
CONNECTOR, RECEPTACLE, JAM NUT MOUNT, ELECTRICAL, CIRCULAR, HIGH DENSITY, QUICK DISCONNECT, ENVIRONMENT RESISTING, INDIVIDUAL RELEASE, CRIMP TYPE CONTACTS (CLASS A, F, AND W - SERIES 4)AS81511/53B (Current)3/19/2026
AE-8C1 Connectors Committee
Titanium Alloy Bars, Forgings, and Rings, 6Al - 4V Extra Low Interstitial (ELI), Duplex Annealed, Fracture ToughnessAMS4931H (Current)3/19/2026
This specification covers a titanium alloy in the form of bars 6.000 inches (152.40 mm) and under in nominal diameter or least distance between parallel sides, forgings, flash-welded rings 6.000 inches (152.40 mm) and under in thickness, and stock for forging and stock for flash-welded rings of any size (see 8.6).
AMS G Titanium and Refractory Metals Committee
BEARING, ROLLER, NEEDLE, TRACK ROLLER, CROWN RADIUSED OD INTEGRAL STUD, TYPE VII ANTIFRICTION, INCHAS21447D (Current)3/19/2026
ACBG Rolling Element Bearing Committee
Pressure Testing, Hydraulic, 17.5 MpaMAM2625C (Current)11/28/2001
This specification provides requirements and procedures for hydraulic-pressure leak testing of parts. AMS 2625 is the inch/pound version of this MAM.
AMS B Finishes Processes and Fluids Committee
Aluminum Silicon Bronze Bars, Rods, and Forgings, 90cu 7.0al 1.9si, Drawn and Stress RelievedAMS4263A (Current)1/1/1993
This specification has been declared 'Superseded' by the Aerospace Materials Division, SAE, as of September, 1992. The requirements of this specification are embodied in the latest issue of AMS 4633. UNS Number: C64200 Alloy: HR50
AMS D Nonferrous Alloys Committee
Titanium Alloy, Bars 11.5Mo 6.0Zr 4.5Sn, 1275 - 1350°F (690 - 730°C) Solution Heat TreatedAMS4977C (Current)1/1/1993
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of August, 1992.
AMS G Titanium and Refractory Metals Committee
Bars, Die Drawn, 0.95cr 0.29mo 0.05te (0.40-0.53c), Tempered, 165,000 Psi YieldAMS6379B (Current)6/1/2001
This specification covers a low-alloy steel in the form of round bars up to 2.00 in. (50.8 mm), incl, in diameter.
AMS E Carbon and Low Alloy Steels Committee
Steel, Investment Castings Alloy and CarbonAMSS22141A (Current)1/21/2003
This specification covers alloy and carbon steel castings made by the investment precision casting process. (See 6.1).
AMS E Carbon and Low Alloy Steels Committee
Cloth, Knitted Nylon Stretch Polychloroprene CoatedAMS3271B (Current)8/25/2011
This specification covers a polychloroprene-coated, one side only, nylon knit in the form of cloth.
AMS P Polymeric Materials Committee
ALUMINUM ALLOY FORGINGS 4.3Zn - 3.3Mg - 0.6Cu - 0.2mn - 0.2Cr (7079-T611) Solution and Precipitation Heat Treated, Low Residual StressesAMS4136 (Current)8/10/2011
AMS D Nonferrous Alloys Committee
ALUMINUM ALLOY WELDING WIRE 5.0Si - 1.2Cu - 0.50Mg (C355.0)AMS4188/3 (Current)12/16/2002
This specification covers an aluminum alloy in the form of extruded or drawn welding wire.
AMS D Nonferrous Alloys Committee
Steel, Corrosion and Heat Resistant, Bars and Forgings 2.5si 12.5si 8.0ni AnnealedAMS5705E (Current)9/4/2002
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of September, 2002. Alloy: CNS UNS Number: S63005
AMS F Corrosion and Heat Resistant Alloys Committee
Tungsten Forgings, Pressed, Sintered, and ForgedAMS7897C (Current)7/1/2002
This specification covers tungsten in the form of forgings produced from billets processed by isostatically cold pressing, utilizing hydrogen reduced tungsten powder, and high-temperature sintering.
AMS G Titanium and Refractory Metals Committee
Titanium Alloy, Extrusions and Flash Welded Rings, 6al 6v 2sn, Beta Extruded Plus Annealed, Heat TreatableAMS4936E (Current)7/23/2002
This specification covers a titanium alloy in the form of extruded bars, tubes, and shapes, and of flash welded rings and stock for flash welded rings.
AMS G Titanium and Refractory Metals Committee
Aluminum Alloy, Sheet, Alclad, 6.0cu 0.40zr, as RolledMAM4209B (Current)3/12/2003
This specification covers an aluminum alloy in the form of sheet procured in metric units. Primarily for parts requiring a high degree of formability (superplasticity) and response to heat treatment.
AMS D Nonferrous Alloys Committee
Steel Tubing (Seamless for Machined Parts) .55ni .25mo (.33 - .38c) Normalized Or Heat-Treated (90,000 Tensile Strength)AMS6283 (Current)12/16/2002
AMS E Carbon and Low Alloy Steels Committee
Steel: Chrome-Molybdenum (4140) Bars Rods, and Forging Stock (For Aircraft Applications)AMSS5626A (Current)1/24/2002
This specification covers chrome-molybdenum (4140) steel bars, rods, and forging stock of aircraft quality.
AMS E Carbon and Low Alloy Steels Committee
Honeycomb Core, Aluminum Alloy, for Sandwich Construction, 5056, 350 (175)AMS4176C (Current)11/28/2001
This specification covers one type of honeycomb core made of aluminum alloy and supplied in the form of blocks, slices, or other configurations as ordered.
AMS D Nonferrous Alloys Committee
Steel, Bars, Forgings, and Tubing, 0.80cr 1.8ni 0.25mo (0.38 0.43)MAM6415C (Current)3/12/2003
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock procured in SI (Metric) units. AMS 6415 is the inch/pound version of this MAM. These products have been used typically for parts, 90 millimeters and under in nominal thickness at time of heat treatment, requiring a through-hardening steel capable of developing a minimum hardness of 40 HRC when properly hardened and tempered and also for parts of greater thickness but requiring proportionately lower hardness, but usage is not limited to such applications. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking after heat treatment; ARP 1110 recommends practices to minimize such conditions.
AMS E Carbon and Low Alloy Steels Committee
Aluminum Alloy, Sheet and Plate 4.5cu 1.5mg 0.60mn (2024-T36) Width 30 In. and UnderAMS4103 (Current)12/16/2002
AMS D Nonferrous Alloys Committee
Cast Aluminum Alloy, Pressure Molded (Aluminum Silicon)AMS4292 (Current)12/16/2002
AMS D Nonferrous Alloys Committee
Steel Tubing (Seamless for Machined Parts) 1.8ni 0.80cr 0.25mo (0.38 - 0.43c) Heat Treated (200,000 Tensile Strength)AMS6420 (Current)12/16/2002
AMS E Carbon and Low Alloy Steels Committee
Pressure Testing, Hydraulic, 1380 KpaMAM2616C (Current)11/28/2001
This specification provides requirements and procedures for hydraulic-pressure leak testing of parts.
AMS B Finishes Processes and Fluids Committee
Titanium Alloy, Bars and Forgings, 11sn 5.0zr 2.3al 1.0mo 0.21si, Solution and Precipitation Heat TreatedAMS4974D (Current)7/23/2002
This specification covers a titanium alloy in the form of bars, wire, forgings, and forging stock.
AMS G Titanium and Refractory Metals Committee
Cloth, Nylon, Polyurethane Coated Thermally, Radio Frequency, or Ultrasonically SealableAMS3272B (Current)8/25/2011
This specification and its supplementary detail specifications cover a woven nylon cloth coated with polyether (EU) urethane.
AMS P Polymeric Materials Committee
Tubing, Plastic, Extra Flexible, Convoluted, Polytetrafluoroethylene, Close ConvolutionAMST81914/2A (Current)3/16/2011
Scope is unavailable.
AE-8C1 Connectors Committee
NICKEL SHEET AND STRIP, CORROSION AND HEAT RESISTANT Thoria Dispersion Strengthened 2.2ThO2AMS5865B (Current)8/15/2011
This specification covers thoria-dispersion-strengthened nickel in the form of sheet and strip.
AMS F Corrosion and Heat Resistant Alloys Committee
Cloth, Nylon, Polyurethane Coated Plain Weave, 6.0 ounces/square yard (200 g/m2)AMS3272/1B (Current)8/25/2011
This specification covers a woven nylon cloth coated with polyether (EU) urethane.
AMS P Polymeric Materials Committee
Shims, Filled Resin Compound Liquid PrecatalyzedAMS3726/3B (Current)8/25/2011
This specification covers a filled, resinous, thermosetting, precatalyzed, liquid compound capable of being applied and cured in place between the surfaces of mechanically fastened (joined) structures.
AMS P Polymeric Materials Committee
ETHYLENE TETRAFLUOROETHYLENE MOLDINGS Stress-RelievedAMS3534A (Current)8/9/2011
This specification covers a melt-processible, copolymer resin of ethylene and tetrafluoroethylene (ETFE) in the form of molded rods, tubes, and shapes.
AMS P Polymeric Materials Committee
ETHYLENE TETRAFLUOROETHYLENE EXTRUSIONSAMS3533A (Current)8/9/2011
This specification covers a melt-processible, copolymer resin of ethylene and tetrafluoroethylene (ETFE) in the form of extruded rods, tubes, and shapes.
AMS P Polymeric Materials Committee
Steel Sheet and Strip, Corrosion and Heat Resistant 20cr 9ni 1.6mo 1.4w 0.58ti Hot Rolled and Stress Relieved, 125,000 PsiAMS5539 (Current)12/16/2002
AMS F Corrosion and Heat Resistant Alloys Committee
ALUMINUM ALLOY WELDING WIRE 7.0Si - 0.52Mg (357.0)AMS4188/5 (Current)12/16/2002
This specification covers an aluminum alloy in the form of extruded or drawn welding wire.
AMS D Nonferrous Alloys Committee
Rubber, Cellular, Chemically BlownAMSR6130A (Current)9/1/2001
This specification establishes requirements for chemically blown cellular rubber.
AMS CE Elastomers Committee
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