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Castings, Classification and InspectionAMS2175B (Current)04/25/2024
This specification establishes nondestructive testing methods, sampling frequency, and acceptance criteria for the inspection of metal castingsAMS B Finishes Processes and Fluids Committee
Material Specification
Tape for Organic Coatings Adhesion TestingAMS3721A (Current)04/25/2024
This specification establishes requirements for a tape that is used to perform organic coatings adhesion testingAMS G8 Aerospace Organic Coatings Committee
Material Specification
Aluminum Alloy, Alclad Sheet 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (Alclad 7075-O) Annealed, Fine GrainedAMS4278C (Current)04/25/2024
This specification covers an aluminum alloy in the form of alclad sheet over 0.039 to 0.126 inches (0.99 to 3.20 mm), inclusive, in nominal thickness with a fine-grain core of ASTM No. 6 or finer (see 8.5AMS D Nonferrous Alloys Committee
Material Specification
Aluminum Alloy, Plate (7160-T7651), 7.0Zn - 2.2Cu - 1.5Mg - 0.10Zr, Solution Heat Treated, Stress Relieved, and OveragedAMS4378A (Current)04/25/2024
This specification covers an aluminum alloy in the form of plate 1.000 to 6.000 inches (25.40 to 152.40 mm), inclusive, in nominal thickness (see 8.5AMS D Nonferrous Alloys Committee
Material Specification
Elastomer: Silicone Rubber (MQ/VMQ), General Purpose, 35 - 45 Durometer Type ‘A’ HardnessAMS3301K (Current)04/25/2024
This specification covers a silicone (MQ/VMQ) elastomer that can be used to manufacture product in the form of sheet, strip, tubing, extrusions, and molded shapes. This specification should not be used for molded rings, compression seals, molded O-ring cord, and molded-in-place gaskets for aeronautical and aerospace applicationsAMS CE Elastomers Committee
Material Specification
Titanium Alloy Bars, Forgings and Forging Stock, 6.0Al - 6.0V - 2.0Sn, Solution Heat Treated and AgedAMS6935D (Current)04/25/2024
This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm) in nominal diameter or least distance between parallel sides, inclusive, forgings of thickness up through 4.000 inches (101.60 mm), inclusive, with bars and forgings having a maximum cross-sectional area of 32 square inches (204.46 cm2), and stock for forging of any size (see 8.6AMS G Titanium and Refractory Metals Committee
Material Specification
Aluminum Alloy Sheet, 4.4Cu - 1.5Mg - 0.60Mn (2024; -T4 Flat Sheet), Solution Heat Treated, High FormabilityAMS4297C (Current)04/25/2024
This specification covers an aluminum alloy in the form of sheet 0.020 to 0.128 inch (0.51 to 3.25 mm), inclusive, in nominal thickness (see 8.5AMS D Nonferrous Alloys Committee
Material Specification
Titanium Alloy Bars, Forgings, and Flash-Welded Rings, 5Al - 2.5V - 4Sn - 1Co - 0.8Fe AnnealedAMS6903 (Current)04/25/2024
This specification covers a titanium alloy in the form of bars, forgings, and flash-welded rings up through 12.000 inches (304.80 mm), inclusive, in diameter or least distance between parallel sides, and stock of any size for forging or flash-welded rings. Bars, forgings, and flash-welded rings with a nominal thickness of 3.000 inches (79.20 mm) or greater shall have a maximum cross-sectional area of 113 square inches (729 cm2) (see 8.5AMS G Titanium and Refractory Metals Committee
Material Specification
Aluminum Alloy, Sheet and Plate, Alclad, 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024, -T861 Sheet and Plate), Solution Heat Treated, 6% Cold Worked and Artificially AgedAMS4467C (Current)04/25/2024
This specification covers an aluminum alloy in the form of alclad sheet and plate supplied in the -T861 temperAMS D Nonferrous Alloys Committee
Material Specification
Aluminum Alloy, Coiled Sheet, Alclad, 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024; -T4 Coiled Sheet), Solution Heat TreatedAMS4475C (Current)04/25/2024
This specification covers an aluminum alloy in the form of alclad coiled sheet from 0.010 to 0.128 inch (0.25 to 3.25 mm), inclusive, in thickness supplied in the -T4 temper (see 8.5AMS D Nonferrous Alloys Committee
Material Specification
Aluminum Alloy, Extruded Profiles (2395-T84), 3.95Cu - 1.15Li - 0.3Ag - 0.5Mg - 0.1Zr, Solution Heat Treated, Stress Relieved by Stretching, and AgedAMS4359A (Current)04/25/2024
This specification covers an aluminum alloy in the form of extruded rods, bars, and profiles (shapes) 0.040 to 1.500 inches (1.02 to 38.10 mm), inclusive, in thickness, and produced with maximum cross-sectional area of 23.25 square inches (15000 mm2) and a maximum circumscribing circle diameter (circle size) of 15.5 inches (394 mm) (see 2.4.1 and 8.6AMS D Nonferrous Alloys Committee
Material Specification
Sealing Compound, Integral Fuel Tanks and General Purpose, Intermittent Use to 360 °F (182 °CAMS3276H (Current)04/25/2024
This specification covers fuel-resistant polysulfide (T) sealing compounds supplied as a two-component systemAMS G9 Aerospace Sealing Committee
Material Specification
Titanium Alloy Welding Wire, 5Al - 2.5SnAMS4953J (Current)04/25/2024
This specification covers a titanium alloy in the form of welding wire (see 8.5AMS G Titanium and Refractory Metals Committee
Material Specification
Aluminum Alloy, Sheet and Plate, 2.5Mg - 0.25Cr (5052-H32), Strain Hardened, Quarter-Hard, and StabilizedAMS4016N (Current)04/25/2024
This specification covers an aluminum alloy in the form of sheet and plate 0.017 to 2.000 inches (0.43 to 50.80 mm), inclusive, in nominal thickness (see 8.6AMS D Nonferrous Alloys Committee
Material Specification
Clamp - Tube Support, Spring Clips and PTFE Cushion, Procurement SpecificationMA3399A (Current)04/24/2024
This procurement specification covers the requirements for metal tube support clamps comprising of two spring clips made of corrosion and heat resistant steel and the associated PTFE single split cushion that supports the tube. See Figure 1G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Technical Standard
BOLT, TEE HEAD - NICKEL ALLOY (UNS N07718), CHAMFERED, .3125-24 UNJF-3A (STRESS RUPTURE RESISTANTAS3411E (Current)04/24/2024
E-25 General Standards for Aerospace and Propulsion Systems
Technical Standard
BOLT, MACHINE - DOUBLE HEX EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, AMS5643 (UNS S17400), . 3750-24, UNJF-3AAS3170B (Current)04/24/2024
E-25 General Standards for Aerospace and Propulsion Systems
Technical Standard
Plain Spherical Bearing Conformity ExaminationARP5448/6A (Current)04/24/2024
This method outlines a standard procedure for performing conformity tests of bearings utilizing liners of bonded polytetrafluoroethylene (PTFE). The data from these tests shall be used to determine if the product meets the conformity requirements of the applicable specificationACBG Plain Bearing Committee
Recommended Practice
Liquid Leak Tightness Evaluation Methodology for EV Battery Packs Informational ReportJ3277_202404 (Current)04/23/2024
This technical information report (IR) presents a methodology to evaluate battery pack liquid leak tightness attributes to be used in a production line to satisfy the functional requirement for IPX7, water ingress requirement, and no sustainable coolant leakage for coolant circuits. The Equivalent Channel Method is used as a suggested production leak tightness requirement for a given battery pack design that will correlate and assure that the battery pack meets or exceeds its functional requirement. Obtaining the specific geometry of the Equivalent Channel (EC) for a given battery pack is done analytically and empirically in consideration of the product design limitations. This document is a precursor to J3277-1, which will present the practices to qualify that product leak tightness is equal or better than the maximum allowed EC for that product using applicable and commercially available leak test technologies. This document may be applied to EV and HEV battery packs as tested duringBattery Standards Testing Committee
Information Report
Rivets, UNS S66286, Steel, Corrosion and Heat Resistant, 80 ksi Shear Strength, Procurement SpecificationAS7235A (Current)04/23/2024
This procurement specification covers solid rivets and hollow end rivets made from a corrosion and heat resistant steel of the type identified under the Unified Numbering System as UNS S66286 and of 80 ksi single shear strength at room temperatureE-25 General Standards for Aerospace and Propulsion Systems
Technical Standard
Off-Road Self-Propelled Work Machines Operator Enclosure Environment Part 1: Terms and DefinitionsJ3078/1_202404 (Current)04/23/2024
SAE J3078 provides test methods and criteria for the evaluation of the operator enclosure environment in earth-moving machinery as defined in ISO 6165. SAE J3078/1 gives the terms and definitions which are used in other parts of SAE J3078. It is applicable to Off-Road Self-Propelled Work Machines as defined in SAE J1116 and tractors and machinery for agriculture and forestry as defined in ANSI/ASAE S390HFTC6, Operator Accommodation
Recommended Practice
PIN, STRAIGHT, HEADED, .0937 DIAMETER, UNS S41800AS9842B (Current)04/23/2024
E-25 General Standards for Aerospace and Propulsion Systems
Technical Standard
NUT, PLAIN, HEXAGON, CADMIUM PLATED, UNS G87400, 125 KSI MINAS9881C (Current)04/23/2024
E-25 General Standards for Aerospace and Propulsion Systems
Technical Standard
Rivets, Solid, UNS N04400, Corrosion Resistant 67Ni - 31Cu Procurement SpecificationAS7233A (Current)04/23/2024
This procurement specification covers aircraft-quality solid rivets made from a corrosion resistant nickel-copper alloy of the type identified under the Unified Numbering System as UNS N04400 and of 46 ksi minimum shear strengthE-25 General Standards for Aerospace and Propulsion Systems
Technical Standard
Aerospace Hydraulic and Pneumatic Specifications, Standards, Recommended Practices, and Information ReportsAIR737G (Current)04/23/2024
This SAE Aerospace Information Report (AIR) lists military and industry specifications, standards, recommended practices, and information reports applicable to aerospace hydraulic and pneumatic systems and componentsA-6 Aerospace Actuation, Control and Fluid Power Systems
Information Report
Fuel Flow Rate Measurement SystemAS407E (Current)04/23/2024
This SAE Aerospace Standard (AS) defines minimum performance standards (MPS) for fuel flowmeters, fuel flow indicators, and fuel flow transmitters. The fuel flow indicators and transmitters are intended for use in 14 CFR Part 23, 25, 27, and 29 aircraft equipped with reciprocating and turbine engines. Multiple function displays are not within the scope of this SAE Aerospace Standard (refer to AS6296A-4FLW Fuel Flowmeters
Technical Standard
Flareless Hydraulic Tube FittingsJ514/2_202404 (Current)04/23/2024
This SAE Standard covers complete general and dimensional specifications for flareless type of hydraulic tube fittings. These fittings are intended for general application in hydraulic systems on industrial equipment and commercial products. These fittings are capable of providing leakproof, full flow connections in hydraulic systems operating at working pressures as specified in Table 1. For any application, it is recommended that sufficient testing be conducted and reviewed by both the user and fitting manufacturer to assure that performance levels will be safe and satisfactory. Formerly, SAE J514 was organized as a single document with ten clauses, which included six sections. This revision of SAE J514 has been organized into three sections as follows: Part 1: 37-degree flared fittings Part 2: Flareless (bite type) fittings Part 3: NPTF pipe fittings and pipe unions It is important to note that this and all SAE J-documents are intended for ground vehicle use only and not intendedHydraulic Tube Fittings Committee
Technical Standard
BEARING, BALL, AIRFRAME, ANTI-FRICTION, EXTRA LIGHT DUTY, CORROSION RESISTANT NITROGEN STEEL (CRENAS27646/1B (Current)04/23/2024
ACBG Rolling Element Bearing Committee
Technical Standard
Rivets, Blind, Corrosion Resistant Alloy 67Ni - 31Cu Procurement SpecificationAS7234A (Current)04/23/2024
This procurement specification covers tubular, blind rivets fabricated from a corrosion resistant nickel-copper alloy of the type identified under the Unified Numbering System as UNS N04405, and of 52 ksi minimum shear strength for self-plugging style rivetsE-25 General Standards for Aerospace and Propulsion Systems
Technical Standard
Tire Burst Test MethodologyARP6265 (Current)04/17/2024
This document describes a recommended test procedure to assess the burst characteristics of tires used on 14CFR Part 25 or similar transport airplanesA-5C Aircraft Tires Committee
Recommended Practice
Aircraft New Tire Standard - Bias and RadialAS4833A (Current)04/17/2024
This SAE Aerospace Standard (AS) sets forth criteria for the selection and verification processes to be followed in providing tires that will be suitable for intended use on civil aircraft. This document encompasses new and requalified radial and bias aircraft tiresA-5C Aircraft Tires Committee
Technical Standard
Aerospace - Accumulator, Hydraulic, Cylindrical, Piston SeparatedARP4379B (Current)04/15/2024
This SAE Aerospace Recommended Practice (ARP) is a guide for defining the requirements for aerospace piston hydraulic accumulators, including details pertinent to the design, fabrication, performance and testing of the accumulator. This type of accumulator contains a piston which separates pressurized gas and fluidA-6C4 Power Sources Committee
Recommended Practice
Fuel and Lubricant Tanks for MotorcyclesJ1241_202404 (Current)04/15/2024
This SAE Recommended Practice is applicable to two- or three-wheel motorcycles intended for highway use. Unless noted, requirements apply to both metallic and nonmetallic tanks. Accessory or aftermarket tanks as well as original equipment tanks are coveredMotorcycle Technical Steering Committee
Recommended Practice
J1939 Digital AnnexJ1939DA_202404 (Current)04/10/2024
This document is intended to supplement the SAE J1939 documents by offering the SAE J1939 information in a form that can be sorted and search for easier useTruck Bus Control and Communications Network Committee
Supplement
Steel, Corrosion-Resistant, Sheet and Strip 18Cr - 8Ni (301) Cold Rolled, 125 ksi (862 MPa) Tensile StrengthAMS5517N (Current)04/10/2024
This specification covers a corrosion-resistant steel in the form of sheet and strip 0.005 inch (0.13 mm) and over in nominal thicknessAMS F Corrosion and Heat Resistant Alloys Committee
Material Specification
CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, 45° SELF-LOCKING AND NON-SELF-LOCKING, CATEGORY 4C (FOR MIL-DTL-38999 SERIES III AND IV CONNECTORSAS85049/125A (Current)04/10/2024
AE-8C1 Connectors Committee
Technical Standard
BOLT, MACHINE - HEXAGON HEAD, PD SHANK, CORROSION AND HEAT RESISTANT STEEL UNS S66286, .5000-20 UNJF-3AAS3104B (Current)04/10/2024
E-25 General Standards for Aerospace and Propulsion Systems
Technical Standard
CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE (FOR AS81659 SERIES 2 CONNECTORSAS39029/12D (Current)04/10/2024
AE-8C1 Connectors Committee
Technical Standard
CLAMP, LOOP TYPE, CUSHIONED SUPPORTAS21919C (Current)04/10/2024
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Technical Standard
HOSE ASSEMBLY, CONVOLUTED, PTFE, METALLIC REINFORCED, LOW PRESSURE, CONDUCTIVE, FLARELESS, STRAIGHT TO STRAIGHTAS6996 (Current)04/10/2024
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Technical Standard
SCREW, MACHINE - HEXAGON HEAD, PD SHANK, CRES AMS5731 (UNS S66286), .164-36 UNJF-3AAS3098A (Current)04/10/2024
E-25 General Standards for Aerospace and Propulsion Systems
Technical Standard
Bolts, Screws, and Studs, Geometric Control RequirementsAS3063C (Current)04/10/2024
This SAE Aerospace Standard (AS) establishes the geometric control requirements for bolts, screws, and studs where worded notes and symbolized notes are used for straightness, concentricity, squareness, and runoutE-25 General Standards for Aerospace and Propulsion Systems
Technical Standard
Steel, Corrosion- and Heat-Resistant, Bars, Wire, Forgings, Mechanical Tubing, and Stock for Forging and Heading, 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V (Alloy A286), Consumable Electrode Remelted, 1650 °F (899 °C) Solution Heat TreatedAMS5734L (Current)04/10/2024
This specification covers a corrosion- and heat-resistant steel in the form of bars, wire, forgings, mechanical tubing up to 5.00 inches (127 mm), inclusive, in nominal diameter or least distance between parallel sides (thickness), and stock for forging or headingAMS F Corrosion and Heat Resistant Alloys Committee
Material Specification
Steel, Bars, Forgings, Mechanical Tubing and Forging Stock, 2.7Si - 0.85Cr - 1.8Ni - 0.4Mo - 0.2V - (0.37 - 0.44C) Premium Aircraft Quality, Double Vacuum MeltedAMS6499C (Current)04/10/2024
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stockAMS E Carbon and Low Alloy Steels Committee
Material Specification
Copper Alloy, Brazing Filler Metal, 52.5Cu - 38Mn - 9.5Ni, 1615 to 1700 °F (879 to 927 °C) Solidus-Liquidus RangeAMS4764H (Current)04/10/2024
This specification covers a copper alloy in the form of wire, rod, sheet, strip, foil, and powder and a viscous mixture (paste) of powder in a suitable binder (see 8.6AMS D Nonferrous Alloys Committee
Material Specification
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, DRILLED, PD SHANK, NICKEL ALLOY, UNS N07718, 185 KSI MIN, .4375-20 UNJF-3AAS3247D (Current)04/10/2024
E-25 General Standards for Aerospace and Propulsion Systems
Technical Standard
PIN AND PLUG, EXPANSION, SET OF PARTS AL ALLOY 2024-T4 AND 2024-T351, SHORT; STD AND .010 OVERSIZE DIAMETERS, UNS A92024AS3588B (Current)04/10/2024
E-25 General Standards for Aerospace and Propulsion Systems
Technical Standard
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, DRILLED, PD SHANK, SILVER PLATED, NICKEL ALLOY, UNS N07718, 185 KSI MIN, .1900-32 UNJF-3AAS3250D (Current)04/10/2024
E-25 General Standards for Aerospace and Propulsion Systems
Technical Standard
NUT, SELF-LOCKING, DOUBLE HEXAGON, REDUCED ENVELOPE, UNS S66286 SILVER PLATED THREADS ONLYAS3625B (Current)04/10/2024
E-25 General Standards for Aerospace and Propulsion Systems
Technical Standard
NUT, PLAIN, CASTELLATED, HEXAGON - UNS S66286, 130 KSI MINAS9358B (Current)04/10/2024
E-25 General Standards for Aerospace and Propulsion Systems
Technical Standard
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