Technical Standards - SAE Mobilus

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BOLT, MACHINE - DOUBLE HEX, EXTENDED WASHER HD, PD SHANK, CUP WASHER LOCKED, CADMIUM PLATED, STEEL, UNS G87400, 125 KSI MIN, .2500-28 UNJF-3AAS9681C (Current)8/17/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - DOUBLE HEX EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, CORROSION-RESISTANT STEEL (UNS S17400), 140KSI UTS MIN, .3125-24, UNJF-3AAS3169C (Current)8/17/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - DOUBLE HEX EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, AMS5643 (UNS S17400), . 3750-24, UNJF-3AAS3170C (Current)8/17/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - DOUBLE HEX EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, AMS5643 (UNS S17400), .4375-20, UNJF-3AAS3171C (Current)8/17/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - DOUBLE HEX EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, AMS5643 (UNS S17400), 140 KSI, .5000-20, UNJF-3AAS3172C (Current)8/17/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, UNS S66286, 130 KSI, .3125-24 UNJF-3AAS9112D (Current)8/17/2026
E-25 General Standards for Aerospace and Propulsion Systems
Chemical Process Test Specimen MaterialAS2390B (Current)8/17/2026
This standard establishes definitions, guidelines, and requirements governing materials (e.g., alloy and heat-treat condition) allowed for use in chemical process test specimens when requirements call for a generic class of alloy.
AMS B Finishes Processes and Fluids Committee
WIRE, ELECTRICAL, FLUOROPOLYMER-INSULATED CROSSLINKED MODIFIED ETFE, LOW FLUORIDE, LIGHTWEIGHT, 80 MICROINCH SILVER-COATED COPPER, 200 °C, 600 VOLT, ROHSAS22759/48C (Current)8/17/2026
AE-8D Wire and Cable Committee
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, CORROSION AND HEAT RESISTANT STEEL, UNS S66286, UTS 130 KSI MIN, .3750-24 UNJF-3AAS9559F (Current)8/15/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - DOUBLE HEX EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, CORROSION-RESISTANT STEEL (UNS S17400), 140 KSI UTS MIN, .1900-32, UNJF-3AAS3167C (Current)8/15/2026
E-25 General Standards for Aerospace and Propulsion Systems
Standard Test Method for Aerodynamic Acceptance of AMS1424 and AMS1428 Aircraft Deicing/Anti-Icing FluidsAS5900F (Current)8/14/2026
This SAE Aerospace Standard (AS) establishes the aerodynamic flowoff requirements and test procedures for AMS1424 Type I and AMS1428 Type II, III, and IV fluids used to deice and/or anti-ice aircraft. The objective of this standard is to ensure acceptable aerodynamic characteristics of the deicing/anti-icing fluids as they flow off of aircraft lifting and control surfaces during the takeoff ground acceleration and climb. Aerodynamic acceptance of an aircraft ground deicing/anti-icing fluid is based upon the fluid’s boundary layer displacement thickness (BLDT) on a flat plate, measured after experiencing the free stream velocity time history of a representative aircraft takeoff. Acceptability of the fluid is determined by comparing BLDT measurements of the candidate fluid with a datum established from the values of a reference fluid BLDT and the BLDT over the dry (clean) test plate. Testing is carried out in the temperature range at which the fluid, undiluted and diluted, is to be used in aircraft service. NOTE: No additional aerodynamic testing is required for non-glycol fluids at this time. For more information about non-glycol fluids, please refer to AMS1424 and AMS1428.
G-12ADF Aircraft Deicing Fluids
TERMINAL BOARD ASSEMBLY, MOLDED-IN-STUD, ELECTRICAS27212F (Current)8/14/2026
AE-8C2 Terminating Devices and Tooling Committee
CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE (FOR MIL-DTL-28840 CONNECTORS)AS39029/84C (Current)8/14/2026
AE-8C1 Connectors Committee
SCREW, MACHINE - STEEL, DIFFUSED NICKEL-CADMIUM PLATED, DOUBLE HEXAGON EXTENDED WASHER HEAD, UNS K14675, 195 KSI MIN, .1640-36 UNJF-3AAS9207D (Current)8/14/2026
E-25 General Standards for Aerospace and Propulsion Systems
STRIP, MOUNTING, NUT INSULATING, FOR AS27212 TERMINAL BOARDAS33731B (Current)8/14/2026
AE-8C2 Terminating Devices and Tooling Committee
Bearing, Ball, Bellcrank, Antifriction, AirframeAS6038B (Current)8/10/2026
ACBG Rolling Element Bearing Committee
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, NICKEL ALLOY (UNS N07001) 165 KSI MIN, .2500-28 UNJF-3AAS9724F (Current)8/10/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, PD SHANK, CUP WASHER LOCKED, CRES, UNS S66286, 130 KSI MIN, .3750-24 UNJF-3AAS9679D (Current)8/10/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - DOUBLE HEXAGON, EXTENDED WASHER HEAD, CORROSION- AND HEAT-RESISTANT STEEL, UNS S66286, 130 KSI MIN, .4375-20 UNJF-3AAS9560A (Current)8/10/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - DOUBLE HEX EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, AMS5643 (UNS S17400), 140 KSI, .5625-18, UNJF-3AAS3173C (Current)8/10/2026
E-25 General Standards for Aerospace and Propulsion Systems
SCREW, MACHINE - STEEL, DIFFUSED NICKEL-CADMIUM PLATED, DOUBLE HEXAGON EXTENDED WASHER HEAD, DRILLED, UNS K14675, 195 KSI MIN, .1640-36 UNJF-3AAS9216D (Current)8/10/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - DOUBLE HEX, EXTENDED WASHER HD, PD SHANK, CUP WASHER LOCKED, CADMIUM PLATED, STEEL, UNS G87400, 125 KSI MIN, .1900-32 UNJF-3AAS9680C (Current)8/10/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, PD SHANK, AMS4967 (TI 6AL - 4V), .1900-32 UNJF-3AAS9750C (Current)8/10/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, CLOSE TOLERANCE SHANK, UNS S66286, 130 KSI MIN, .1900-32 UNJF-3AAS91101E (Current)8/10/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - STEEL, DIFFUSED NICKEL-CADMIUM PLATED, DOUBLE HEXAGON EXTENDED WASHER HEAD, UNS K14675, 195 KSI MIN, .3125-24 UNJF-3AAS9210D (Current)8/10/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, PD SHANK, CUP WASHER LOCKED, CRES UNS S66286, 130 KSI MIN, .3125-24 UNJF-3AAS9678D (Current)8/10/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, PD SHANK AMS5616, .3125-24 UNJF-3AAS9887B (Current)8/10/2026
E-25 General Standards for Aerospace and Propulsion Systems
ASSEMBLED COUPLING, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, ENVELOPE DIMENSIONSAS5831A (Current)8/7/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Short Flareless Fittings, Installation Procedures and Torque ForAS4700A (Current)8/6/2026
This SAE Aerospace Standard (AS) establishes the standard installation procedures and torque values for the AS short flareless hydraulic tube fittings in sizes -20 and -24, and parts listed in this standard, made from 6A1-4V Titanium, 15-5 PH CRES, and 7075 Aluminum Alloy.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
FITTING, ADAPTER, REDUCER/EXPANDER, FLARED TO BOSSAS934D (Current)7/30/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Valve; Air Relief, Low PressureAS8712A (Current)7/30/2026
This specification covers the requirements for one type of low-pressure relief valve for use in pressurized shipping containers.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
FLANGE PROFILES, V-COUPLING, DESIGN STANDARDAS24563C (Current)7/28/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Hose, Air Duct, Flexible, AircraftAS8796A (Current)7/28/2026
This specification covers lightweight, circular cross-sectional flexible airduct hose, fabricated from laminated fabric reinforced plastics, or laminated fabric reinforced synthetic rubbers, to be used in aircraft air-conditioning and anti-icing systems.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
BEARING, BALL, ANTI-FRICTION, AIRFRAMEAS20218C (Current)7/24/2026
SCOPE IS UNAVAILABLE.
ACBG Rolling Element Bearing Committee
BEARINGS, PLAIN, SELF-LUBRICATING SELF-ALIGNING, HIGH SPEED OSCILLATION -65 TO +160 °FAS81819/1B (Current)7/21/2026
SCOPE IS UNAVAILABLE.
ACBG Plain Bearing Committee
Adapter, Closed-Circuit Fuel Servicing - StandardizationAS6848 (Current)7/21/2026
The Adapter Receiver specified herein has no classification. No distinction is made between commercial or military use.
AE-5C Aviation Ground Fueling Systems Committee
BOLT, MACHINE - DOUBLE HEX EXTENDED WASHER HEAD, DRILLED, CLOSE TOL SHANK, AMS5643 (UNS S17400), 140 KSI, .1900-32 UNJF-3AAS3174C (Current)7/21/2026
E-25 General Standards for Aerospace and Propulsion Systems
CRIMPING TOOLS, TYPE 1, HAND OR POWER ACTUATED, WIRE TERMINATION, PNEUMATIC TOOL FOR AS22520/1 POSITIONERS, CONTACT WIRE BARREL SIZES 12 THRU 20AS22520/29A (Current)7/21/2026
AE-8C2 Terminating Devices and Tooling Committee
Copper-Beryllium Alloy (Copper Alloy Numbers C17500 and C17510), StripAS81021C (Current)7/20/2026
This specification covers the requirements for the acquisition of two alloys of copper-beryllium alloy strip, having higher electrical conductivity than copper-beryllium alloy strip normally used (see 6.1). All sizes of strip are covered by this specification.
AMS D Nonferrous Alloys Committee
Thermal Effectiveness of Sleeve/Tubing/Tape InsulationJ2302_202607 (Current)7/20/2026
This procedure measures the resistance to radiant heat flow of insulating materials in sleeve, tubing, or tape (collectively referred to as “sleeve”) form. The sleeve’s effectiveness (SE) is determined by measuring the difference in surface temperature of a flat black, single-diameter ceramic cylinder with and without the standard diameter sleeve at the specified temperature, position, and distance from the radiant heat source.
Harness Covering Standards Committee
FITTING, ADAPTER, BULKHEAD, EXTERNAL THREAD, BEAM SEAL TO INTEGRAL WELD RINGAS4229D (Current)7/20/2026
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, PD SHANK, STEEL AMS6322, CADMIUM PLATED, .3750-24 UNJF-3AAS9917C (Current)7/20/2026
E-25 General Standards for Aerospace and Propulsion Systems
BOLT, MACHINE - DOUBLE HEXAGON EXTENDED WASHER HEAD, PD SHANK, CUP WASHER LOCKED, CRES, UNS S66286, 130 KSI MIN, .2500-28 UNJF-3AAS9677C (Current)7/17/2026
E-25 General Standards for Aerospace and Propulsion Systems
Lighting, Aircraft Interior, Installation ofAS18276B (Current)7/16/2026
This specification covers the installation of aircraft interior lighting for military aircraft.
A-20C Interior Lighting
Worldwide On-Board Diagnostic Requirements OverviewJ3248_202607 (Current)7/14/2026
This document focuses on the latest in-force regulations. However, in addition to latest information, the report may include historical information. As regulations are superseded, the previous entry will remain to help understand the change in requirements over time. The initial focus of the document includes light-, medium-, and heavy-duty on-road vehicles with all propulsion systems. The document will include information from the United States and Canada, with later publications expanding to other regions. Forecasts for future regulations will not be included in the spreadsheet but be kept in a separate document. The document may be expanded to other types of applications/vehicles as information becomes available.
Vehicle E E System Diagnostic Standards Committee
BEARING, BALL, AIRFRAME, ANTIFRICTION, DOUBLE ROW, HEAVY DUTYAS27644E (Current)7/13/2026
SCOPE IS UNAVAILABLE.
ACBG Rolling Element Bearing Committee
CONNECTOR, RECEPTACLE, ELECTRIC, CRIMP TYPE, JAM NUT MOUNTING, PUSH-PULL, COUPLING, SERIES 2 (CLASS E AND J)AS31441B (Current)7/13/2026
AE-8C1 Connectors Committee
CRIMPING TOOLS, TYPE I, TERMINAL, HAND OR POWER ACTUATED, WIRE TERMINATION, PNEUMATIC TOOL FOR AS22520/7 POSITIONERS, USE FOR WIRE BARREL SIZES 16 AND SMALLERAS22520/49 (Current)7/13/2026
AE-8C2 Terminating Devices and Tooling Committee
Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, Up to 1500 psi and 450 °F, Hydraulic and PneumaticAS1946G (Current)7/13/2026
This SAE Aerospace Standard (AS) defines the requirements for polytetrafluoroethylene (PTFE) lined, metallic reinforced, hose assemblies suitable for use in aerospace hydraulic, fuel, and lubricating oil systems at temperatures between -67 and 450 °F for Class I assemblies, -67 and 275 °F for Class II assemblies, and at nominal pressures up to 1500 psi. The hose assemblies are also suitable for use within the same temperature and pressure limitations in aerospace pneumatic systems where some gaseous diffusion through the wall of the PTFE liner can be tolerated. The use of these hose assemblies in pneumatic storage systems is not recommended. In addition, installations in which the limits specified herein are exceeded, or in which the application is not covered specifically by this standard (for example, oxygen), shall be subject to the approval of the procuring activity.
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
CONNECTOR, RECEPTACLE, ELECTRIC, CRIMP TYPE, WALL MOUNTING FLANGE, PUSH-PULL, COUPLING, SERIES 2 (CLASS E AND J)AS31401B (Current)7/13/2026
AE-8C1 Connectors Committee
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