SAE International Datasheets for Standards and Technical Documents

Standards and technical documents includes standards, codes, regulation, handbooks, manuals, comprehensive guides and other formal publications. Standards, codes, and regulation establish uniform specifications, procedures or technical criteria.
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Product Name Notes
A fault tolerant, real time high speed data communication standard is defined based on a ring topology and the use of a Token passing access method with distributed control. The...
Amendment 1 of AS39029.
Amendment 1 of AS39029/22.
Amendment 1 of AS39029/29A.
Amendment 1 of AS39029/31.
Amendment 1 of AS39029/31A.
Amendment 1 of AS39029/32A.
Amendment 1 of AS39029/35A.
Amendment 1 of AS39029/37.
Amendment 1 of AS39029/44A.
Amendment 1 of AS39029/45A.
Amendment 1 of AS39029/5A.
Amendment 1 of AS39029/69.
Amendment 1 of AS39029/70.
Amendment 1 of AS39029/92.
Amendment 1of AS39029/34A.
Amendment 2 of AS39029/31A.
Gland details are described for rod diameters from 1/4 to 15-1/2 in, inclusive, corresponding to AS568 O-Ring Dash No. sizes -108/-111, -206/-222, -325/-349 and -425/-460.
Gland details are described for rod diameters from 1/4 to 15-1/2 inches, inclusive, corresponding to AS 568 O-Ring Dash No. sizes -108/-111, -206/-222, -325/-349 and -425/-460.
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Technical Standard
This Aeronautical Standard covers Automatic Pilots intended for use on aircraft to automatically operate the aerodynamic controls to maintain flight and/or to provide maneuvering about the three axes through servo...
This Aeronautical Standard covers both direct and repeating type gyroscopically stabilized Bank and Pitch Indicating Instruments.
This Aeronautical Standard covers five basic types of airspeed instruments as follows:
This Aeronautical Standard covers five basic types of airspeed instruments with indication range essentially as follows: TYPE I - 1 revolution TYPE II - 1 revolution (unequal scale) TYPE III...
This Aeronautical Standard covers four (4) basic types of direct indicating instruments as follows: TYPE I - Range 0-2000 feet per minute climb and descent TYPE II - Range 0-3000...
This Aeronautical Standard covers magnetic drag tachometers with or without built-in synchroscopes.
This Aeronautical Standard covers minimum requirements for gyroscopically stabilized Magnetic Direction Instruments for use in aircraft.
This Aeronautical Standard covers the basic type of carbon monoxide detector instrument used to determine toxic concentrations of carbon monoxide by the measurement of heat changes through catalytic oxidation.
This Aeronautical Standard covers the following basic types of fire detection instruments, or combinations thereof, intended for use in protecting aircraft powerplant installation, auxiliary powerplants, combustion heaters and other installations...
This Aeronautical Standard covers two (2) basic types of instruments as follows: TYPE I - Range 35,000 feet. Barometric Pressure. Scale range at least 28.1 - 30.99 inches of mercury...
This Aeronautical Standard covers two basic types as follows: Type I - Air Operated Type II - Electrically Operated
This Aeronautical Standard covers two basic types of fuel, oil and hydraulic pressure instruments as follows: Type I - Direct Indicating Type II - Remote Indicating This Aerospace Standard does...
This Aeronautical Standard covers two basic types of instruments as follows: Type I - Direct Reading Type II - Remote Indicating
This Aeronautical Standard covers two basic types of instruments as follows: Type I - Float Instruments Type II - Capacitance Instruments
This aeronautical standard covers two basic types of instruments as follows: Type I - Pitot Pressure, straight and L-shaped, 12 and 14 volt nominal, 2 wire circuit. Type II -...
This Aeronautical Standard covers two basic types of instruments as follows: Type I - Range 35,000 feet. Barometric Pressure. Scale range at least 28.1 - 30.99 inches of mercury (946...
This Aeronautical Standard covers two basic types of instruments as follows:
This Aeronautical Standard covers two basic types of instruments, or combinations thereof, intended for use in indicating fuel consumption of aircraft engines as follows: TYPE I - Measure rate of...
This aeronautical standard covers two basic types of instruments, or combinations thereof, intended for use in indicating fuel consumption of aircraft engines.
This aeronautical standard covers two basic types of pressure instruments. These are intended for use in measuring fuel, oil or hydraulic pressures as follows: This aeronautical standard does not apply...
This Aerospace Standard (AS) defines the requirements for a heavy duty polytetrafluoroethyl ene (PTFE) lined, metallic reinforced, hose assembly suitable for use in 400 °F (204 °C) 5000 psi (34...
This Aerospace Standard (AS) defines the requirements for a heavy duty polytetrafluoroethyl ene (PTFE) lined, metallic reinforced, hose assembly suitable for use in 400 °F 5000 psi, aircraft and missile...
This Aerospace Standard (AS) defines the test requirements for determining that bus monitors meet the requirements of MIL-STD-1553B, Digital Time Division Command/Response Multiplex Data Bus.
This Aerospace Standard covers three basic types of cargo compartment fire detector instruments.
This Aerospace Standard covers two basic types of fuel, oil and hydraulic Pressure instruments as follows: Type I- Direct Indicating Type II- Remote Indicating This Aerospace Standard does not apply...
This Aerospace Standard covers two basic types of manifold pressure instruments as follows: Type I - Direct Indicating Type II - Remote Indicating
This drawing specifies parts AS41104 and AS41105. To view suppliers qualified to manufacture this part, visit https://ts200.sae-it c.org/ .
This SAE Aerospace Standard (AS) contains a sample test plan for AS15531 or MIL-STD-1553B Remote Terminals (RT) that may serve several different purposes. This document is intended to be contractually...
This SAE Aerospace Standard (AS) covers an alternate gland design for the installation of scraper/ wiper rings in the lower end of landing gear shock struts for the purpose of...
This SAE Aerospace Standard (AS) covers an alternate gland design for the installation of scraper/wiper rings in the lower end of landing gear shock struts for the purpose of contaminant...
This SAE Aerospace Standard (AS) defines cleanliness classes for particulate contamination of hydraulic fluids and includes methods of reporting related data ( Appendix A ). The contamination classes selected are...
This SAE Aerospace Standard (AS) defines cleanliness levels for particulate contamination of hydraulic fluids and includes methods of reporting data relating to the contamination levels. The contamination levels selected are...
This SAE Aerospace Standard (AS) defines contamination classes and levels for particulate contamination of hydraulic fluids and includes methods of reporting related data ( Appendix A ). The contamination levels...
This SAE Aerospace Standard (AS) defines contamination classes and levels for particulate contamination of hydraulic fluids and includes methods of reporting related data ( Appendix A ).
This SAE Aerospace Standard (AS) defines gland details for rod diameters from 1/4 to 15-1/2 in. inclusive corresponding to AS568 O-Ring Dash No. sizes -108/-111, -206/-222, -325/-349 and -425/-460. The...
This SAE Aerospace Standard (AS) defines gland details for scrapers for rod diameters from 1/4 to 15-1/2 inch (6.35 to 393.70 mm) inclusive, corresponding to AS568 O-ring Dash No. sizes...
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...
This SAE Aerospace Standard (AS) defines the requirements for air cycle air conditioning systems used on military air vehicles for cooling, heating, ventilation, and moisture and contamination control. General recommendations...
This SAE Aerospace Standard (AS) establishes the basic requirements for the design, construction and testing of air mode 2.44 m × 2.44 m (8 ft × 8 ft) cross-section containers.
This SAE Aerospace Standard (AS) establishes the basic requirements for the design, construction and testing of air mode 2.44 m X 2.44 m (8 ft X 8 ft) cross-section containers.
This SAE Aerospace Standard (AS) has been prepared by the Ring Implementation Task Group of the SAE AS-2 Committee. It is intended as a companion document to the SAE AS4075...
This SAE Aerospace Standard defines cleanliness levels for particulate contamination of hydraulic fluids and includes methods of reporting data relating to the contamination levels. The contamination levels selected are an...
This SAE Aerospace Standard defines the swaging process and the roller expander qualification requirements for the attachment of tube fitting to tubing used in low pressure systems of aircraft.
This SAE Aerospace Standard establishes the requirements and procedures for Contractile Strain Ratio (CSR) testing of cold-worked and stress-relieved titanium tubing such as Ti-3AI-2.5V tubing per AMS 4944.
This slash sheet specifies the operational parameters and characteristics of a particular implementation of the SAE Linear, Token Passing Bus (LTPB) Interface Unit. This slash sheet defines the following: a...
This specification covers all gyroscopic and servo control types of automatic pilots intended for use on aircraft to operate automatically the control surfaces of the aircraft to maintain a stabilized...
This specification covers anti-friction bearing universal joints for intermittent and continuous operation suitable for use in military applications.
This specification covers instruments intended for use in airplanes to indicate engine manifold absolute pressure.
This specification covers instruments intended for use in airplanes to indicate the fuel, oil or hydraulic pressures.
This specification covers magnetic drag tachometers with or without built-in synchroscopes.
This specification covers minimum requirements for gyroscopically stabilized (or integrated) magnetic direction indicators for use in aircraft.
This specification covers six types of instruments as follows: TYPE I - 30 - 250 miles per hour range TYPE II - 40 - 300 miles per hour range TYPE...
This specification covers six types of instruments as follows:
This specification covers the basic type of instrument for detection of toxic concentrations of carbon monoxide whose operation is based on measurement of heat changes through catalytic oxidation.
This specification covers the following basic types of instruments, or combinations thereof, intended for use in indicating fuel consumption of aircraft engines.
This specification covers the following basic types of instruments, or combinations thereof, intended for use in protecting aircraft power plant installations, auxiliary power plants, combustion heaters and other installation where...
This specification covers the following basic types: Type I - Pitot Pressure, Straight and L-shaped, 12 and 24 volt nominal, 2 wire circuit. Type II - Pitot and Static Pressures,...
This specification covers the general requirements for electrical solenoids used to actuate various devices through the conversion of electrical signals into mechanical motion. These solenoids are of the axial stroke...
This specification covers the general requirements for removable crimp, solderless wrap, and solder type electrical contacts for use in connectors and other electric and electronic components (see 6.1 ) with...
This specification covers the requirements for non-separable, antifriction needle bearings.
This specification covers three basic types of instruments as follows: TYPE I - Air Driven TYPE II - D-C Operated TYPE III - A-C Operated
This specification covers three types as follows: Type I - Range 0 - 2000 feet per minute climb and descent. Type II - Range 0 - 4000 feet per minute...
This specification covers two basic types as follows: Type I - Air Operated. Type II - Electrically Operated.
This specification covers two basic types as follows: Type I - Direct Reading Type II - Remote Indicating
This specification covers two basic types as follows: Type I - Having limited freedom of operation. Type II - Having unlimited freedom of operation.
This specification covers two basic types as follows: Type I Carbon Monoxide Type II Photo-Electric Cell
This specification covers two types as follows:
This specification covers two types of instruments. These instruments are for the purpose of measuring temperature, such as those of oil coolant, carburetor air, free air and cylinder head.
This specification covers: Type I - Float Gages Type II - Capacitance Gages
This specification defines the requirements for A-286 cres T-bolts and eye bolts, with room temperature tensile strength of 160 000 to 190 000 psi, for use with clamps and V-band...
This specification defines the requirements for A-286 cres T-bolts and eye bolts, with room temperature tensile strength of a minimum of 160,000 psi, for use with clamps and V-band couplings...
This specification defines the requirements for A286 cres T-bolts and eye bolts, with room temperature tensile strength of a minimum of 160000 psi, for use with clamps and V-band couplings...
This standard covers flight directors for use on aircraft to indicate to the pilot, by visual means, the correct control application for the operation of an aircraft in accordance with...
This standard covers the requirements for non-separable, airframe anti-friction needle bearings, corrosion resistant and traditional materials, intended for use in flight vehicle control systems, with radial loads. Under Department of...
This standard covers the requirements for non-separable, airframe anti-friction needle bearings, corrosion resistant and traditional materials, intended for use in flight vehicle control systems, with radial loads.
This standard covers the requirements for non-separable, Airframe Anti-friction Needle Bearings, intended for use in flight vehicle control systems, with radial loads.
This standard covers the requirements for non-separable, airframe antifriction needle bearings and corrosion-resistant and traditional materials intended for use in flight vehicle control systems with radial loads.
This standard specifies the characteristics of the SAE Linear Token Passing Bus (LTPB) Interface Unit. The LTPB provides a high reliability, high bandwidth, low latency serial interconnection network suitable for...
This test plan consists of two major sections for testing of MIL-STD-1553B data bus systems: Bus Network and System Integration Tests.
This test plan consists of two major sections for the production testing of bus controllers: Electrical tests and Protocol tests.
This test plan defines the requirements of data bus components which comply with the requirements of MIL-STD-1553B, Digital Time Division Command/Response Multiplex Data Bus.
This test plan is broken into three major sections for the testing of bus controllers Electrical, Protocol and Noise tests.
This test plan is broken into two major sections for the production testing of remote terminals: Electrical and Protocol.

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