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.
Standards and Technical Documents: Learn more
| Product Name | Notes |
|---|---|
| Field of Application This document shall be used in conjunction with: AS6286 Training and Qualification Program for Deicing/Anti-icing of Aircraft on the Ground AS6286/1 Processes including Methods AS6286/2 Equipment AS6286/4... | |
| No scope available. | |
| Procurement specification is principally for defining protection sleeves on a cable or group of electrical/fiber optic wires (wiring bundle). Single wire protection depends on the minimum diameter of the wire. | |
| Scope is unavailable. | |
|
FITTING ASSEMBLY, ELBOW, 45°, AXIALLY SWAGED, FEMALE FLARELESS, HYDRAULIC, UP TO 1500 PSI -- AS6193A
FITTING ASSEMBLY, ELBOW, 90°, AXIALLY SWAGED, FEMALE FLARELESS, HYDRAULIC, UP TO 1500 PSI -- AS6192A
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Technical Standard |
| The AS6224 specification covers environment resistant, permanent insulation repair sleeves for repairing different types of insulation damages of wire or cable jackets in installed applications. The repair sleeve is intended... | |
| The intent of this document is to define the methodology for suspect parts inspection using radiological inspection. The purpose of radiology for suspect counterfeit part inspection is to detect deliberate... | |
| The scope of this document is to: 1 Specify techniques to detect SC parts using electrical testing. 2 Provide various levels of electrical testing that can be used by the... | |
| The verification matrix (VM) in this slash sheet is intended for use to establish compliance to AS6174A. This slash sheet is applicable to AS6174A. Nothing in this slash sheet, however,... | |
| This Aerospace Standard (AS) defines the requirements for a heavy braid polytetrafluoroethyl ene (PTFE) lined, metallic reinforced, hose assembly suitable for use in high temperature, 400 °F, high pressure, 3000... | |
| This Aerospace Standard (AS) defines the requirements for a heavy duty polytetrafluoroethyl ene (PTFE) lined, metallic reinforced, hose assembly suitable for use in high temperature, high pressure, 4000 psi, aircraft... | |
| This Aerospace Standard covers hose assemblies intended for use in aircraft high temperature fluid systems. The specified temperature range is -65°F (-54°C) to +400°F (204°C). Operating pressures are listed in... | |
| This AS establishes minimum requirements for halocarbon clean agent hand-held fire extinguishers carried aboard civil aircraft. The requirements include: design (cylinder, valve, gauge, mounting equipment), performance (firefighting effectiveness - hidden... | |
| This AS establishes minimum requirements for halocarbon clean agent hand-held fire extinguishers carried on board civil aircraft. The requirements include: design (cylinder, valve, gauge, mounting equipment), performance (firefighting effectiveness -... | |
| This document covers the standards of de-icing/anti-icing equipment. In conjunction with the main document and other related slash sheets it will provide guidelines for the proper procedures to deice and... | |
| This document defines a set of standard application layer interfaces called JAUS Environment Sensing Services. JAUS Services provide the means for software entities in an unmanned system or system of... | |
| This document defines a set of standard application layer interfaces called JAUS Manipulator Services. JAUS Services provide the means for software entities in an unmanned system or system of unmanned... | |
| This document defines a set of standard application layer interfaces called JAUS Mission Spooling Services . JAUS Services provide the means for software entities in an unmanned system or system... | |
| This document defines a set of standard application layer interfaces called JAUS Mission Spooling Services. JAUS Services provide the means for software entities in an unmanned system or system of... | |
| This document defines a set of standard application layer interfaces called JAUS Unmanned Ground Vehicle Services . JAUS Services provide the means for software entities in an unmanned system or... | |
| This document defines capabilities and limitations of FTIR spectroscopy as it pertains to counterfeit electronic component detection and suggests possible applications to these ends. Additionally, this document outlines requirements associated... | |
| This document describes an assessment of the effectiveness of a specified test plan used to screen for counterfeit parts. The assessment includes the determination of the types of defects detected... | |
| This document describes the requirements of the following test methods for counterfeit detection of electronic components: a Method A: General EVI, Sample Selection, and Handling b Method B: Detailed EVI,... | |
| This document describes the requirements of the following test methods for counterfeit detection of electronic components: a Method A: General External Visual Inspection (EVI), Sample Selection, and Handling b Method... | |
| This document establishes common industry practices and recommended screening, qualification, and lot acceptance testing of Plastic Encapsulated Microcircuits (PEMs) for use in space application environments. | |
| This document establishes the minimum requirements for ground based aircraft deicing/anti-icing methods and procedures to ensure the safe operation of aircraft during icing conditions on the ground. This document does... | |
| This document establishes the minimum requirements for ground-based aircraft deicing/anti-icing methods and procedures to ensure the safe operation of aircraft during icing conditions on the ground. This document does not... | |
| This document establishes the minimum training and qualification requirements for ground based aircraft deicing/anti-icing methods and procedures. All guidelines referred to herein are applicable only in conjunction with the applicable... | |
| This document establishes the minimum training and qualification requirements for ground-based aircraft deicing/anti-icing methods and procedures. All guidelines referred to herein are applicable only in conjunction with the applicable documents. | |
| This document establishes the requirements for screening, qualification, and lot acceptance testing of Plastic Encapsulated Discrete Semiconductors (PEDS) for use in space application environments. The scope of this document is... | |
| This document shall be used in conjunction with: - AS6286, Training and Qualification Program for Deicing/Anti-icing of Aircraft on the Ground - AS6286/1, Methods - AS6286/3, Fluids - AS6286/4, Weather... | |
| This document shall be used in conjunction with: - AS6286, Training and Qualification Program for Deicing/Anti-icing of Aircraft on the Ground - AS6286/1, Processes Including Methods - AS6286/2, Equipment -... | |
| This document shall be used in conjunction with: AS6286 - Training and Qualification Program for Deicing/Anti-icing of Aircraft on the Ground AS6286/1 - Processes including Methods AS6286/2 - Equipment AS6286/3... | |
| This document shall be used in conjunction with: AS6286 Training and Qualification Program for Deicing/Anti-icing of Aircraft on the Ground AS6286/1 Processes including Methods AS6286/2 Equipment AS6286/4 Weather AS6286/5 Health,... | |
| This document shall be used in conjunction with: AS6286, Training and Qualification Program for Deicing/Anti-icing of Aircraft on the Ground AS6286/2, Equipment AS6286/3, Fluids AS6286/4, Weather AS6286/5, Health, Safety and... | |
| This document shall be used in conjunction with: | |
| This document was prepared by the SAE AS-1A2 Committee to establish techniques for validating the Network Controller (NC) complies with the NC requirements specified in AS5653, Revision B. Note that... | |
| This document was prepared by the SAE AS-1A2 Committee to establish techniques for validating the Network Terminal (NT) complies with the NT requirements specified in AS5653, Revision B. Note that... | |
| This document was prepared by the SAE AS-1A2 Committee to establish techniques for verifying that Network Controllers (NCs), Network Terminals (NTs), switches, cables, and connectors comply with the physical layer... | |
| This drawing specifies parts AS60709, AS60710, AS60711, AS60712, AS60713, AS60714, AS60715, AS60716, AS60717, AS60718, AS60719, AS60720, AS60721, AS60722, AS60723, AS60724, AS60725, AS60726, AS60727, AS60728, AS60729, AS60730, AS60731, AS60732, AS60734, AS60736,... | |
| This drawing specifies parts AS60811, AS60812, AS60813, AS60814, AS60815, AS60816, AS60817, AS60818, AS60819, AS60820, AS60821, AS60822, AS60823, AS60824, AS60825, AS60826, AS60827, AS60828, AS60829, AS60830, AS60831, AS60832, AS60834, AS60836, AS60838, AS60840,... | |
| This drawing specifies parts AS60912, AS60913, AS60914, AS60915, AS60916, AS60917, AS60918, AS60919, AS60920, AS60921, AS60922, AS60923, AS60924, AS60925, AS60926, AS60927, AS60928, AS60929, AS60930, AS60931, AS60932, AS60934, AS60936, AS60938, AS60940, AS60942,... | |
| This drawing specifies parts AS61014, AS61015, AS61016, AS61017, AS61018, AS61019, AS61020, AS61021, AS61022, AS61023, AS61024, AS61025, AS61026, AS61027, AS61028, AS61029, AS61030, AS61031, AS61032, AS61034, AS61036, AS61038, AS61040, AS61042, AS61044, AS61046,... | |
| This drawing specifies parts AS61116, AS61117, AS61118, AS61119, AS61120, AS61121, AS61122, AS61123, AS61124, AS61125, AS61126, AS61127, AS61128, AS61129, AS61130, AS61131, AS61132, AS61134, AS61136, AS61138, AS61140, AS61142, AS61144, AS61146, AS61148, AS61150,... | |
| This drawing specifies parts AS61218, AS61219, AS61220, AS61221, AS61222, AS61223, AS61224, AS61225, AS61226, AS61227, AS61228, AS61229, AS61230, AS61231, AS61232, AS61234, AS61236, AS61238, AS61240, AS61242, AS61244, AS61246, AS61248, AS61250, AS61252, AS61254,... | |
| This drawing specifies parts AS61309, AS61310, AS61311, AS61312, AS61313, AS61314, AS61315, AS61316, AS61317, AS61318, AS61319, AS61320, AS61321, AS61322, AS61323, AS61324, AS61325, AS61326, AS61327, AS61328, AS61329, AS61330, AS61331, AS61332, AS61334, AS61336,... | |
| This drawing specifies parts AS61411, AS61412, AS61413, AS61414, AS61415, AS61416, AS61417, AS61418, AS61419, AS61420, AS61421, AS61422, AS61423, AS61424, AS61425, AS61426, AS61427, AS61428, AS61429, AS61430, AS61431, AS61432, AS61434, AS61436, AS61438, AS61440,... | |
| This drawing specifies parts AS61512, AS61513, AS61514, AS61515, AS61516, AS61517, AS61518, AS61519, AS61520, AS61521, AS61522, AS61523, AS61524, AS61525, AS61526, AS61527, AS61528, AS61529, AS61530, AS61531, AS61532, AS61534, AS61536, AS61538, AS61540, AS61542,... | |
| This drawing specifies parts AS61614, AS61615, AS61616, AS61617, AS61618, AS61619, AS61620, AS61621, AS61622, AS61623, AS61624, AS61625, AS61626, AS61627, AS61628, AS61629, AS61630, AS61631, AS61632, AS61634, AS61636, AS61638, AS61640, AS61642, AS61644, AS61646,... | |
| This drawing specifies parts AS61716, AS61717, AS61718, AS61719, AS61720, AS61721, AS61722, AS61723, AS61724, AS61725, AS61726, AS61727, AS61728, AS61729, AS61730, AS61731, AS61732, AS61734, AS61736, AS61738, AS61740, AS61742, AS61744, AS61746, AS61748, AS61750,... | |
| This drawing specifies parts AS61818, AS61819, AS61820, AS61821, AS61822, AS61823, AS61824, AS61825, AS61826, AS61827, AS61828, AS61829, AS61830, AS61831, AS61832, AS61834, AS61836, AS61838, AS61840, AS61842, AS61844, AS61846, AS61848, AS61850, AS61852, AS61854,... | |
| This drawing specifies parts AS61937, AS61938, AS61939, AS61940, AS61941, AS61942, AS61943, AS61944, AS61945, AS61946, AS61947, AS61948, AS61949, AS61950, AS61951, AS61952, AS61953, AS61954, AS61955, AS61956, AS61957, AS61958, AS61959, AS61960, AS61961, AS61962,... | |
| This drawing specifies parts AS62201, AS62202, AS62203, AS62204, AS62205, AS62206, AS62207, AS62208, AS62209, AS62210, AS62211, AS62212, AS62213, AS62214, AS62215, AS62216, AS62217, AS62218, AS62219, AS62220, AS62221, AS62222, AS62223, AS62224, AS62225, AS62226,... | |
| This drawing specifies parts AS62251, AS62252, AS62253, AS62254, AS62255, AS62256, AS62257, AS62258, AS62259, AS62260, AS62261, AS62262, AS62263, AS62264, AS62265, AS62266, AS62267, AS62268, AS62269, AS62270, AS62271, AS62272, AS62273, AS62274, AS62275, AS62276,... | |
| This drawing specifies parts AS62302, AS62303, AS62307, AS62308, AS62309, AS62310, AS62311, AS62312, AS62314, AS62320, AS62321, AS62324, AS62325, AS62327, AS62328, AS62330, AS62333, AS62338, AS62339, AS62340, AS62341, and AS62342. To view suppliers... | |
| This drawing specifies parts AS62403, AS62404, AS62405, AS62406, AS62407, AS62408, AS62409, AS62410, AS62411, AS62412, AS62413, AS62414, AS62415, AS62416, AS62417, AS62418, AS62419, AS62420, AS62421, AS62422, AS62423, AS62424, AS62425, AS62426, AS62427, AS62428,... | |
| This drawing specifies parts AS62501, AS62502, AS62503, AS62504, AS62505, AS62506, AS62507, AS62508, AS62509, AS62510, AS62511, AS62512, AS62513, AS62514, AS62515, AS62516, AS62517, AS62518, AS62519, AS62520, AS62521, AS62522, AS62523, AS62524, AS62525, AS62526,... | |
| This drawing specifies parts AS62601, AS62602, AS62603, AS62604, AS62605, AS62606, AS62607, AS62608, AS62609, AS62610, AS62611, AS62612, AS62613, AS62614, AS62615, AS62616, AS62617, AS62618, AS62619, AS62620, AS62621, AS62622, AS62623, AS62624, AS62625, AS62626,... | |
| This drawing specifies parts AS62806, AS62807, AS62808, AS62809, AS62810, AS62811, AS62812, AS62813, AS62814, AS62815, AS62816, AS62817, AS62818, AS62819, AS62820, AS62821, AS62822, AS62823, AS62824, AS62825, AS62826, AS62827, AS62828, AS62829, AS62830, AS62831,... | |
| This drawing specifies parts AS62905, AS62906, AS62907, AS62908, AS62909, AS62910, AS62911, AS62912, AS62913, AS62914, AS62915, AS62916, AS62917, AS62918, AS62919, AS62920, AS62921, AS62922, AS62923, AS62924, AS62925, AS62926, AS62927, AS62928, AS62929, AS62930,... | |
| This method outlines the requirements, capabilities, and limitations associated with the application of Design Recovery for the detection of counterfeit electronic parts including: Operator training; Sample preparation; Imaging techniques; Data... | |
| This method standardizes inspection, test procedures and minimum training and certification requirements to detect Suspect/Counterfeit (SC) Electrical, Electronic, and Electromechanical (EEE) components or parts utilizing Delid/Decapsulation Physical Analysis. The methods... | |
| This procedure establishes the instructions to prepare tube ends, install and inspect axially swaged permanent tube fittings qualified to AS6116. This procedure is applicable when specified on the engineering drawing... | |
| This SAE Aerospace Standard (AS) covers the requirements and technical guidance for evaluation of life-cycle cost, productivity, and safety/health factors related to power hand tool selection. It applies approaches to... | |
| This SAE Aerospace Standard (AS) covers ULDs utilized in finding submerged aircraft. Such ULDs are installed within the aircraft in a manner that they are unlikely to become separated during... | |
| This SAE Aerospace Standard (AS) defines a set of standard application layer interfaces called JAUS UMV Services. JAUS Services provide the means for software entities in an unmanned system or... | |
| This SAE Aerospace Standard (AS) defines the minimum performance standard to demonstrate compliance with the regulatory design, test and operational requirements for a Temperature Controlled Container (TCC). | |
| This SAE Aerospace Standard (AS) defines the requirements for a convoluted polytetrafluoroethyl ene (PTFE) lined, metallic reinforced, hose assembly suitable for use in aircraft fluid systems at temperatures of -65... | |
| This SAE Aerospace Standard (AS) defines the requirements for a heavy braid polytetrafluoroethyl ene (PTFE) lined, metallic reinforced, hose assembly suitable for use in high temperature, 400 °F, high pressure,... | |
| This SAE Aerospace Standard (AS) defines the requirements for a heavy duty polytetrafluoroethyl ene (PTFE) lined, metallic reinforced, hose assembly suitable for use in high temperature, high pressure, 4000 psi,... | |
| This SAE Aerospace Standard (AS) defines the requirements for a heavy-duty polytetrafluoroethyl ene (PTFE) lined, metallic reinforced, hose assembly suitable for use in high temperature, high pressure, 4000 psi, aircraft... | |
| This SAE Aerospace Standard (AS) describes cleaning methods for four cleanliness levels of polytetrafluoroethyl ene hose assemblies and rigid tube assemblies for use in aerospace systems. | |
| This SAE Aerospace Standard (AS) documents a common understanding of terms, compliance issues, and occupant injury criteria to facilitate the design and certification of oblique facing passenger seat installations specific... | |
| This SAE Aerospace Standard (AS) documents and establishes common industry practices, and screening and qualification testing, of Plastic Encapsulated Microcircuits (PEMs) for use in military and avionics application environments. | |
| This SAE Aerospace Standard (AS) establishes requirements applicable to metal stock that is ordered and produced in accordance with an Aerospace Material Specification (AMS). Topics include producer requirements, distributor requirements,... | |
| This SAE Aerospace Standard (AS) establishes requirements applicable to metal stock that is ordered and produced in accordance with an SAE Aerospace Material Specification (AMS). Topics include producer requirements, distributor... | |
| This SAE Aerospace Standard (AS) establishes the minimum requirements for ground-based aircraft deicing/anti-icing methods and procedures to ensure the safe operation of aircraft during icing conditions on the ground. This... | |
| This SAE Aerospace Standard (AS) establishes the requirements for externally swaged aluminum tube fittings on aluminum tubing with flareless separable fitting ends for use in hydraulic supply and return aerospace... | |
| This SAE Aerospace Standard (AS) specifies minimum performance standards for Electronic Flight Information System (EFIS) displays that are head-down and intended for use in the flight deck by the flight... | |
| This SAE Aerospace Standard (AS) specifies standardized gland design criteria and dimensions for static face seals for internal pressure and external pressure applications for aerospace hydraulic and pneumatic applications using... | |
| This SAE Aerospace Standard (AS) standardizes inspection and test procedures, workmanship criteria, and minimum training and certification requirements to detect Suspect/Counterfeit (SC) Electrical, Electronic, and Electromechanical (EEE) parts. The requirements... | |
| This SAE Aerospace Standard (AS) standardizes practices to identify reliable sources to procure electrical, electronic, and electromechanical (EEE) parts, assess and mitigate the risk of distributing suspect counterfeit or counterfeit... | |
| This SAE Aerospace Standard standardizes practices to: a identify reliable sources to procure parts, b assess and mitigate risk of distributing fraudulent/counterfe it parts, c control suspect or confirmed fraudulent/counterfe... | |
| This SAE Standard standardizes practices to: a maximize availability of authentic materiel, b procure materiel from reliable sources, c assure authenticity and conformance of procured materiel, including methods such as... | |
| This set of criteria is intended for use by accredited Certification Bodies (CBs) to establish compliance and grant certification to AS6081A. It may also be used by others to assess... | |
| This set of criteria is intended for use by accredited Certification Bodies (CBs) to establish compliance, and grant certification to AS6081, Aerospace Standard; Fraudulent/Counterfe it Electronic Parts; Avoidance, Detection, Mitigation,... | |
| This specification covers definition of landing impact tests which are to be conducted on landing gear assemblies including shock absorbers, suggested instrumentation for the tests and required data of the... | |
| This specification covers general requirements for the installation of sound and thermal insulation in aircraft. | |
| This specification covers heavy braid hose assemblies intended for use in high-temperature, 400°F (204°C), high-pressure, 3000 psi (210 bar) aircraft hydraulic systems, also for use in pneumatic systems which allow... | |
| This specification covers new cylindrical drums to be used as exterior shipping containers (see 6.1 ). | |
| This specification covers one type of fuel pressure transmitter designated MS28005-7. | |
| This specification covers the requirements for flexible shielded electrical conduit for aircraft installations. | |
| This specification covers the requirements for new reusable cylindrical drums consisting of body, cover, gasket, and closing device(s) to be used as interior and exterior shipping containers. | |
| This specification covers the requirements for shielded electrical conduit for aircraft installations. | |
| This specification defines the requirements for heavy duty hose assemblies suitable for use in high temperature, high-pressure, 4000 psi (27,584 kPa), aircraft and missile hydraulic fluid systems. | |
| This specification describes cleaning methods for four cleanliness levels of tetrafluoroethylene hose assemblies for use in aerospace systems. | |
| This standard covers design requirements, performance requirements, and methods of procurement for tools and associated accessories used to cut aerospace vehicle electrical wire and cable. Aerospace vehicle electrical wire has... | |
| This standard covers jacketed multi-conductor copper data cables for aerospace usage. | |
| This standard covers jacketed multi-conductor copper data cables for aerospace use. | |
| This standard defines a generic set of electrical interfaces between a host aircraft ("platform") and an electro-optic/infrar ed (EO/IR) sensor. This includes connectors, cabling, fiber optics, signals, and power. | |
| This standard defines the data interfaces between a host aircraft ("platform") and an Electro-Optic/Infrar ed (EO/IR) sensor. These data interfaces cover various types of data including: imagery, metadata, command, status,... | |
| This standard defines the mechanical interface and specifies provisions for the electrical and environmental connectors between the host aircraft ("platform") and a turreted electro-optic/infrar ed (EO/IR) sensor. | |
| This standard defines the use of data interfaces between a host platform and an electro-optic/infrar ed (EO/IR) system for maintenance and test (M&T) purposes. In particular, this standard defines the... | |
| This standard documents and establishes common industry practices, and screening and qualification testing, of plastic encapsulated discrete semiconductors (PEDs) for use in military and avionics application environments. | |
| This supplement forms a part of Aerospace Standard AS620, HOSE ASSEMBLIES, CONVOLUTED, POLYTETRAFLUOROETHYL ENE, METALLIC REINFORCED, HIGH TEMPERATURE, MEDIUM PRESSURE, AIRCRAFT, and shall be used to identify hose assembly standards... | |
| This supplement forms a part of the Aerospace Standard AS604, Hose Assembly, Polytetrafluoroethyl ene, Metallic Reinforced, 3000 psi, 400 °F, Heavyweight, Hydraulic and Pneumatic, and shall be used to identify... | |
| This supplement forms a part of the Aerospace Standard AS614, Hose Assembly, Polytetrafluoroethyl ene, Metallic Reinforced, 4000 psi, 400 °F, Heavy Duty, Hydraulic and Pneumatic, and shall be used to... | |
| This test method provides stakeholders (runway deicing/anti-icing product manufacturers, users, regulators, and airport authorities) with a relative ice penetration capacity of runway deicing/anti-icing product, by measuring the ice penetration as... | |
| This test method provides stakeholders (runway deicing/anti-icing product manufacturers, users, regulators, and airport authorities) with relative ice melting capacity of runway deicing/anti-icing products, by measuring the amount of ice melted... | |
| This test method provides stakeholders (runway deicing/anti-icing product manufacturers, users, regulators, and airport authorities) with relative ice undercutting capacity of runway deicing/anti-icing products, by measuring the area of ice undercut... | |
| This test method provides the capabilities, limitations, and suggested possible applications of TGA as it pertains to the detection of counterfeit electronic components. Additionally, this document outlines requirements associated with... | |
| Through the use of ultra-high frequency ultrasound, typically above 10 MHz, Acoustic Microscopy (AM) non-destructively finds and characterizes physical features and latent defects (visualization of interior features in a layer... | |
| To define capabilities and limitations of Raman spectroscopy as it pertains to counterfeit detection of EEE parts and suggest possible applications to these ends. Additionally, this document outlines requirements associated... | |
| XRF technique for counterfeit detection is applicable to electrical, electronic and electromechanical (EEE) parts as listed in AS6171 General Requirements. In general, the detection technique is meant for use on... |
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