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 |
|---|---|
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| Scope is unavailable. | |
| Technical Standard | |
| The exhaust gas temperature instruments covered by this standard are of the electrical servo null balance type, actuated by a varying emf output of one or more parallel connected Chromel-Alumel... | |
| The requirements contained herein are intended for those standards that are promulgated by national standards organizations and used in the aerospace industry. These technical data include narrative text, tables and... | |
| This Aeronautical 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... | |
| This Aeronautical Standard covers the basic type of maximum allowable airspeed indicators used to indicate continuously both the indicated airspeed and the maximum allowable airspeed in the ranges shown below; | |
| This Aeronautical Standard covers the basic types of maximum allowable airspeed instruments which give a continuous indication of both indicated airspeed and maximum allowable airspeed not exceeding 650 knots. | |
| 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 basic types of temperature indicators as follows: TYPE I - Ratiometer type actuated by changes of electrical resistance of a temperature sensing electrical resistance element; | |
| This Aeronautical Standard covers two basic types of temperature instruments as follows: | |
| This Aerospace Standard (AS) defines the requirements for polytetrafluoroethyl ene (PTFE) heavy duty hose assemblies suitable for use in aircraft and missile hydraulic fluid systems service to 8000 psi and... | |
| This Aerospace Standard covers an air data computer characterized by the concept of transducing and computing the majority of air data requirements for an aircraft. The display instruments and other... | |
| This Aerospace 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... | |
| This Aerospace Standard covers four basic types of direct reading pressure actuated rate of climb (vertical speed) indicators as follows: Type I - Range 0-2000 feet per minute climb and... | |
| This Aerospace Standard covers one type of maximum-allowable-ai rspeed instrument which gives a continuous indication of both indicated airspeed and maximum allowable airspeed not exceeding 650 knots. | |
| This Aerospace Standard covers tachometer instruments (RPM indicator, 0-110 percent RPM and 0-120 percent RPM indicators and generator) for remote indication of engine speed. | |
| This Aerospace Standard covers the direct reading pressure actuated type mach meter. | |
| This Aerospace Standard covers three basic types of true mass flow indicating instruments. Each may consist of an indicator, transmitter and other auxiliary means such as a power supply or... | |
| This Aerospace Standard covers two basic types of temperature instruments as follows: TYPE I: Ratiometer type, actuated by changes in electrical resistance of a temperature sensing electrical resistance element; the... | |
| This Aerospace Standard covers two basic types of temperature instruments as follows: | |
| This Aerospace Standard covers two types of compensated altimeters which indicate, by visual means, the pressure altitude compensated for the static pressure system errors of the aircraft. | |
| This aerospace test standard establishes the requirements and procedures for evaluating and comparing the impulse fatigue performance of high pressure hydraulic fittings and tubing. This test method may be used... | |
| This document covers the requirements for insulated, single-conductor, electric wires with tin-coated, silver-coated, or nickel-coated conductors of copper or copper alloy as specified in an applicable generated performance sheet (see... | |
| This document covers the requirements for insulated, single-conductor, electric wires with tin-coated, silver-coated, or nickel-coated conductors of copper or copper alloy as specified in the applicable performance sheet (see Appendix... | |
| This document defines the method for voltage identification by the use of color-coded insulators at the base of the lamp. Table 1 shows the design volts and corresponding insulator colors. | |
| This document defines the method for voltage identification by use of color coded insulators at the base of the lamp. Table 1 shows lamp part numbers and corresponding insulator colors. | |
| This document establishes requirements, test procedures, and acceptance criteria for the fire testing of fluid handling components and materials used in aircraft fluid systems. It is applicable to fluid handling... | |
| This document establishes techniques for validating that a mission store complies with the interface requirements contained in MIL-STD-1760 Revision D. | |
| This document establishes techniques for validating that a mission store complies with the interface requirements delineated in MIL-STD-1760. | |
| This document specifies that black is the only color that can be used for the insulator at the bottom of the base of T-1 and T-1 \u00be Flanged Base lamps. | |
| This drawing specifies parts 6AS43003-914, AS43003-901, AS43003-902, AS43003-903, AS43003-904, AS43003-905, AS43003-906, AS43003-907, AS43003-908, AS43003-909, AS43003-910, AS43003-911, AS43003-912, AS43003-914, AS43003-918, AS43003-920, AS43003-924, AS43003-928, and AS43003-932. To view suppliers qualified to manufacture... | |
| This drawing specifies parts AS42440, AS42441, AS42442, AS42443, AS42444, AS42445, AS42446, AS42447, AS42448, AS42449, AS42451, AS42452, AS42453, AS42455, and AS42457. To view suppliers qualified to manufacture this part, visit https://ts200.sae-it... | |
| This drawing specifies parts AS42701, AS42702, AS42703, AS42704, AS42705, AS42706, AS42707, AS42708, AS42709, AS42710, AS42711, AS42712, AS42713, AS42714, AS42715, AS42716, AS42717, AS42718, AS42719, AS42720, AS42721, AS42722, AS42723, AS42724, AS42725, AS42726,... | |
| This drawing specifies parts AS42749, AS42750, AS42751, AS42752, AS42753, AS42754, AS42755, AS42756, AS42757, AS42758, AS42759, AS42760, AS42761, AS42762, AS42763, AS42764, AS42765, AS42766, AS42767, AS42768, AS42769, AS42770, AS42771, AS42772, AS42773, AS42774,... | |
| This drawing specifies parts AS42910, AS42911, AS42912, AS42913, AS42914, and AS42915. To view suppliers qualified to manufacture this part, visit https://ts200.sae-it c.org/ . | |
| This drawing specifies parts AS42951-009, AS42951-010, AS42951-011, AS42951-012, AS42951-013, AS42951-014, AS42951-015, AS42951-016, AS42951-017, AS42951-018, AS42951-019, AS42951-020, AS42951-021, and AS42951-022. To view suppliers qualified to manufacture this part, visit https://ts200.sae-it c.org/... | |
| This drawing specifies parts AS43013-001, AS43013-002, AS43013-003, AS43013-004, AS43013-005, AS43013-006, AS43013-007, AS43013-008, AS43013-009, AS43013-010, AS43013-011, AS43013-012, AS43013-013, AS43013-014, AS43013-015, AS43013-016, AS43013-017, AS43013-018, AS43013-019, AS43013-020, AS43013-021, AS43013-022, AS43013-023, AS43013-024, and AS43013-025. | |
| This drawing specifies parts AS43014-001, AS43014-002, AS43014-003, AS43014-004, AS43014-005, AS43014-006, AS43014-007, AS43014-008, AS43014-009, AS43014-010, AS43014-011, AS43014-012, AS43014-013, AS43014-014, AS43014-015, AS43014-016, AS43014-017, AS43014-018, AS43014-019, AS43014-020, AS43014-021, AS43014-022, AS43014-023, and AS43014-024. To... | |
| This drawing specifies parts AS43205, AS43206, AS43207, AS43208, AS43209, AS43210, AS43211, AS43212, AS43213, AS43214, AS43215, AS43216, AS43217, AS43218, AS43219, AS43220, AS43221, AS43222, AS43223, AS43224, AS43225, AS43226, AS43227, AS43228, AS43229, AS43230,... | |
| This drawing specifies parts AS43306, AS43307, AS43308, AS43309, AS43310, AS43311, AS43312, AS43313, AS43314, AS43315, AS43316, AS43317, AS43318, AS43319, AS43320, AS43321, AS43322, AS43323, AS43324, AS43325, AS43326, AS43327, AS43328, AS43329, AS43330, AS43331,... | |
| This drawing specifies parts AS43407, AS43408, AS43409, AS43410, AS43411, AS43412, AS43413, AS43414, AS43415, AS43416, AS43417, AS43418, AS43419, AS43420, AS43421, AS43422, AS43423, AS43424, AS43425, AS43426, AS43427, AS43428, AS43429, AS43430, AS43431, AS43432,... | |
| This drawing specifies parts AS43508, AS43509, AS43510, AS43511, AS43512, AS43513, AS43514, AS43515, AS43516, AS43517, AS43518, AS43519, AS43520, AS43521, AS43522, AS43523, AS43524, AS43525, AS43526, AS43527, AS43528, AS43529, AS43530, AS43531, AS43532, AS43534,... | |
| This drawing specifies parts AS43605, AS43606, AS43607, AS43608, AS43609, AS43610, AS43611, AS43612, AS43613, AS43614, AS43615, AS43616, AS43617, AS43618, AS43619, AS43620, AS43621, AS43622, AS43623, AS43624, AS43625, AS43626, AS43627, AS43628, AS43629, AS43630,... | |
| This drawing specifies parts AS43706, AS43707, AS43708, AS43709, AS43710, AS43711, AS43712, AS43713, AS43714, AS43715, AS43716, AS43717, AS43718, AS43719, AS43720, AS43721, AS43722, AS43723, AS43724, AS43725, AS43726, AS43727, AS43728, AS43729, AS43730, AS43731,... | |
| This drawing specifies parts AS43807, AS43808, AS43809, AS43810, AS43811, AS43812, AS43813, AS43814, AS43815, AS43816, AS43817, AS43818, AS43819, AS43820, AS43821, AS43822, AS43823, AS43824, AS43825, AS43826, AS43827, AS43828, AS43829, AS43830, AS43831, AS43832,... | |
| This drawing specifies parts AS43908, AS43909, AS43910, AS43911, AS43912, AS43913, AS43914, AS43915, AS43916, AS43917, AS43918, AS43919, AS43920, AS43921, AS43922, AS43923, AS43924, AS43925, AS43926, AS43927, AS43928, AS43929, AS43930, AS43931, AS43932, AS43934,... | |
| This procurement specification covers retaining rings of the spiral wound type with uniform rectangular cross-section, made of a corrosion and heat resistant age hardenable iron base alloy of the type... | |
| This SAE Aerospace Standard (AS) covers 12 point flare nut crowfoot, flare nut wrenches, double end flare nut wrenches, combination box and flare nut wrenches, and ratcheting flare nut wrenches... | |
| This SAE Aerospace Standard (AS) covers 12-point open box end crowfoot, flare nut, double open box end, combination box and open box end, and ratcheting open box end wrenches that... | |
| This SAE Aerospace Standard (AS) covers 6-point and 12-point flare nut crowfoot, flare nut wrenches, double end flare nut wrenches, combination box end and flare nut wrenches, combination open end... | |
| This SAE Aerospace Standard (AS) covers handles and attachments for use with sockets and crowfoot wrenches in aerospace applications involving high torque, limited clearances, and generally clean conditions. This document... | |
| This SAE Aerospace Standard (AS) covers one type of maximum-allowable-ai rspeed instrument which gives a continuous indication of both indicated airspeed and maximum allowable airspeed not exceeding 650 knots. | |
| This SAE Aerospace Standard (AS) covers tachometer instruments (RPM indicator, 0-110 percent RPM and 0-120 percent RPM indicators and generator) for remote indication of engine speed. | |
| This SAE Aerospace Standard (AS) covers three basic types of true mass flow indicating instruments. Each may consist of an indicator, transmitter and other auxiliary means such as a power... | |
| This SAE Aerospace Standard (AS) covers two basic types of temperature instruments as follows: Type I: Ratiometer type, actuated by changes in electrical resistance of a temperature sensing electrical resistance... | |
| This SAE Aerospace Standard (AS) defines interface configurations for the ground air conditioning service connection on commercial transport aircraft. In addition, it defines the clearances required to accommodate the connection... | |
| This SAE Aerospace Standard (AS) defines the nomenclature for surface finishes commonly used for sheet and strip in aerospace material specifications. It is applicable to steel and to iron, nickel,... | |
| This SAE Aerospace Standard (AS) establishes techniques for validating that a mission store complies with the interface requirements delineated in MIL-STD-1760 Revision E. | |
| This SAE Aerospace Standard (AS) establishes the minimum performance standards for equipment used as secondary direct current (DC) electrical power sources in aerospace electric power systems. The purpose of this... | |
| This SAE Aerospace Standard (AS) establishes the minimum performance standards for equipment used as secondary direct current (DC) electrical power sources in aerospace electric power systems. | |
| This SAE Aerospace Standard (AS) provides a method for gas turbine engine performance computer programs to be written using FORTRAN COMMON blocks. If a "function-call application program interface" (API) is... | |
| This SAE Aerospace Standard (AS) provides general information for the interpretation and clarification of engineering drawing requirements relating to the manufacture and inspection of fluid system couplings, tube fittings, and... | |
| This SAE Aerospace Standard (AS) provides minimum design, hole preparation, installation and removal requirements for AS3272, AS3273, MA3274, and MA3275 serrated shank self-locking clinch nuts. This standard is applicable when... | |
| This SAE Aerospace Standard (AS) provides required contours and limits of size of the surfaces of the internal fluid passages of tube fittings for the portions that are not already... | |
| This SAE Aerospace Standard (AS) provides the essential minimum design, installation and removal standard for AS4200 adapter and is applicable when specified on engineering drawings, or in procurement documents. | |
| This SAE Aerospace Standard (AS) provides the essential minimum design, installation, and removal standard for AS4200 adapter and is applicable when specified on engineering drawings or in procurement documents. | |
| This SAE Aerospace Standard(AS) provides general information for the interpretation and clarification ofengineering drawing requirements relating to the manufacture and inspection of fluid system couplings, tube fittings, and hose ends. | |
| This SAE International Standard covers handles and attachments for use with sockets and crowfoot wrenches in aerospace applications involving high torque, limited clearances, and generally clean conditions. This document provides... | |
| This specification covers the requirements for Aircraft Hydraulic, Self-Sealing, Quick Disconnect Couplings for use in 5000 and 8000 lbf/in 2x (gage) lightweight hydraulic systems. | |
| This specification covers the requirements for aircraft hydraulic, self-sealing, quick disconnect couplings for use in 8000 lbf/in 2x (gage) lightweight hydraulic systems. | |
| This specification establishes the requirements for a probe type self-sealing, self-aligning, non-locking coupling intended for aerospace hydraulic and cooling systems. | |
| This specification establishes the requirements for the following types of self-locking nuts: a Wrenching Nuts: i.e., hexagon and double hexagon nuts. b Anchor Nuts: i.e., plate nuts, gang channel nuts,... | |
| This Standard covers air data equipment (hereinafter designated the instrument) which when connected to sources of aircraft electrical power, static pressure, total pressure and outside air temperature (singly or in... | |
| This standard covers stall warning instruments to provide positive warning to the pilot of an impending stall. Stall, as defined for the purpose of this standard, is the minimum steady... | |
| This standard describes test methods for insulated, single conductor, electric wire intended for aerospace applications. Particular requirements for the wire being tested need to be specified in a procurement document... | |
| This Standard is intended to establish preferred abbreviations for use on panels, controls, instruments, displays, placards and markings. The recommendations apply to terms used in the flight deck of transport... | |
| This test plan defines the test requirements for determining that Bus Interface Units (BIUs) meet the requirements of SAE AS4074, Linear Token Passing Multiplex Data Bus. |
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