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
Amendment 1 of 81044/6
Amendment 1 of AS7928.
Amendment 1 of AS7928/1A.
Amendment 1 of AS7928/2A.
Amendment 1 of AS7928A.
Amendment 1 of AS7974.
Amendment 1 of AS81044.
Amendment 1 of AS81044/5
Amendment 1 of AS81044/7
Amendment 1 of AS81044/8.
Amendment 1 of AS81044/9
Amendment 1 of AS81582.
Amendment 1 of AS81582_2.
Amendment 1 of AS81659.
Amendment 1 of AS81659/71.
Amendment 1 of AS81703.
Amendment 2 of AS81044.
Amendment 2 of AS81582.
Amendment A2 of AS81659.
AS7928 includes insulated and uninsulated crimp-style copper lug terminals and conductor splices for stranded conductors.
AS81044 covers single conductor electric wires made as specified in the applicable detail specification with tin-coated, silver-coated, or nickel-coated copper or copper alloy conductors insulated with crosslinked polyalkene, crosslinked alkane-imide...
No scope available. An Amendment corresponding to this standard is available at AS7928_4_A1
No scope available.
Technical Standard
The AS8050 master document contains general information for qualification of aerospace fiber optic, circular, modular, and rectangular connectors as part of a fiber optic interconnect assembly comprising of a connector,...
The Nickel Cadmium battery covered by this Aerospace Standard is the type which is generally, although not exclusively, used for engine starting purposes in turbine-powered aircraft and/or on aircraft with...
The tests specified herein provide a laboratory means to determine the performance characteristics of static electric power inverters under electrical and environmental conditions representative of those encountered in actual aeronautical...
This Aerospace Standard (AS) covers the general minimum performance standards for generators/starter-g enerators and associated voltage regulators for use in direct current (DC) electric systems for civil aircraft.
This Aerospace Standard (AS) covers the general minimum performance standards of A-C generators and associated regulators for civil aircraft. The generator is a nominal 120/208-volt, 400-Hz, 3-phase, Y-connected system that...
This Aerospace Standard (AS) defines minimum performance standards, qualification requirements, and minimum documentation requirements for passenger and crew seats in civil rotorcraft and transport airplanes. The goal is to achieve...
This aerospace standard (AS) defines the requirements of portable protective breathing equipment for use during smoke/fire conditions on board an aircraft.
This Aerospace Standard (AS) specifies minimum performance requirements for primary pressure altimeter systems other than air data computers. This AS covers altimeter systems that measure and display altitude as a...
This Aerospace Standard (AS), establishes minimum performance standards for those sensors, computers, transponders, and airplane flight deck controls/displays which together comprise a Takeoff Performance Monitor (TOPM) System. This standard also...
This Aerospace Standard covers all automatic pressure altitude code generating equipment manufactured under this standard and complying with the requirements specified herein up to the maximum range of pressure altitude...
This Aerospace Standard covers Flight Director Equipments which display to the pilot a computed command for the operation of an aircraft in accordance with selected Mode(s). The term "Equipment" may...
This Aerospace Standard covers two basic Stall Warning Systems, one measures air flow and pressure distribution on the airfoil and the other measures the angle of airflow with respect to...
This Aerospace Standard defines minimum light intensity in terms of candelas in vertical and horizontal-direction s about the longitudinal, vertical and lateral axes of the aircraft. It also defines color...
This Aerospace Standard specifies laboratory test procedures and minimal requirements for the manufacturer of torso restraint systems for use in small fixed wing aircraft and rotorcraft. It is intended to...
This Aerospace Standard will define minimum light intensity in terms of "effective intensity" as defined in paragraph 3.5 of this standard and specified vertical and horizontal directions about the longitudinal...
This AS covers all types of electronic display systems, as qualified in "Purpose", both panel mounted (head down) and electro-optical (head up), monochromatic and color which are used in the...
This AS covers any protective system which serves the stated purpose.
This AS covers subsonic and supersonic Mach Meter instruments which, when connected to sources of static (Ps), and total (Pt), or impact (Pt-Ps), pressure provide indication of Mach number. These...
This AS covers ULD utilized in finding flight data recorders, cockpit voice recorders or aircraft. Such ULDs are installed adjacent to the recorders in a manner that they are unlikely...
This AS covers Underwater Locating Devices (ULD) to assist in finding flight recorders, cockpit recorders or aircraft or both. Such ULDs are to be installed adjacent to the recorders in...
This AS covers Vertical Velocity Instruments which display the rate of change of pressure altitude of an aircraft, as follows: Type A - Direct reading, self-contained, pressure actuated Type B...
This AS covers Vertical Velocity Instruments which display the rate of change of pressure altitude of an aircraft, as follows:
This AS defines components in "Capacitance Sensor" and "Non-Capacitance Sensor" type Fuel and Oil Quantity Indicating Systems. "Non-Capacitance" systems may employ any measurement technique current in the art including, but...
This AS defines instruments which use inputs of static and pitot pressure equal to those which are utilized to establish the pressure altitude and speed of that aircraft. These pressures...
This document applies to the development of Plans for integrating and managing electronic materials and processes for equipment in the military and commercial aerospace markets; as well as other ADHP...
This document defines a set of standard application layer interfaces called JAUS Autonomous Capabilities Services . JAUS Services provide the means for software entities in an unmanned system or system...
This document defines the minimum degree of purity and maximum levels of certain deleterious impurities allowable for aviator's breathing oxygen at the point of manufacture or generation. It covers gaseous,...
This document defines the minimum degree of purity for aviator's breathing oxygen at the point of manufacture. It covers gaseous, liquid, and chemically generated oxygen.
This document defines the minimum performance levels that are required for electrical wire used in civil aircraft.
This document defines the minimum performance standards for personnel parachute assemblies to be carried in aircraft or worn by passengers, crew, or parachutists for emergency use. This document covers three...
This document establishes the minimum requirements for design and qualification of equipment identified as Gyroscopically Stabilized Magnetic Direction Instruments.
This document establishes the minimum requirements for design and qualification of equipment identified as Gyroscopically Stabilized Non-Magnetic Direction Instruments.
This SAE Aerospace Standard (AS) applies to a personal, portable oxygen concentrator (POC) to be supplied and used by a passenger requiring supplemental oxygen therapy while traveling on board civil,...
This SAE Aerospace Standard (AS) applies to all temperature instruments used in aircraft applications and environments. The word "instrument" as used in this Standard encompasses only the display device and...
This SAE Aerospace Standard (AS) covers air data computer equipment (hereinafter designated the computer) which when connected to sources of aircraft electrical power, static pressure, total pressure, outside air temperature,...
This SAE Aerospace Standard (AS) covers any protective system that serves the stated purpose.
This SAE Aerospace Standard (AS) covers combustion heaters and accessories used in, but not limited to, the following applications: a Cabin heating (all occupied regions and windshield heating) b Wing...
This SAE Aerospace Standard (AS) covers combustion heaters used in the following applications: a Cabin heating (all occupied regions and windshield heating) b Wing and empennage anti-icing c Engine and...
This SAE Aerospace Standard (AS) covers internal combustion heat exchanger type heaters used in the following applications: a Cabin heating (all occupied regions and windshield heating) b Wing and empennage...
This SAE Aerospace Standard (AS) covers the following basic types: Type I - Pitot pressure, straight and L-shaped, electrically heated. Type II - Pitot and static pressures, straight and L-shaped,...
This SAE Aerospace Standard (AS) defines and clarifies terms used in aerospace materials and process specifications, standards, and recommended practices.
This SAE Aerospace Standard (AS) defines Minimum Performance Standards (MPS), qualification requirements, and minimum documentation requirements for side-facing seats in civil rotorcraft, transport aircraft, and general aviation aircraft. The goal...
This SAE Aerospace Standard (AS) defines minimum performance standards, qualification requirements, and minimum documentation requirements for passenger and crew seats in civil rotorcraft, transport aircraft, and general aviation aircraft. The...
This SAE Aerospace Standard (AS) defines the performance requirements for equipment to be used by untrained cabin occupants for protection from toxic and irritant atmospheres while on board and during...
This SAE Aerospace Standard (AS) establishes minimum design and performance requirements for carts, containers and associated components intended for installation in galleys and other areas of transport category airplanes. The...
This SAE Aerospace Standard (AS) establishes minimum design and performance requirements for galley insert equipment with an electrical and/or pressure system, as well as associated components intended for installation in...
This SAE Aerospace Standard (AS) establishes minimum performance standards for new equipment anticollision light systems. This Aerospace Standard defines minimum light intensity in terms of "effective intensity" as defined in...
This SAE Aerospace Standard (AS) establishes minimum performance standards for new equipment position lights for nighttime operation. It is intended to describe suitable means for compliance with current Federal Aviation...
This SAE Aerospace Standard (AS) establishes minimum performance standards for new equipment position lights. This Aerospace Standard defines minimum light intensity in terms of candelas in vertical and horizontal directions...
This SAE Aerospace Standard (AS) establishes minimum performance standards for new equipment position lights. This SAE Aerospace Standard (AS) defines minimum and maximum light intensity in terms of candelas in...
This SAE Aerospace Standard (AS) establishes the minimum performance requirements for an angle of attack (AOA) system.
This SAE Aerospace Standard (AS) establishes the minimum performance standards for equipment used as secondary alternating current (AC) electrical power sources in aerospace electric power systems.
This SAE Aerospace Standard (AS) establishes the minimum requirements for design and qualification of equipment identified as Gyroscopically Stabilized Magnetic Direction Instruments.
This SAE Aerospace Standard (AS) is intended to apply to those oxygen regulators which supply gaseous oxygen at breathing pressures to meet physiological requirements of aircraft flight crew members. It...
This SAE Aerospace Standard (AS) provides a performance station designation system for aircraft propulsion systems and their derivatives.
This SAE Aerospace Standard (AS) provides dimensions and procedures for a standardized test fixture used to evaluate the static performance of O-rings and other seal types in glands per AS4716...
This SAE Aerospace Standard (AS) provides guidelines for the functional, performance, qualification and acceptance testing, and documentation requirements for the components of an airborne engine vibration monitoring (EVM) system which...
This SAE Aerospace Standard (AS) provides requirements for design and installation of aircraft jacking pad adapters and the mating jack socket interface to permit use of standard jacking equipment to...
This SAE Aerospace Standard (AS) specifies laboratory test procedures and minimum requirements for the manufacturer of restraint systems for use in civil aircraft. It is intended to establish a minimum...
This SAE Aerospace Standard (AS) specifies minimum performance requirements for pressure altimeter systems other than air data computers. This document covers altimeter systems that measure and display altitude as a...
This SAE Aerospace Standard (AS) specifies minimum performance requirements for primary pressure altimeter systems other than air data computers. This document covers altimeter systems that measure and display altitude as...
This SAE Aerospace Standard (AS) specifies minimum performance standards for airborne binocular Head Up Displays (HUDs) in fixed wing aircraft. This document covers criteria for conformal and non-conformal HUD systems...
This SAE Aerospace Standard (AS) specifies minimum performance standards for airborne binocular Head-Up Displays (HUDs) in fixed wing (14 CFR part 23, 25) aircraft; while this document is also applicable...
This SAE Aerospace Standard (AS) specifies minimum performance standards for all types of Electronic Displays and Electronic Display Systems that are intended for use in the flight deck by the...
This SAE Aerospace Standard (AS) specifies minimum performance standards for Electronic Displays which are intended for use in the cockpit by the pilot or other flight personnel under standard and...
This SAE Aerospace Standard (AS) specifies minimum performance standards for the following types of fire detection instruments intended for use in protecting aircraft cargo compartments, galleys, electronic equipment bays and...
This SAE Aerospace Standard describes the system used by passenger boarding stairs (PBS) mobile passenger boarding ramps (PBS) and boarding bridges (PBB) to inform on-board cabin crew about the docking...
This Society of Automotive Engineers (SAE) Aerospace Standard (AS) Annex defines Minimum Performance Standards (MPS), qualification requirements, and minimum documentation requirements for side-facing seats in civil rotorcraft, transport aircraft, and...
This specification applies to complete cable assemblies (using either molded on or attachable plugs) used to connect external electric power to aircraft and to attachable plugs used as replacement for...
This specification covers antifriction bearings in the -65°F to 350°F temperature range as specified on the applicable military standard.
This Specification covers constant displacement hydraulic motors, generally remotely mounted, using hydraulic fluid under pressure as the energy transfer medium for driving various accessories. Hydraulic motors shall be suitable for...
This specification covers environment-resistin g, quick disconnect, EMI/RFI shielded and non-shielded umbilical, electric connectors and adapter assemblies with removable crimp or nonremovable solder-type contacts and accessories. Connectors are rated for...
This specification covers four series of electrical connectors (plugs and receptacles) with removable crimp contacts and accessories (see 6.1 ). AS81511 connectors are not recommended for new design. All AS81511...
This specification covers general design and performance requirements for the mobility of towed ground support equipment. The complete mobility requirements for an item of towed aerospace ground equipment not specified...
This specification covers insulated and uninsulated crimp-style copper terminal lugs and conductor splices for stranded conductors.
This specification covers pressure boundary layer control systems of turbo-jet and turbo-prop aircraft for increasing the aerodynamic lift of the wings and flaps during approach, landing, and takeoff.
This specification covers single conductor electric wires made as specified in the applicable specification sheet with tin-coated, silver-coated, or nickel-coated copper or copper alloy conductors insulated with crosslinked polyalkene, crosslinked...
This specification covers Terminal Junction System (TJS) components which are used for interconnection of wiring and incorporation of passive components (see 6.1 ). These environment resistant components have in common...
This specification covers the general requirements for integrally illuminated information panels.
This specification covers the requirements for a light assembly for use on aircraft cabin desks.
This specification covers the requirements for an interval timer for controlling the duration of an electrical pulse to a solenoid valve for use in Rain Repellent systems covered by Specification...
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...
This specification covers the requirements for two types of a two-part, transparent, reversion resistant flexible insulating compound, to provide resilient, environmental, and electrical insulation of components in systems in temperature...
This specification covers three series of environment resisting, circular, miniature electrical connectors (plugs and receptacles) with removable crimp and/or nonremovable solder contacts, and accessories. The connectors are only recommended for...
This specification covers three series of environment resisting, circular, miniature electrical connectors (plugs and receptacles) with removable crimp and/or nonremovable solder contacts, and accessories.
This specification covers tools used to install tiedown straps on wire bundles and for installing connector accessory shield termination bands (see 6.1 ).
This specification covers two series of electrical, rectangular connectors with crimp type removable contacts. These connectors are provided with single, dual, triple, and quadruple insert shell configurations.
This specification covers two types and three weight/speed categories of personnel carrying parachute assemblies:
This specification establishes performance requirements for markings that have been applied to electrical insulating materials (see 6.1 ).
This specification establishes the qualification and acceptance limits for aeronautical engine low tension spark igniters.
This specification gives general requirements for electric devices for which the detail requirements are given by standards only, as the detail requirements for the devices are not complex enough to...
This Standard applies to all temperature instruments used in aircraft applications and environments. The word "instrument" as used in this Standard encompasses only the display device and does not include...
This standard covers Airspeed Instruments which display airspeed of an aircraft, as follows:
This standard covers ball bearings in the -65 to +350 °F temperature range as specified on the applicable drawing standards.
This standard covers ball bearings in the -65 to +350 °F temperature range or as specified on the applicable drawing standards.
This Standard covers Bank and Pitch Instruments which measure and display the angular displacement of bank and pitch from a gyroscopic vertical reference. This reference may be pneumatically or electrically...
This standard covers gaseous, liquid, and chemical aviators breathing oxygen.
This standard covers internal combustion heat exchanger type heaters used in the following applications: a Cabin heating (all occupied regions and windshield heating) b Wing and empennage anti-icing c Engine...
This standard covers oronasal type masks which use a continuous flow oxygen supply. Each such mask comprises a facepiece with valves as required, a mask suspension device, a reservoir, or...
This standard covers oxygen masks and breathing valves used with both panel mounted and mask mounted demand and pressure-demand oxygen regulators. Mask mounted oxygen regulators are covered under other standards,...
This 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 where...
This standard covers the following basic types:
This standard covers the following types of fire detection instruments intended for use in protecting aircraft cargo compartments, galleys, electronic equipment bays and other similar installations.
This standard covers three (3) basic types of flight recorders as defined below: All requirements specified in sections 3 , 4 , 5 , 6 & 7 of this standard...
This standard covers three (3) basic types of flight recorders as defined below: All requirements specified in Sections 3 , 4 , 5 , 6 and 7 of this standard...
This standard covers three basic types of total-temperature-me asuring instruments used as a means of determining the total temperature developed by adiabatic heating of the air due to motion of...
This standard covers Turn and Slip Instruments which measure and display the rate of turn about the vertical axis and incorporate an integral slip indicator.
This Standard covers two basic types of manifold pressure instruments:
This standard establishes the dimensional and visual quality requirements, lot requirements and packaging and labeling requirements for O-rings molded from AMS7601 butyl rubber. It shall be used for procurement purposes.
This standard provides minimum performance criteria for air data instruments intended to provide cockpit indication of: a Indicated airspeed (V i ) b Computer airspeed (V c ) c True...
This standard provides requirements for design and installation of aircraft jacking point adapters, as identified by ASCC AIR STD 25/7 Aircraft Jacking Pads, to permit use of standard jacking equipment.

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