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 |
|---|---|
| (10) AADL specifications may be processed manually or by tools for analysis and generation. This section documents additional requirements and permissions for determining compliance. Providers of processing method implementations must... | |
| Accelerometers are transducers, or sensors, that convert acceleration into an electrical signal that can be used for airframe, drive, and propulsion system vibration monitoring and analysis within vehicle health and... | |
| Accelerometers are transducers, or sensors, that convert acceleration into an electrical signal which can be used for vibration monitoring and analysis. This document defines interface requirements for accelerometers and associated... | |
| Amendment 1 of AS5590. | |
| AS5259 covers design requirements, performance requirements, and methods of procurement for tools and associated accessories used to crimp wire barrels of aircraft electrical wiring components including ferrules, terminals, splices, and... | |
| AS5653 may be applied to Air Vehicles and Stores implementing MIL-STD-1760 Interface Standard for Aircraft/Store Electrical Interconnection System. | |
| Blade trackers measure: (a) rotor blade height and (b) lead-lag for use in a Rotor Track and Balance (RT&B) function in a Health and Usage Monitoring System (HUMS). HUMS is... | |
| IEEE-1394b, Interface Requirements for Military and Aerospace Vehicle Applications, establishes the requirements for the use of IEEE Std 1394\u2122-2008 as a data bus network in military and aerospace vehicles. The... | |
| In lieu of TSO-C135, this SAE Aerospace Standard (AS) prescribes the minimum performance standards for wheels, brakes, and wheel and brake assemblies using electric power actuation for transport category (14... | |
| No scope available. | |
| Scope is unavailable. | |
| Technical Standard | |
| The complete requirements for acquiring the molded components described herein shall consist of this document and the latest issue of AS 5258. | |
| The complete requirements for acquiring the molded components described herein shall consist of this document and the latest issue of AS5258. | |
| The objective of this Minimum Operational Performance Specification is to specify the minimum performance of onboard inflight icing detection systems. Throughout the document, these devices are referred to as Flight... | |
| The purpose of this SAE Aerospace Standard (AS) is to provide guidelines for the components and configurations that define the four versions of the Weather Support to Deicing Decision Making... | |
| The purpose of this SAE Aerospace Standard is to provide guidelines for the components and configurations that define the research and commercial versions of the Weather Support to Deicing Decision... | |
| The scope of this document is to: 1 Provide a requirements document for RFID tag manufacturers to produce passive-only UHF RFID tags for the aerospace industry. 2 Identify the minimum... | |
| This Aerospace Standard (AS) 5659/4 Physical Layer Specification provides guidance for the physical layer of optical networks which use Wavelength Division Multiplexing (WDM), within the AS5659 WDM LAN specification document... | |
| This Aerospace Standard establishes a uniform procedure for calculation of electron vacancy numbers in superalloys. It is intended for use by suppliers of raw materials and parts, typically castings, for... | |
| This Aerospace Standard shall be used in conjunction with AMS 4946 to provide requirements for qualification testing and for Qualified Products Listing (QPL) and Qualified Manufacturer Listing (QML) for Ti-3Al-2.5V... | |
| This document contains minimum operational performance specification (MOPS) of active on-board INFLIGHT ICING DETECTION SYSTEMS (FIDS). This MOPS specifies FIDS operational performance which is the minimum necessary to satisfy regulatory... | |
| This document defines performance standards which mechanical fiber optic cable splices must meet to be accepted for use in aerospace platforms and environments. | |
| This document defines the steps and documentation required to perform a digital fiber optic link loss budget. This document does not specify how to design a digital fiber optic link. | |
| This document establishes standard requirements for aerospace sealants and adhesion promoters, which may be incorporated as part of Aerospace Material Specifications (AMS) for such products. This document provides for commonality... | |
| This document establishes standard requirements for aerospace sealants, which may be incorporated as part of Aerospace Material Specifications (AMS) for such products. This document provides for commonality of methods and... | |
| This document establishes test plans/procedures for the AS5643 Standard that by itself defines guidelines for the use of IEEE-1394b as a data bus network in military and aerospace vehicles. This... | |
| This document establishes the Rotorcraft Industry Technology Association (RITA) Health and Usage Monitoring System Data Interchange Specification. The RITA HUMS Data Interchange Specification will provide information exchange within a rotorcraft... | |
| This document provides interpretation of ISO/IEC 17025 and establishes additional requirements for accreditation of testing laboratories for evaluating organic coatings. | |
| This document provides standards for several aspects of aero-thermal system performance modeling using object-oriented programming systems. Nomenclature, application program interface, and user interface are addressed with the emphasis on nomenclature. | |
| This document specifies a multipoint, digital, serial interface that incorporates other interface standards such as EIA-485 and the nine bit interrupt mode of many microcontrollers. Standardized interfaces are critical to... | |
| This drawing specifies parts AS52760, AS52761, AS52762, and AS52763. To view suppliers qualified to manufacture this part, visit https://ts200.sae-it c.org/ . | |
| This drawing specifies parts AS52790, AS52791, AS52792, and AS52793. To view suppliers qualified to manufacture this part, visit https://ts200.sae-it c.org/ . | |
| This drawing specifies parts AS53763, AS53764, AS53765, AS53766, AS53767, AS53768, AS53769, AS53770, AS53771, AS53772, AS53773, AS53774, AS53775, AS53776, AS53777, AS53778, AS53779, AS53780, AS53781, AS53782, AS53783, AS53784, AS53785, AS53786, AS53787, AS53788,... | |
| This drawing specifies parts AS54364, AS54365, and AS54366. To view suppliers qualified to manufacture this part, visit https://ts200.sae-it c.org/ . | |
| This drawing specifies parts AS54471-12, AS54471-18, AS54471-2, and AS54471-5. To view suppliers qualified to manufacture this part, visit https://ts200.sae-it c.org/ . | |
| This drawing specifies parts AS54472-14, AS54472-2, and AS54472-5. To view suppliers qualified to manufacture this part, visit https://ts200.sae-it c.org/ . | |
| This drawing specifies parts AS54473-15, AS54473-3, and AS54473-5. To view suppliers qualified to manufacture this part, visit https://ts200.sae-it c.org/ . | |
| This drawing specifies parts AS54509, AS54510, AS54511, AS54512, AS54513, AS54514, AS54515, AS54516, AS54517, AS54518, AS54519, AS54520, AS54521, AS54522, AS54523, AS54524, AS54525, AS54526, AS54527, AS54528, AS54529, AS54530, AS54531, AS54532, AS54534, AS54536,... | |
| This drawing specifies parts AS54611, AS54612, AS54613, AS54614, AS54615, AS54616, AS54617, AS54618, AS54619, AS54620, AS54621, AS54622, AS54623, AS54624, AS54625, AS54626, AS54627, AS54628, AS54629, AS54630, AS54631, AS54632, AS54634, AS54636, AS54638, AS54640,... | |
| This drawing specifies parts AS54712, AS54713, AS54714, AS54715, AS54716, AS54717, AS54718, AS54719, AS54720, AS54721, AS54722, AS54723, AS54724, AS54725, AS54726, AS54727, AS54728, AS54729, AS54730, AS54731, AS54732, AS54734, AS54736, AS54738, AS54740, AS54742,... | |
| This drawing specifies parts AS54814, AS54815, AS54816, AS54817, AS54818, AS54819, AS54820, AS54821, AS54822, AS54823, AS54824, AS54825, AS54826, AS54827, AS54828, AS54829, AS54830, AS54831, AS54832, AS54834, AS54836, AS54838, AS54840, AS54842, AS54844, AS54846,... | |
| This drawing specifies parts AS54916, AS54917, AS54918, AS54919, AS54920, AS54921, AS54922, AS54923, AS54924, AS54925, AS54926, AS54927, AS54928, AS54929, AS54930, AS54931, AS54932, AS54934, AS54936, AS54938, AS54940, AS54942, AS54944, AS54946, AS54948, AS54950,... | |
| This drawing specifies parts AS55018, AS55019, AS55020, AS55021, AS55022, AS55023, AS55024, AS55025, AS55026, AS55027, AS55028, AS55029, AS55030, AS55031, AS55032, AS55034, AS55036, AS55038, AS55040, AS55042, AS55044, AS55046, AS55048, AS55050, AS55052, AS55054,... | |
| This drawing specifies parts AS55200-1, AS55200-2, and AS55200-3. To view suppliers qualified to manufacture this part, visit https://ts200.sae-it c.org/ . | |
| This drawing specifies parts AS55201-2, AS55201-4, and AS55201-6. To view suppliers qualified to manufacture this part, visit https://ts200.sae-it c.org/ . | |
| This drawing specifies parts AS55202-2, AS55202-5, and AS55202-8. To view suppliers qualified to manufacture this part, visit https://ts200.sae-it c.org/ . | |
| This drawing specifies parts AS55203-10, AS55203-3, and AS55203-6. To view suppliers qualified to manufacture this part, visit https://ts200.sae-it c.org/ . | |
| This drawing specifies parts AS55510, AS55511, AS55512, AS55513, AS55514, AS55515, AS55516, AS55517, AS55518, AS55519, AS55520, AS55521, AS55522, AS55523, AS55524, AS55525, AS55526, AS55527, AS55528, AS55529, AS55530, AS55531, AS55532, AS55534, AS55536, AS55538,... | |
| This drawing specifies parts AS55612, AS55613, AS55614, AS55615, AS55616, AS55617, AS55618, AS55619, AS55620, AS55621, AS55622, AS55623, AS55624, AS55625, AS55626, AS55627, AS55628, AS55629, AS55630, AS55631, AS55632, AS55634, AS55636, AS55638, AS55640, AS55642,... | |
| This drawing specifies parts AS55713, AS55714, AS55715, AS55716, AS55717, AS55718, AS55719, AS55720, AS55721, AS55722, AS55723, AS55724, AS55725, AS55726, AS55727, AS55728, AS55729, AS55730, AS55731, AS55732, AS55734, AS55736, AS55738, AS55740, AS55742, AS55744,... | |
| This drawing specifies parts AS55814, AS55815, AS55816, AS55817, AS55818, AS55819, AS55820, AS55821, AS55822, AS55823, AS55824, AS55825, AS55826, AS55827, AS55828, AS55829, AS55830, AS55831, AS55832, AS55834, AS55836, AS55838, AS55840, AS55842, AS55844, AS55846,... | |
| This drawing specifies parts AS56012, AS56013, AS56014, AS56015, AS56016, AS56017, AS56018, AS56019, AS56020, AS56021, AS56022, AS56023, AS56024, AS56025, AS56026, AS56027, AS56028, AS56029, AS56030, AS56031, AS56032, AS56034, AS56036, AS56038, AS56040, AS56042,... | |
| This drawing specifies parts AS56113, AS56114, AS56115, AS56116, AS56117, AS56118, AS56119, AS56120, AS56121, AS56122, AS56123, AS56124, AS56125, AS56126, AS56127, AS56128, AS56129, AS56130, AS56131, AS56132, AS56134, AS56136, AS56138, AS56140, AS56142, AS56144,... | |
| This drawing specifies parts AS56214, AS56215, AS56216, AS56217, AS56218, AS56219, AS56220, AS56221, AS56222, AS56223, AS56224, AS56225, AS56226, AS56227, AS56228, AS56229, AS56230, AS56231, AS56232, AS56234, AS56236, AS56238, AS56240, AS56242, AS56244, AS56246,... | |
| This drawing specifies parts AS56310, AS56311, AS56312, AS56313, AS56314, AS56315, AS56316, AS56317, AS56318, AS56319, AS56320, AS56321, AS56322, AS56323, AS56324, AS56325, AS56326, AS56327, AS56328, AS56329, AS56330, AS56331, AS56332, AS56334, AS56336, AS56338,... | |
| This drawing specifies parts AS56412, AS56413, AS56414, AS56415, AS56416, AS56417, AS56418, AS56419, AS56420, AS56421, AS56422, AS56423, AS56424, AS56425, AS56426, AS56427, AS56428, AS56429, AS56430, AS56431, AS56432, AS56434, AS56436, AS56438, AS56440, AS56442,... | |
| This drawing specifies parts AS56505, AS56506, AS56507, AS56508, AS56509, AS56510, AS56511, AS56512, AS56513, AS56514, AS56515, AS56516, AS56517, AS56518, AS56519, AS56520, AS56521, AS56522, AS56523, AS56524, AS56525, AS56526, AS56527, AS56528, AS56529, AS56530,... | |
| This drawing specifies parts AS56606, AS56607, AS56608, AS56609, AS56610, AS56611, AS56612, AS56613, AS56614, AS56615, AS56616, AS56617, AS56618, AS56619, AS56620, AS56621, AS56622, AS56623, AS56624, AS56625, AS56626, AS56627, AS56628, AS56629, AS56630, AS56631,... | |
| This drawing specifies parts AS56707, AS56708, AS56709, AS56710, AS56711, AS56712, AS56713, AS56714, AS56715, AS56716, AS56717, AS56718, AS56719, AS56720, AS56721, AS56722, AS56723, AS56724, AS56725, AS56726, AS56727, AS56728, AS56729, AS56730, AS56731, AS56732,... | |
| This drawing specifies parts AS56808, AS56809, AS56810, AS56811, AS56812, AS56813, AS56814, AS56815, AS56816, AS56817, AS56818, AS56819, AS56820, AS56821, AS56822, AS56823, AS56824, AS56825, AS56826, AS56827, AS56828, AS56829, AS56830, AS56831, AS56832, AS56834,... | |
| This interface standard applies to fuzes used in airborne weapons that use a 3-in fuze well. It defines: Physical envelope of the fuze well at the interface with the fuze. | |
| This interface standard applies to fuzes used in airborne weapons that use a 3-Inch Fuze Well. It defines: a Physical envelope of the fuze well at the interface with the... | |
| This is a SAE Standard specification with minimum performance characteristics for Turbine Flowmeter (TFM) that pertains only to sizes from \u00bd to 2 inches. The utilization of TFM is for... | |
| This procurement specification covers bolts, screws and studs made from a work-strengthened corrosion and heat resistant, age Hardenable nickel base alloy of the type identified under the Unified Numbering System... | |
| This procurement specification covers bolts, screws, and studs made from a work-strengthened corrosion and heat resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System... | |
| This SAE Aerospace specification establishes the requirements for heat cured solid film lubricants for aerospace fastener/threaded applications only. For other general or high temperature applications, see AS1701. | |
| This SAE Aerospace Standard (AS) aims at identifying the design criteria and testing methods adequate to guarantee the ultimate load and operational dependability of cargo restraint strap assemblies with a... | |
| This SAE Aerospace Standard (AS) contains requirements for a digital time division command/response multiplex data bus, for use in systems integration that is functionally similar to MIL-STD-1553B with Notice 2... | |
| This SAE Aerospace Standard (AS) covers devices whose primary function is the retention of fasteners, except for such devices that are integral with the item being retained. | |
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Hose Assembly, Heated, 125 psig, Lined Silicone, Potable Water, Procurement Specification -- AS5420A
Hose Assembly, Heated, 125 psig, Lined Silicone, Potable Water, Procurement Specification -- AS5420B
Hose Assembly, Heated, 125 psig, Lined Silicone, Potable Water, Procurement Specification -- AS5420C
Hose Assembly, Heated, 125 psig, Lined Silicone, Potable Water, Procurement Specification -- AS5420D
Hose Assembly, Heated, 125 psig, Lined Silicone, Potable Water, Procurement Specification -- AS5420E
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This SAE Aerospace Standard (AS) covers the requirements for a flexible, lightweight, low pressure, self-extinguishing, integrally heated silicone hose assembly. The hose has a fully fluorinated fluoropolymer inner liner and... |
| This SAE Aerospace Standard (AS) covers the requirements for thermocouple extension cable. Manufacturers of primary thermocouple wire in accordance with this specification must be qualified to the similar wire type... | |
| This SAE Aerospace Standard (AS) defines a data communications Transport Layer for the Joint Architecture for Unmanned Systems (JAUS). This Transport Specification defines the formats and protocols employed for the... | |
| This SAE Aerospace Standard (AS) defines minimum performance standards and related qualification criteria for add-on child restraint systems (CRS) which provide protection for small children in passenger seats of transport... | |
| This SAE Aerospace Standard (AS) defines the editorial format and policies necessary for the publication of Interface Control documents. The Common Interface Control Document Format Standard defines a common format... | |
| This SAE Aerospace Standard (AS) defines the editorial format and policies necessary for the publication of platform/subsystem Interface Control documents. The Common Interface Control Document Format Standard defines a common... | |
| This SAE Aerospace Standard (AS) details the design of fork pockets on containers and equipment for use with pallet lift trucks and forklift trucks. | |
| This SAE Aerospace Standard (AS) establishes a uniform procedure for calculation of electron vacancy numbers in superalloys. It is intended for use by suppliers of raw materials and parts, typically... | |
| This SAE Aerospace Standard (AS) establishes guidelines for the use of IEEE-1394-2008 Beta (formerly IEEE-1394b) as a data bus network in military and aerospace vehicles. It encompasses the data bus... | |
| This SAE Aerospace Standard (AS) establishes guidelines for the use of IEEE-1394b as a data bus network in military and aerospace vehicles. It encompasses the data bus cable and its... | |
| This SAE Aerospace Standard (AS) establishes minimum ice and rain performance criteria for electrically-heated pitot and pitot-static probes intended for use on the following classes of fixed-wing aircraft and rotorcraft. | |
| This SAE Aerospace Standard (AS) establishes requirements for the manufacture and certification of tool steel rings for magnetic particle inspection. | |
| This SAE Aerospace Standard (AS) establishes requirements for the manufacture of shim-type reference standards containing artificial flaws (notches) for use in the magnetic particle inspection process. | |
| This SAE Aerospace Standard (AS) establishes standard requirements for aerospace sealants and adhesion promoters, which may be incorporated as part of SAE Aerospace Material Specifications (AMS) for such products. This... | |
| 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 standard requirements for Message Boards (MBs) at Deicing Facilities. This standard also defines the minimum content and appearance of the display, functional... | |
| This SAE Aerospace Standard (AS) establishes the minimum standard requirements for message boards (MBs) at designated deicing facilities. The design of aircraft deicing facilities is covered by ARP4902. Standards for... | |
| This SAE Aerospace Standard (AS) establishes the requirements for a V-band grooved clamp couplings that are intended for use on fluid-line tubing joints, tailpipe joints, and accessory mount joints, on... | |
| This SAE Aerospace Standard (AS) establishes the requirements for heat cured solid film lubricants. For other general or high temperature applications, refer to AS1701. This document requires qualified products. | |
| This SAE Aerospace Standard (AS) establishes the requirements for heat cured solid film lubricants. For other general or high temperature applications, see AS1701. | |
| This SAE Aerospace Standard (AS) establishes the requirements for heat-cured solid film lubricants. For other general or high-temperature applications, refer to AS1701. This document requires qualified products. | |
| This SAE Aerospace Standard (AS) establishes the requirements for port preparation, installation and removal procedure for AS5550 fitting assembly and AS5865 fitting reducer assembly, and is applicable when specified on... | |
| This SAE Aerospace Standard (AS) establishes the requirements for port preparation, installation, and removal procedure for AS5550 fitting assembly and AS5865 fitting reducer assembly, and is applicable when specified on... | |
| This SAE Aerospace Standard (AS) establishes the requirements for the use of IEEE-1394b as a data bus network in military and aerospace vehicles. It defines the concept of operations and... | |
| This SAE Aerospace Standard (AS) establishes the surface pretreatment, temperature and baking time required to cure AS5272 lubricant when it is applied over the surfaces of manufactured parts of various... | |
| This SAE Aerospace Standard (AS) establishes the surface pretreatment, temperature, and baking time required to cure AS5272 lubricant when it is applied over the surfaces of manufactured parts of various... | |
| This SAE Aerospace Standard (AS) provides design criteria and performance tests for crash axes intended for use by aircraft crew members to assist in evacuation, extrication, fire fighting, or other... | |
| This SAE Aerospace Standard (AS) provides design criteria for onboard stairways intended for use by passengers aboard multi-deck transport category airplanes. It is not intended for stairways designed for use... | |
| This SAE Aerospace Standard (AS) provides technical information for hand-held wire stripper tools used to strip aerospace wire sizes 10 - 30 AWG. The AS includes inspection criteria for the... | |
| This SAE Aerospace Standard (AS) provides technical information for hand-held wire stripper tools used to strip aerospace wires sizes 10 - 30 AWG. The AS includes inspection criteria for the... | |
| This SAE Aerospace Standard (AS) provides the essential minimum design, installation, and removal standard for AS4383 adapter reducer and is applicable when specified on engineering drawings, or in procurement documents. | |
| This SAE Aerospace Standard (AS) shall be used in conjunction with AMS 4946 to provide requirements for qualification testing and for Qualified Products Listing (QPL) and Qualified Manufacturer Listing (QML)... | |
| This SAE Aerospace Standard (AS) shall be used in conjunction with AMS4946 to provide requirements for qualification testing and for Qualified Products Listing (QPL) and Qualified Manufacturer Listing (QML) for... | |
| This SAE Aerospace Standard (AS) specifies a data communications layer for the transport of messages defined by the Joint Architecture for Unmanned Systems (JAUS) or other Software Defined Protocols (SDP). | |
| This SAE Aerospace Standard (AS) specifies requirements for the interface between a rotational system indexing sensor and its interface electronics. These sensors generate one or more electrical pulses for each... | |
| This SAE Aerospace Standard (AS) specifies the general requirements for data recording procedures, packaging, and storing of elastomeric seals and seal assemblies which include an elastomeric element prior to the... | |
| This SAE Aerospace Standard (AS) specifies the general requirements for hydraulic system reservoirs that are installed in commercial and military aircraft and helicopters and also in missile hydraulic systems. This... | |
| This SAE Aerospace Standard (AS) specifies the interface requirements for towbar attachment fittings on the nose gear (when towing operations are performed from the nose gear) of conventional tricycle type... | |
| This SAE Aerospace Standard (AS) will specify what type night vision goggles are required, minimum requirements for compatible crew station lighting, aircraft exterior lighting such as anticollision lights and position/navigation... | |
| This SAE Aerospace Standard standardizes practices to: a maximize availability of authentic parts, b procure parts from reliable sources, c assure authenticity and conformance of procured parts, d control parts... | |
| This SAE Aerospace Standard standardizes practices to: a maximize availability of authentic parts, b procure parts from reliable sources, c assure authenticity and conformance of procured parts, d control suspect... | |
| This SAE Technical Report is an Aerospace Standard, compliant with the Organization and Operating Guide for the Aerospace Council of the SAE Technical Standards Board. It is consistent with the... | |
| This specification applies to a communication protocol for networked control systems. The protocol provides peer-to-peer communication for networked control and is suitable for implementing both peer-to-peer and master-slave control strategies. | |
| This specification covers connector and cable accessory heat shrinkable, electrical insulating, molded components fabricated from various polymer based compositions. These components are intended for use as connector and cable accessory... | |
| This specification covers design requirements, performance requirements, and methods of procurement for tools and associated accessories used to crimp wire barrels of aircraft electrical wiring components including ferrules, terminals, splices... | |
| This specification covers flexible couplings for joining tubing with AS5131 Type A beaded ends for use in aircraft fuel and vent systems (see 6.1 ). | |
| This specification covers flexible couplings for joining tubing with MS33660 Type A beaded ends for use in aircraft fuel and vent systems (see 6.1 ). | |
| This specification covers fuse holders for use in aircraft electric circuits in conjunction with MIL-F-5372 current limiter type fuses. These fuse holders are suitable for operation at −54° to 125°C. | |
| This specification covers fuse holders for use in aircraft electric circuits in conjunction with MIL-F-5372 current limiter type fuses. These fuse holders are suitable for operation at -54° to 125°C. | |
| This specification covers general requirements for direct current electrically held, environmentally sealed toggle switches for use in alternating current (AC) and direct current (DC) applications. (See 6.1 .) | |
| This specification covers hand driven, hydraulic ram pumps used on type I (-65° to +160°F) aircraft hydraulic systems. | |
| This specification covers the design and installation requirements for Type I and II military aircraft hydraulic systems. | |
| This specification covers the design and installation requirements for Types I and II aircraft hydraulic systems. | |
| This specification covers the design and installation requirements for Types I and II military aircraft hydraulic systems. | |
| This specification covers the design requirements and all performance requirements for procurement of 1 7/8 inch dial pilot's standby compasses as specified herein. | |
| This specification covers the general requirements for cabin air safety valves for use in pressurized cabins of aircraft to prevent excess positive and negative pressures in the cabin and to... | |
| This specification covers the performance requirements for a plug and receptacle, multiple termini, fiber optic connector. Fiber optic connectors using removable termini, and are capable of operating within a temperature... | |
| This specification covers the performance requirements for a plug and receptacle. The connector inserts may contain multiple termini or multiple termini and electrical contacts. The connectors use removable termini, or... | |
| This specification covers the requirements for current limiter type fuses for use in aircraft primary electrical power systems conforming to MIL-STD-704. These limiters are suitable for use in AS53731 fuse... | |
| This specification covers the requirements for current limiter type fuses for use in aircraft primary electrical power systems conforming to MIL-STD-704. These limiters are suitable for use in MIL-F-5373 fuse... | |
| This specification covers those devices whose primary function is locking, and excludes those devices which have integral locking features incorporated into the item being locked. | |
| This specification establishes general requirements for a family of trip-free Electromechanical Power Controller/Relays (EMPC) with electronic overcurrent sensing and control, intended for use in electrical systems conforming to RTCA, D0160... | |
| This specification establishes the design, performance, and test requirements for hydraulic flow rate fuses intended to be used for hydraulic circuit protection on aircraft. | |
| This specification establishes the design, performance, and test requirements for hydraulic quantity measuring fuses intended to be used for hydraulic circuit protection. | |
| This specification establishes the requirements for self-locking wrenchable nuts with thread sizes 0.7500 thru 1.5000 inches. The nuts are made of corrosion and heat resistant precipitation hardenable iron base alloy... | |
| This specification includes detailed requirements for a fiber optic cable splice compliant with AS5405. | |
| This specification is designed to present detailed procedure to be followed in splicing cable terminals. The types of cable to which this specification applies are listed in Section 2 and... | |
| This specification provides dimensional standards for crimp type contact wire barrel design and is a replacement for MS3190. Some wire barrel designs may exist in AS39029 but are not considered... | |
| This specification provides dimensional standards for crimp type contact wire barrel design. Some wire barrel designs may exist in AS39029, but, are not considered approved for future use therefore, will... | |
| This Standard aims at identifying the design criteria and testing methods adequate to guarantee the ultimate load and operational dependability of cargo restraint strap assemblies with a typical 22 250... | |
| This Standard aims at identifying the design criteria and testing methods adequate to guarantee the ultimate load and operational dependability of cargo restraint strap assemblies with a typical 22,250 N... | |
| This standard covers devices whose primary function is the retention of fasteners, except for such devices that are integral with the item being retained. | |
| This standard covers jacketed single-fiber multimode and single-mode fiber optic cables for aerospace usage. | |
| This standard covers those devices whose primary function is locking, and excludes those devices which have integral locking features incorporated into the item being locked. | |
| This standard covers those devices whose primary function is retaining and excludes those devices that have integral locking features incorporated into the item being retained. | |
| This standard defines a language for describing both the software architecture and the execution platform architectures of performance-critical , embedded, real-time systems; the language is known as the SAE Architecture... | |
| This standard establishes the acceptance criteria for surface discontinuities as revealed by magnetic particle or liquid penetrant examination of nuts. | |
| This standard is applicable to the marking of aerospace vehicle electrical wires and cables using ultraviolet (UV) lasers. This standard specifies the process requirements for the implementation of UV laser... | |
| This standard is for use by organizations that procure and integrate EEE parts. These organizations may provide EEE parts that are not integrated into assemblies (e.g., spares and/or repair EEE... | |
| This standard is for use by organizations that procure and/or integrate and/or repair EEE parts and/or assemblies containing such items, including maintenance, repair, and overhaul (MRO) organizations. The requirements of... | |
| This standard is for use by organizations that procure and/or integrate EEE parts and/or assemblies containing such items. The requirements of this standard are generic and intended to be applied/flowed... | |
| This standard, consisting of five documents, applies to designers, suppliers, and users of optical network services, systems, and components within mobile military and commercial aerospace platforms. The standard applies to... | |
| This supplement forms a part of the Aerospace Standard AS5420, Hose Assembly, Heated, 125 psig, Lined Silicone, Potable Water, Procurement Specification, and shall be used to identify hose assembly standards... | |
| To create a standard that instructs both supplier and user in the testing and characterization of initial build fiber optic cable assemblies for avionics/aerospace applications. This can be in the... |
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