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 |
|---|---|
| Delete AS7108, clarify thickness requirements for coating of threads, clarify tape test requirements, update references, and general revision. | |
| No scope available. | |
| Operators of commercial passenger and cargo aircraft in unanimity will request aircraft manufacturers to follow this standard in the design of the nose gear (when towing operations are normally done... | |
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COUPLING, FLEXIBLE, VARIABLE CAVITY, THREADED FERRULE TYPE TUBE ENDS, ENVELOPE DIMENSIONS -- AS1711A
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Technical Standard |
| The emphasis in this standard is the development of data word and message formats for AS15531 or MIL-STD-1553 data bus applications. This standard is intended as a guide for the... | |
| The standard modules in this standard conform with ISO/R 54 and apply to spur and helical involute cylindrical gears. | |
| This aerospace specification defines the requirements for a threadless, flexible, self-bonding coupling assembly which, when installed on machined fixed cavity ferrules, provides a flexible connection for joining tubing and components... | |
| This Aerospace Standard establishes an identification system and provides design and tolerance information in describing two series of image quality indicators currently used in radiography of aerospace components, especially in... | |
| This Aerospace Standard provides minimum design, installation, and removal requirements for AS3319 through AS3322 studs and is applicable when specified on engineering drawings, or in procurement documents. | |
| This AS covers the requirements for three sizes of compartment restrained lower deck containers (Unit Load Devices) for the 767 airplane and which do not require airworthiness certification. NOTE: IATA... | |
| This AS covers the requirements for three sizes of compartment restrained lower deck containers (Unit Load Devices) for the 767 airplane and which do not require airworthiness certification. | |
| This document covers the performance requirements for solid dry film lubricants, air dried or heat cured, for use in aerospace applications. These lubricants are intended to prevent galling, and may... | |
| This document covers the performance requirements for solid dry film lubricants, air dried, or heat cured for use in aerospace applications. These lubricants are intended to prevent galling, and may... | |
| This document defines requirements for digital, command/ response time division multiplexing (data bus) techniques for fiber optic implementation. The concept of operation and information flow on the multiplex data bus... | |
| This document defines the requirements for a threadless, flexible, self-bonding coupling assembly, which, when installed on machined fixed cavity ferrules, provides a flexible connection for joining tubing and components in... | |
| This document defines the requirements for weld fittings and machine weldments using an orbiting welding head suitable for use on cold worked 3Al-2.5V titanium and 21Cr-6Ni-9Mn CRES tubing. | |
| This document defines the requirements for weld fittings and machine weldments using an orbiting welding head suitable for use on cold worked 3Al-2.5V titanium, 21Cr-6Ni-9Mn CRES and 718 nickel alloy... | |
| This document defines the requirements for weld fittings and machine weldments using an orbiting welding head suitable for use on cold worked 3Al-2.5V titanium, 21Cr-6Ni-9Mn CRES, and 718 nickel alloy... | |
| 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 equivalent to MIL-STD-1553B with Notice 2. | |
| This SAE Aerospace Standard (AS) covers the design, fabrication, performance and operational testing requirements for lower deck containers for use in main line aircraft which do not require airworthiness certification... | |
| This SAE Aerospace Standard (AS) covers the requirements for lower deck containers in wide body and standard body aircraft which do not require airworthiness certification under the condition of compartment... | |
| This SAE Aerospace Standard (AS) covers the requirements for three sizes of compartment restrained lower deck containers (unit load devices) for the 767 airplane and which do not require airworthiness... | |
| This SAE Aerospace Standard (AS) defines the requirements for a threaded flexible coupling assembly, which utilizes ferrules or machined tube end fittings to join tubing and components in aircraft fuel... | |
| This SAE Aerospace Standard (AS) defines the requirements for a threadless, flexible, self-bonding coupling assembly which, when installed on machined fixed cavity ferrules, provides a flexible connection for joining tubing... | |
| This SAE Aerospace Standard (AS) defines the requirements for a threadless, flexible, self-bonding coupling assembly which, when installed on machined fixed-cavity ferrules, provides a flexible connection for joining tubing and... | |
| This SAE Aerospace Standard (AS) establishes the standard modules for aerospace metric involute gear teeth and establishes the tooth dimensions of aerospace metric involute gear teeth in terms of the... | |
| This SAE Aerospace Standard (AS) specifies the interface requirements for tow bar attachment fittings on the nose gear (when towing operations are performed from the nose gear) of conventional tricycle... | |
| This SAE Aerospace Standard provides minimum design, installation, and removal requirements for AS3319 through AS3322 studs and is applicable when specified on engineering drawings, or in procurement documents. | |
| This specification covers the design requirements and configuration of letters, numerals, and identification for aircrew station displays and control panels. | |
| This specification covers the general requirements for pneumatic control valves for use with the starters on aircraft gas turbine engines. This specification shall be used in conjunction with AS943, ARP949,... | |
| This specification covers the requirements for aircraft, hydraulic, self-sealing, quick disconnect couplings, for use in Type II hydraulic systems (-65 to +275 °F temperature range) as defined by AS5440. | |
| This specification covers the requirements for aircraft, hydraulic, self-sealing, quick disconnect couplings, for use in Type II hydraulic systems (-65 to +275 °F temperature range) as defined by MIL-H-5440. | |
| This specification covers the requirements for format and outline of contents of operating instructions in published form or in manuscript form suitable for publication. | |
| This specification covers the requirements for the preparation of Limits, Table of Limits and Lubrication Charts in published form for service and production use. | |
| This specification covers the requirements for the preparation of Operating Instructions in published form or in manuscript form suitable for publication as designated herein. | |
| This specification covers the requirements for the preparation of Tables of Limits and Limits and Lubrication Charts in published form. | |
| This specification covers the requirements for the preparation or Table of Limits, and Limits and Lubrication Charts in published form for service and production use. | |
| This specification covers the requirements for two types of oxygen pressure reducers. | |
| This specification defines the requirements for a threaded flexible coupling assembly, which utilizes ferrules or machined tube end fittings to join tubing and components in aircraft fuel, vent or other... | |
| This specification defines the requirements for a threaded flexible coupling assembly, which utilizes ferrules or machined tube end fittings, to join tubing and components in aircraft fuel, vent or other... | |
| This specification defines the requirements for a threaded rigid coupling assembly, which utilizes ferrule type machined tube end fittings, to join tubing and components in aircraft fuel, vent and other... | |
| This specification defines the requirements for a threaded rigid coupling assembly, which utilizes ferrule type machined tube end fittings, to join tubing and components in aircraft fuel, vent, and other... | |
| This specification defines the requirements for weld fittings and machine weldments using an orbiting welding head suitable for use on cold worked 3A1-2.5V titanium and 21Cr-6Ni-9Mn CRES tubing. | |
| This specification defines the requirements for weld fittings and machine weldments using an orbiting welding head suitable for use on cold worked 3Al-2.5V titanium and 21Cr-6Ni-9Mn CRES tubing. | |
| This specification establishes the requirements for the (TBS) jet fuel starter for the (TBS) gas turbine engine used in the (TBS) aircraft. | |
| This standard covers heat and corrosion resistant steel loop clamps with a woven steel wire cushion that is attached to the clamp by spot welding and is intended for use... | |
| This standard gives the dimensional requirements for insert arrangements used in MIL-C-5015, MIL-C-22992 (Classes C, J, and R), and MIL-C-83723 (Series II) electrical connectors. | |
| This standard gives the general physical, electrical and chemical methods for testing fiber optics cables for conformance with the requirements. It was prepared in order to eliminate unnecessary of undesirable... | |
| This standard gives the general physical, electrical and chemical methods for testing fiber optics cables for conformance with the requirements. It was prepared in order to eliminate unnecessary or undesirable... | |
| This standard is supplementary to AS 41 'Propeller Shaft Ends, Single Rotation', and AS 91 'Propeller Shaft Ends, Dual Rotation (Propeller Supplied Bearing)'. It is applicable to all engines that... | |
| This standards gives the dimensional requirements for insert arrangements used in MIL-C-5015, MIL-C-22992 (Classes C, J, and R), and MIL-C-83723 (Series II) electrical connectors. |
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