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 |
|---|---|
| Amendment 1 of AS81714. | |
| Amendment 1 of AS81714/1. | |
| Amendment 1 of AS81790. | |
| Amendment 1 of AS81824A. | |
| Amendment 1 of AS83519A. | |
| Amendment 1 of AS85028. | |
| Amendment 1 of AS85049/103A | |
| Amendment 1 of AS85049/104A | |
| Amendment 1 of AS85049/105A | |
| Amendment 1 of AS85049/109B. | |
| Amendment 1 of AS85049/10A. | |
| Amendment 1 of AS85049/111B | |
| Amendment 2 of AS81714. | |
| Amendment 2 of AS81790. | |
| Amendment 2 of AS83519A. | |
| Amendment 2 of AS85028. | |
| Amendment 2 of AS85049/109B | |
| Amendment 2 of AS85049/111B. | |
| Amendment 3 of AS83519A. | |
| Amendment 3 of AS85049/109B. | |
| AS81714 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 the... | |
| AS81969 covers the general requirements for installing and removal tools for use in installing and removing electrical contacts used in connectors and other electrical and electronic components (see section 6... | |
| No scope available. | |
| Technical Standard | |
| The AS81824 specification covers environment resistant, permanent crimp type, splices having heat shrinkable insulating sleeve and meltable environmental seals or heatless sealing sleeves. The splices may be used with tin,... | |
| The purpose of this standard is to specify minimum requirements for aircraft anti-collision lights. This standard covers two types of aircraft anti-collision lights. | |
| The tubing described in this document is for use in electrical interconnect systems for the protection and routing of wire bundle installations. | |
| This aerospace standard establishes the basic requirements for the specification and testing of air/surface (intermodal) 8 x 8 ft (2.44 x 2.44 m) cross-section containers. The basic requirements for the... | |
| This document establishes two classes of containers, Type A for Air (only) and Type B for Air/Surface (Intermodal). | |
| This document establishes two classes of containers, Type A for Air only and Type B for Air/Land. | |
| This document has been taken directly from U.S. Military Specification MIL-C-81790A, Amendment 1 and contains only minor editorial and format changes required to bring it into conformance with the publishing... | |
| This document provides details of test methods that should be taken into consideration when qualifying fiber optic termini to the product specifications (slash sheets). The product specifications (slash sheets) provide... | |
| This SAE Aerospace Standard (AS) covers airframe plain spherical bearings utilizing a copper-beryllium ball and corrosion resistant steel outer race for use between −65 °F and +350 °F. | |
| This SAE Aerospace Standard (AS) covers plain spherical bearings which are self-aligning and self-lubricating by utilizing polytetrafluoroethyl ene (PTFE in a fabric composite or molded material that is bonded to... | |
| This SAE Aerospace Standard (AS) covers plain spherical bearings which are self-aligning and self-lubricating by utilizing polytetrafluoroethyl ene (PTFE) in a fabric composite or molded material that is bonded to... | |
| This SAE Aerospace Standard (AS) defines an external thread with a rounded root radius based on a minimum root radius of .108 × Pitch. | |
| This SAE Aerospace Standard (AS) defines an involute with a 30° pressure angle and a full radius at the roots thus reducing the stress concentration in the area of the... | |
| This SAE Aerospace Standard (AS) establishes the basic requirements for the specification and testing of air surface (intermodal) 8 ft × 8 ft (2.44 m × 2.44 m) cross-section containers. | |
| This SAE Aerospace Standard (AS) establishes the basic requirements for the specification and testing of air surface (intermodal) 8 ft x 8 ft (2.44 m x 2.44 m) cross-section containers. | |
| This slash sheet defines the design, performance, and interoperability requirements for fiber optic expanded beam, ball lens, single-mode pin termini installed in size 16 cavity connectors. | |
| This slash sheet defines the design, performance, and interoperability requirements for fiber optic expanded beam, ball lens, single-mode socket termini installed in size 16 cavity connectors. | |
| This specification covers airframe plain spherical bearings utilizing a beryllium-copper ball and corrosion resistant steel outer race for use between -65°F and +350°F. | |
| This specification covers both insulated and uninsulated solid conductor wire, designed for solderless wrap connections in electrical and electronic devices and equipment. The terminations of the wire are intended to... | |
| This specification covers connector accessories for use with electrical connectors under environmental or non-environmental conditions. Applicable connector accessories defined in this specification are delineated for the suppression of Electromagnetic Interference... | |
| This specification covers environment and fluid resisting, rectangular type, rack to panel electrical connectors (plugs and receptacles). These connectors utilize individually sealing removable crimp type contacts and are capable of... | |
| This specification covers environment resistant, heat-shrinkable solder type shield terminations. They may be used on data-bus, RF and shielded cables in applications where the operating temperature does not exceed 150°C. | |
| This specification covers environment resistant, heat-shrinkable solder type shield terminations. They may be used on data-bus, RF and shielded cables in applications where the operating temperature does not exceed 150... | |
| This specification covers environment resistant, heat-shrinkable solder type shield terminations. They may be used on data-bus, RF, and shielded cables in applications. Operating temperature of each product are as indicated... | |
| This specification covers environment resistant, permanent crimp type, splices having a heat shrinkable insulating sleeve and meltable environmental seals. They may be used with tin plated and silver plated conductors... | |
| This specification covers plain and flanged sleeve bearings which are self-lubricating by incorporating polytetrafluoroethyl ene (PTFE) in a liner in the bore for use in a temperature range of -65° | |
| This specification covers plain rod end bearings which are self-aligning and self-lubricating by incorporating polytetrafluoroethyl ene (PTFE) in a liner between the ball and outer ring for use in the... | |
| This specification covers plain rod end bearings which are self-aligning and self-lubricating by incorporating polytetrafluoroethyl ene (PTFE) in a liner between the ball and race for use in the temperature... | |
| This specification covers plain rod end bearings, corrosion resistant steel (CRES) or alloy steel, which are self-aligning and self-lubricating by incorporating polytetrafluoroethyl ene (PTFE) in a liner between the ball... | |
| This specification covers plain spherical bearings which are self-aligning and self-lubricating by incorporating polytetrafluoroethyl ene (PTFE) in a liner between the ball and race (outer ring). PTFE is incorporated in... | |
| This specification covers requirements for material used in electrical insulating heat shrinkable components. The continuous operating temperature of these materials shall range from -75°C to +200°C (-103°F to +392°F). (See... | |
| 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 requirements for aircraft external electric power receptacles. | |
| This specification covers the requirements for sliding spherical, sleeve, and thrust self-lubricating bearings which are for use in the ambient temperature range -65°F to +160°F at high cyclic speeds. | |
| This specification covers the requirements for two types of anti-icing and deicing-defrosting fluids for use on aircraft. | |
| This specification established (1) the common requirements for hydraulic units capable of functioning as starters and as pumps suitable for use in aircraft and missiles and (2) the methods to... | |
| This specification establishes dimensional, structural, and environmental requirements for a series of air-land cargo containers. | |
| This specification establishes requirements for ice detectors. | |
| This specification prescribes general requirements for marking of aircraft ground support equipment and other vehicles (i.e., runway sweepers, firetrucks, refuelers, etc.), used on or near the flight line area with... | |
| This specification prescribes general requirements for marking of aircraft ground support equipment and other vehicles (i.e., runway sweepers, firetrucks, refulers, etc.), used on or near the flight line area with... | |
| This standard covers plain and flanged sleeve bearings which are self-lubricating by incorporating polytetrafluoroethyl ene (PTFE) in a liner in the bore for use in the temperature range of -65... | |
| This standard covers plain spherical bearings which are self-aligning and self-lubricating by utilizing polytetrafluoroethyl ene (PTFE in a fabric composite or molded material that is bonded to the inner diameter... | |
| This standard covers the requirements for spherical, self-aligning, self-lubricating bearings that are for use in the ambient temperature range of -65 to +160 °F (-54 to +71 °C) at high... | |
| This standard covers the requirements for spherical, self-aligning, self-lubricating bearings which are for use in the ambient temperature range -65 to +160 °F (-54 to +71 °C) at high cyclic... | |
| This standard covers the requirements for spherical, self-aligning, self-lubricating, bearings which are for use in the ambient temperature range of -65 to +160 °F (-54 to +71 °C) at high... | |
| This standard is applicable to reciprocating engines powering unmanned aerial vehicles (UAV) that have rated power values less than 22.4 kW and are not to be used for human transport. | |
| This standard provides the recommended requirements for electrostatic spray application of AMS3143 powder coatings to aerospace components. Adherence to these requirements will facilitate satisfactory performance of the applied powder coating. |
| << Prev | Next >> |