SAE Aerospace Standards

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  • Bolts, Screws and Studs, Nickel Alloy, UNS N07718 Work-Strengthened, Tensile Strength 220 ksi Procurement Specification

    Standard [CURRENT] 2020-08-03

    SAE AS 5270A:2020-08-03

    Bolts, Screws and Studs, Nickel Alloy, UNS N07718 Work-Strengthened, Tensile Strength 220 ksi Procurement Specification

    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 ...

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  • Lubricant, Solid Film, Heat Cured, Corrosion Inhibiting, Procurement Specification

    Standard [CURRENT] 2024-09-11

    SAE AS 5272G:2024-09-11

    Lubricant, Solid Film, Heat Cured, Corrosion Inhibiting, Procurement Specification

    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 ...

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  • Performance Standard for Child Restraint Systems in Transport Category Airplanes

    Standard [CURRENT] 2025-05-01

    SAE AS 5276/1A:2025-05-01

    Performance Standard for Child Restraint Systems in Transport Category Airplanes

    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 ...

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  • Tool Steel Ring for Magnetic Particle Inspection

    Standard [CURRENT] 2023-02-20

    SAE AS 5282C:2023-02-20

    Tool Steel Ring for Magnetic Particle Inspection

    This SAE Aerospace Standard (AS) establishes requirements for the manufacture and certification of tool steel rings for magnetic particle inspection.

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  • Standard Specification for Turbine Flowmeters

    Standard [CURRENT] 2017-02-09

    SAE AS 5304:2017-02-09

    Standard Specification for Turbine Flowmeters

    This is a SAE Standard specification with minimum performance characteristics for Turbine Flowmeter (TFM) that pertains only to sizes from 1/2 to 2 inches. The utilization of TFM is for ...

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  • Fitting end, Spherical, 37° Flared Tube Connection Design Standard

    Standard [CURRENT] 2007-11-19

    SAE AS 5309A:2007-11-19

    Fitting end, Spherical, 37° Flared Tube Connection Design Standard

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  • Fitting End, Bulkhead, Spherical, 37° Flared tube Connection Design Standard

    Standard [CURRENT] 2007-11-19

    SAE AS 5310A:2007-11-19

    Fitting End, Bulkhead, Spherical, 37° Flared tube Connection Design Standard

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  • Storage of Elastomer Seals and Seal Assemblies Which Include an Elastomer Element Prior to Hardware Assembly

    Standard [CURRENT] 2022-11-18

    SAE AS 5316:2022-11-18

    Storage of Elastomer Seals and Seal Assemblies Which Include an Elastomer Element Prior to Hardware Assembly

    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 ...

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  • COUPLINGS, CLAMP, GROOVED, V-BAND, 1.75 TO 14.25 FLANGE OD (-65 TO 800 °F)

    Standard [CURRENT] 2017-04-11

    SAE AS 5355/1B:2017-04-11

    COUPLINGS, CLAMP, GROOVED, V-BAND, 1.75 TO 14.25 FLANGE OD (-65 TO 800 °F)

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  • COUPLINGS, CLAMP, GROOVED, V-BRAND, 1.75 TO 6.25 FLANGE OD (-65 TO 250 °F)

    Standard [CURRENT] 2017-03-28

    SAE AS 5355/2B:2017-03-28

    COUPLINGS, CLAMP, GROOVED, V-BRAND, 1.75 TO 6.25 FLANGE OD (-65 TO 250 °F)

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