SAE Aerospace Standards

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  • Ferrule, Coupling, Rigid, Fixed Cavity Threaded, Ferrule Type Tube Ends

    Standard [CURRENT] 2009-05-06

    SAE AS 1737C:2009-05-06

    Ferrule, Coupling, Rigid, Fixed Cavity Threaded, Ferrule Type Tube Ends

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  • Nut Assembly Coupling Rigid, Fixed Cavity, Threaded, Ferrule Type Tube Ends, Type I

    Standard [CURRENT] 2009-05-06

    SAE AS 1738C:2009-05-06

    Nut Assembly Coupling Rigid, Fixed Cavity, Threaded, Ferrule Type Tube Ends, Type I

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  • Fiber Optics Mechanization of a Digital Time Division Command/Response Multiplex Data Bus

    Standard [CURRENT] 2018-03-14

    SAE AS 1773A:2018-03-14

    Fiber Optics Mechanization of a Digital Time Division Command/Response Multiplex Data Bus

    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 ...

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  • Nut, Fitting, Retained, Lightweight

    Standard [CURRENT] 2008-06-22

    SAE AS 1790H:2008-06-22

    Nut, Fitting, Retained, Lightweight

    No scope available

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  • WIRE, RETAINER - TUBE COUPLING NUT

    Standard [CURRENT] 2023-10-10

    SAE AS 1791E:2023-10-10

    WIRE, RETAINER - TUBE COUPLING NUT

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  • Nut, Fitting, Lightweight, Flareless

    Standard [CURRENT] 2008-07-01

    SAE AS 1792E:2008-07-01

    Nut, Fitting, Lightweight, Flareless

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  • Terminology for Titanium Microstructures

    Standard [CURRENT] 2020-07-16

    SAE AS 1814F:2020-07-16

    Terminology for Titanium Microstructures

    This list of terms, with accompanying photomicrographs where appropriate, is intended as a guide for use in the preparation of material specifications.

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  • Methodology of Calculating Aircraft Cargo Volumes

    Standard [CURRENT] 2014-03-25

    SAE AS 1825C:2014-03-25

    Methodology of Calculating Aircraft Cargo Volumes

    The scope of this SAE Aerospace Standard (AS) shall cover the methodology of defining and determining the "internal volumes" of both the main deck and lower deck aircraft cargo compartments. The ...

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  • Electrical Power, 270 VDC, Aircraft, Characteristics and Utilization of

    Standard [CURRENT] 2023-04-03

    SAE AS 1831A:2023-04-03

    Electrical Power, 270 VDC, Aircraft, Characteristics and Utilization of

    This SAE Aerospace Standard (AS) establishes the characteristics and utilization of 270 V DC electric power at the utilization equipment interface and the constraints of the utilization equipment ...

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  • Nozzles and Ports - Gravity Fueling Interface Standard for Civil Aircraft

    Standard [CURRENT] 2012-01-03

    SAE AS 1852D:2012-01-03

    Nozzles and Ports - Gravity Fueling Interface Standard for Civil Aircraft

    This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical ...

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