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SAE Aerospace Standards

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  • Health and Usage Monitoring System, Blade Tracker Interface Specification

    Standard [CURRENT] 2020-04-02

    SAE AS 5393A:2020-04-02

    Health and Usage Monitoring System, Blade Tracker Interface Specification

    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 a generic term for a ...

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  • Health and Usage Monitoring System, Advanced Multipoint Interface Specification

    Standard [CURRENT] 2020-04-11

    SAE AS 5394A:2020-04-11

    Health and Usage Monitoring System, Advanced Multipoint Interface Specification

    This document specifies a multipoint, digital, serial interface that incorporates other interface standards such as EIA-485 and the nien bit interrupt mode of many microcontrollers. Standardized ...

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  • Health and Usage Monitoring System Data Interchange Specification

    Standard [CURRENT] 2025-09-18

    SAE AS 5395A:2025-09-18

    Health and Usage Monitoring System Data Interchange Specification

    This document establishes the Rotorcraft Industry Technology Association (RITA) Health and Usage Monitoring System Data Interchange Specification. The RITA HUMS Data Interchange Specification will ...

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  • Design and Performance Criteria Aircraft Crash Axes

    Standard [CURRENT] 2021-04-23

    SAE AS 5402A:2021-04-23

    Design and Performance Criteria Aircraft Crash Axes

    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 ...

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  • Mechanical Splice for Aerospace Fiber Optic Cables

    Standard [CURRENT] 2018-09-07

    SAE AS 5405:2018-09-07

    Mechanical Splice for Aerospace Fiber Optic Cables

    This document defines performance standards which mechanical fiber optic cable splices must meet to be accepted for use in aerospace platforms and environments.

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  • Mechanical Splice, Fiber Optic, Crimp and Cleave, for Aerospace Simplex Cable

    Standard [CURRENT] 2018-09-07

    SAE AS 5405/1:2018-09-07

    Mechanical Splice, Fiber Optic, Crimp and Cleave, for Aerospace Simplex Cable

    This specification includes detailed requirements for a fiber optic cable splice compliant with AS5405.

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  • FITTING, UNION, TUBE, .375 BULKHEAD

    Standard [CURRENT] 2015-02-17

    SAE AS 5406D:2015-02-17

    FITTING, UNION, TUBE, .375 BULKHEAD

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  • WIRE, THERMOCOUPLE, HIGH TEMPERATURE AND FIRE RESISTANT LIGHT WEIGHT, SMALL DIAMETER NICKEL/CHROMIUM (KP); NICKEL/ALUMINUM/MANGANESE (KN) THERMOCOUPLE EXTENSION, 260 °C

    Standard [CURRENT] 2018-12-07

    SAE AS 5419/1A:2018-12-07

    WIRE, THERMOCOUPLE, HIGH TEMPERATURE AND FIRE RESISTANT LIGHT WEIGHT, SMALL DIAMETER NICKEL/CHROMIUM (KP); NICKEL/ALUMINUM/MANGANESE (KN) THERMOCOUPLE EXTENSION, 260 °C

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  • WIRE, THERMOCOUPLE, FLUOROPOLYMER INSULATED, ABRASION RESISTANT, EXTRUDED PTFE NICKEL/CHROMIUM (KP); NICKEL/ALUMINUM/MANGANESE (KN) THERMOCOUPLE EXTENSION MEDIUM WEIGHT, 260 °C

    Standard [CURRENT] 2018-12-07

    SAE AS 5419/2A:2018-12-07

    WIRE, THERMOCOUPLE, FLUOROPOLYMER INSULATED, ABRASION RESISTANT, EXTRUDED PTFE NICKEL/CHROMIUM (KP); NICKEL/ALUMINUM/MANGANESE (KN) THERMOCOUPLE EXTENSION MEDIUM WEIGHT, 260 °C

    84.50 EUR VAT included

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  • WIRE, THERMOCOUPLE, FLUOROPOLYMER INSULATED, EXTRUDED TFE NICKEL/CHROMIUM (KP); NICKEL/ALUMINUM/MANGANESE (KN) THERMOCOUPLE EXTENSION, 260 °C

    Standard [CURRENT] 2018-12-07

    SAE AS 5419/3A:2018-12-07

    WIRE, THERMOCOUPLE, FLUOROPOLYMER INSULATED, EXTRUDED TFE NICKEL/CHROMIUM (KP); NICKEL/ALUMINUM/MANGANESE (KN) THERMOCOUPLE EXTENSION, 260 °C

    84.50 EUR VAT included

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