SAE Aerospace Standards

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  • Handbook for the SAE AS4075 High Speed Ring Bus Standard

    Standard [CURRENT] 2012-05-03

    SAE AIR 4289A:2012-05-03

    Handbook for the SAE AS4075 High Speed Ring Bus Standard

    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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  • Overview and Rationale for GOA Framework Standard

    Standard [CURRENT] 2018-05-07

    SAE AIR 5315A:2018-05-07

    Overview and Rationale for GOA Framework Standard

    This document is a companion document to SAE AS4893 "Generic Open Architecture (GOA) Framework Standard" and provides an overview and rationale for SAE AS4893. The GOA Framework establishes an ...

    166.90 EUR VAT included

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  • Ultraviolet (UV) Lasers for Aerospace Wire Marking

    Standard [CURRENT] 2012-03-20

    SAE AIR 5468B:2012-03-20

    Ultraviolet (UV) Lasers for Aerospace Wire Marking

    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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  • Common Launch Acceptability Region Approach (CLARA)Rationale Document

    Standard [CURRENT] 2012-08-27

    SAE AIR 5712A:2012-08-27

    Common Launch Acceptability Region Approach (CLARA)Rationale Document

    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 ...

    140.20 EUR VAT included

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  • General Requirements for WDM Backbone Networks

    Standard [CURRENT] 2018-01-23

    SAE AIR 6005:2018-01-23

    General Requirements for WDM Backbone Networks

    This document (AIR6005) provides the framework for the specifications of a WDM OBN within the SAE AS5659 WDM LAN Specification document family, in particular, the Transparent Optical Backbone ...

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  • Interface for Micro Munition (IMM) Handbook

    Standard [CURRENT] 2016-09-16

    SAE AIR 6114:2016-09-16

    Interface for Micro Munition (IMM) Handbook

    This document was prepared by the SAE AS-1B1 IMM Task Group to explain and document background information and design decisions made during the development of AS5726. This handbook is published ...

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  • Unmanned Systems (UxS) Control Segment (UCS) Architecture: Version Description Document

    Standard [CURRENT] 2024-02-23

    SAE AIR 6520A:2024-02-23

    Unmanned Systems (UxS) Control Segment (UCS) Architecture: Version Description Document

    Governance of the Unmanned Aircraft System (UAS) Control Segment (UCS) Architecture was transferred from the United States Office of the Secretary of Defense (OSD) to SAE International in April 2015.

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  • Spark Plug Rating Calibration

    Standard [CURRENT] 1998-08-01

    SAE ARP 890A:1998-08-01

    Spark Plug Rating Calibration

    Procedure for obtaining the corrected heat-rating values (indicated mean effective pressure, IMEP) of spark plugs rated in the SAE 17.6 cubic inch rating engine (SAE AS840).

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  • Across Hex Corner Dimensions for Fluid Fittings and Nuts

    Standard [CURRENT] 2003-05-30

    SAE ARP 1942A:2003-05-30

    Across Hex Corner Dimensions for Fluid Fittings and Nuts

    This SAE Aerospace Recommended Practice (ARP) defines the minimum across hexagon corner dimensions for fluid tube fittings and nuts. The ARP covers commonly specified inch and millimeter hexagon ...

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  • JAUS Compliance and Interoperability Policy

    Standard [CURRENT] 2014-09-05

    SAE ARP 6012A:2014-09-05

    JAUS Compliance and Interoperability Policy

    This document, the JAUS Compliance and Interoperability Policy (ARP6012), recommends an approach to documenting the complete interface of an unmanned system or component in regard to the ...

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  • Altitude Graphs, Aircraft Reciprocating Engine Performance

    Standard [CURRENT] 2018-04-19

    SAE AS 1C:2018-04-19

    Altitude Graphs, Aircraft Reciprocating Engine Performance

    This SAE Aerospace Standard (AS) provides for aircraft reciprocating engines formats for altitude graph sheets recommended for use when presenting engine performance data.

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  • Magnetos, Aircraft, Drives for

    Standard [CURRENT] 2013-02-05

    SAE AS 13A:2013-02-05

    Magnetos, Aircraft, Drives for

    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 ...

    101.70 EUR VAT included

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  • Definitions, Aircraft Reciprocating Engine Performance

    Standard [CURRENT] 2018-06-20

    SAE AS 20D:2018-06-20

    Definitions, Aircraft Reciprocating Engine Performance

    This document lists definitions that are commonly used in describing aircraft reciprocating engine performance.

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  • Spark Plugs, Aircraft Engine

    Standard [CURRENT] 1987-11-05

    SAE AS 28B:1987-11-05

    Spark Plugs, Aircraft Engine

    This specification covers reciprocating engine shielded and unshielded spark plugs.

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  • Ignition Shielding, Aircraft

    Standard [CURRENT] 1996-11-01

    SAE AS 29:1996-11-01

    Ignition Shielding, Aircraft

    This standard covers two basic types of ignition shielding as follows: Type I - Unfilled and Type II - Filled

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  • Propeller Shaft Ends - Single Rotation

    Standard [CURRENT] 2013-01-04

    SAE AS 41F:2013-01-04

    Propeller Shaft Ends - Single Rotation

    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 ...

    123.10 EUR VAT included

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  • Starters, Mounting Pads and Drives, Types I, II, III, IV

    Standard [CURRENT] 2013-01-04

    SAE AS 44B:2013-01-04

    Starters, Mounting Pads and Drives, Types I, II, III, IV

    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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  • Generator, Mounting Pad and Drive, 4 Bolt

    Standard [CURRENT] 2001-10-01

    SAE AS 46A:2001-10-01

    Generator, Mounting Pad and Drive, 4 Bolt

    This SAE Aerospace Standard (AS) defines the requirements for heavy-duty hose assemblies suitable for use in 400 degrees F, 3000 psi aircraft hydraulic systems. Assemblies are suitable where rapid ...

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  • PUMP, FUEL, MOUNTING PAD AND DRIVE

    Standard [CURRENT] 2013-12-19

    SAE AS 47B:2013-12-19

    PUMP, FUEL, MOUNTING PAD AND DRIVE

    Scope is unavailable.

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  • Tachometer Drive - Type 1

    Standard [CURRENT] 2019-02-18

    SAE AS 54A:2019-02-18

    Tachometer Drive - Type 1

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  • Tachometer, Mounting Pad and Drive - Type II

    Standard [CURRENT] 2013-01-04

    SAE AS 55B:2013-01-04

    Tachometer, Mounting Pad and Drive - Type II

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  • Lever Ends - Fuel and Power Control

    Standard [CURRENT] 2018-09-19

    SAE AS 56D:2018-09-19

    Lever Ends - Fuel and Power Control

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  • Carburetor Flange, Aircraft, 4 Bolt - Single Barrel No. 2, 3, 4, 5, 6, 7, & 9

    Standard [CURRENT] 2013-01-03

    SAE AS 63B:2013-01-03

    Carburetor Flange, Aircraft, 4 Bolt - Single Barrel No. 2, 3, 4, 5, 6, 7, & 9

    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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  • Screw Thread Form, American National, Modified (National Round - NR)

    Standard [CURRENT] 2018-01-29

    SAE AS 82C:2018-01-29

    Screw Thread Form, American National, Modified (National Round - NR)

    This SAE Aerospace Standard (AS) defines an external thread with a rounded root radius based on a minimum root radius of .108 x Pitch.

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  • Splines, Involute (Full Fillet)

    Standard [CURRENT] 2014-02-06

    SAE AS 84D:2014-02-06

    Splines, Involute (Full Fillet)

    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 root.

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  • Propeller Blades Aluminum Alloy, Shank Dimensions for

    Standard [CURRENT] 2013-03-12

    SAE AS 90B:2013-03-12

    Propeller Blades Aluminum Alloy, Shank Dimensions for

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  • Propeller Shaft Ends, Dual Rotation (Propeller Supplied Bearing)

    Standard [CURRENT] 2013-03-12

    SAE AS 91D:2013-03-12

    Propeller Shaft Ends, Dual Rotation (Propeller Supplied Bearing)

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  • CONES, FRONT, PROPELLER HUB

    Standard [CURRENT] 2015-02-24

    SAE AS 92C:2015-02-24

    CONES, FRONT, PROPELLER HUB

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  • Cones, Rear, Propeller Hub

    Standard [CURRENT] 2013-03-12

    SAE AS 93E:2013-03-12

    Cones, Rear, Propeller Hub

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  • Snap Ring, Non-Controllable Propeller Hub (UNS G87400)

    Standard [CURRENT] 2013-03-12

    SAE AS 94C:2013-03-12

    Snap Ring, Non-Controllable Propeller Hub (UNS G87400)

    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 ...

    80.30 EUR VAT included

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  • FITTING ASSEMBLY, CROSS, REDUCER AND NON-REDUCER, INTERNAL FLARE ON ONE END, TO FLARED TUBE

    Standard [CURRENT] 2023-05-22

    SAE AS 95A:2023-05-22

    FITTING ASSEMBLY, CROSS, REDUCER AND NON-REDUCER, INTERNAL FLARE ON ONE END, TO FLARED TUBE

    91.00 EUR VAT included

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  • FITTING, CROSS, SHORT FLARELESS

    Standard [CURRENT] 2017-10-04

    SAE AS 100C:2017-10-04

    FITTING, CROSS, SHORT FLARELESS

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  • CROSS ASSEMBLY, RETAINED NUT, SHORT FLARELESS

    Standard [CURRENT] 2017-10-26

    SAE AS 101A:2017-10-26

    CROSS ASSEMBLY, RETAINED NUT, SHORT FLARELESS

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  • Fitting, Cross, Reducer, Flareless and Short Flareless

    Standard [CURRENT] 2017-10-12

    SAE AS 102C:2017-10-12

    Fitting, Cross, Reducer, Flareless and Short Flareless

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  • FITTING ASSEMBLY, CROSS, FLARELESS AND SHORT FLARELESS, REDUCER, RETAINED NUT

    Standard [CURRENT] 2017-10-18

    SAE AS 103C:2017-10-18

    FITTING ASSEMBLY, CROSS, FLARELESS AND SHORT FLARELESS, REDUCER, RETAINED NUT

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  • Surface Finish (RMS)

    Standard [CURRENT] 2013-01-04

    SAE AS 107E:2013-01-04

    Surface Finish (RMS)

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  • HOSE ASSEMBLY, PTFE, CRES REINFORCED, 3000 PSI, 400 °F, STRAIGHT TO STRAIGHT, FLARELESS, LIGHTWEIGHT

    Standard [CURRENT] 2021-05-19

    SAE AS 115K:2021-05-19

    HOSE ASSEMBLY, PTFE, CRES REINFORCED, 3000 PSI, 400 °F, STRAIGHT TO STRAIGHT, FLARELESS, LIGHTWEIGHT

    91.00 EUR VAT included

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  • HOSE ASSEMBLY, PTFE, CRES REINFORCED, 3000 PSI, 400 °F, STRAIGHT TO 45°, FLARELESS, LIGHTWEIGHT

    Standard [CURRENT] 2021-05-19

    SAE AS 116K:2021-05-19

    HOSE ASSEMBLY, PTFE, CRES REINFORCED, 3000 PSI, 400 °F, STRAIGHT TO 45°, FLARELESS, LIGHTWEIGHT

    91.00 EUR VAT included

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  • HOSE ASSEMBLY, PTFE, CRES REINFORCED, 3000 PSI, 400 °F, STRAIGHT TO 90°, FLARELESS, LIGHTWEIGHT

    Standard [CURRENT] 2021-05-19

    SAE AS 117K:2021-05-19

    HOSE ASSEMBLY, PTFE, CRES REINFORCED, 3000 PSI, 400 °F, STRAIGHT TO 90°, FLARELESS, LIGHTWEIGHT

    91.00 EUR VAT included

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  • HOSE ASSEMBLY, PTFE, CRES REINFORCED, 3000 PSI, 400 °F, 45° TO 45°, FLARELESS, LIGHTWEIGHT

    Standard [CURRENT] 2021-05-19

    SAE AS 118K:2021-05-19

    HOSE ASSEMBLY, PTFE, CRES REINFORCED, 3000 PSI, 400 °F, 45° TO 45°, FLARELESS, LIGHTWEIGHT

    96.30 EUR VAT included

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  • HOSE ASSEMBLY, PTFE, CRES REINFORCED, 3000 PSI, 400 °F, 45 TO 90°, FLARELESS, LIGHTWEIGHT

    Standard [CURRENT] 2021-05-19

    SAE AS 119K:2021-05-19

    HOSE ASSEMBLY, PTFE, CRES REINFORCED, 3000 PSI, 400 °F, 45 TO 90°, FLARELESS, LIGHTWEIGHT

    96.30 EUR VAT included

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  • HOSE ASSEMBLY, PTFE, CRES REINFORCED, 3000 PSI, 400 °F, 90° TO 90°, FLARELESS, LIGHTWEIGHT

    Standard [CURRENT] 2021-05-19

    SAE AS 120K:2021-05-19

    HOSE ASSEMBLY, PTFE, CRES REINFORCED, 3000 PSI, 400 °F, 90° TO 90°, FLARELESS, LIGHTWEIGHT

    96.30 EUR VAT included

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  • PROPELLER SHAFT END, FLANGED TYPE - NO. 1, 2, 3, 4, 5, & 6

    Standard [CURRENT] 2018-05-07

    SAE AS 127E:2018-05-07

    PROPELLER SHAFT END, FLANGED TYPE - NO. 1, 2, 3, 4, 5, & 6

    80.30 EUR VAT included

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  • TUBE BENDING RADIUS

    Standard [CURRENT] 2024-10-02

    SAE AS 130B:2024-10-02

    TUBE BENDING RADIUS

    This standard establishes basic design criteria including preferred bend radii, straight lengths between bends, flattening and surface conditions in the bend area. Also included is a table of ...

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  • PADS, OIL INLET AND OUTLET, TYPES I, II & III - FOR AIRPLANE CONNECTIONS AIRCRAFT ENGINES

    Standard [CURRENT] 2014-08-12

    SAE AS 131B:2014-08-12

    PADS, OIL INLET AND OUTLET, TYPES I, II & III - FOR AIRPLANE CONNECTIONS AIRCRAFT ENGINES

    Scope is unavailable.

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  • Hose Assembly, Metal - Medium Pressure, Flareless, Welded, Straight to Straight

    Standard [CURRENT] 2008-03-17

    SAE AS 136G:2008-03-17

    Hose Assembly, Metal - Medium Pressure, Flareless, Welded, Straight to Straight

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  • Hose Assembly, Metal - Medium Pressure, Flareless, Welded, Straight to 45°

    Standard [CURRENT] 2008-03-17

    SAE AS 137G:2008-03-17

    Hose Assembly, Metal - Medium Pressure, Flareless, Welded, Straight to 45°

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  • Hose Assembly, Metal - Medium Pressure, Flareless, Welded, Straight to 90°

    Standard [CURRENT] 2009-03-10

    SAE AS 138G:2009-03-10

    Hose Assembly, Metal - Medium Pressure, Flareless, Welded, Straight to 90°

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  • Hose Assembly, Metal - Medium Pressure, Flareless, Welded, 45° to 45°

    Standard [CURRENT] 2008-03-17

    SAE AS 139G:2008-03-17

    Hose Assembly, Metal - Medium Pressure, Flareless, Welded, 45° to 45°

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  • Hose Assembly, Metal - Medium Pressure, Flareless, Welded, 45° to 90°

    Standard [CURRENT] 2008-03-17

    SAE AS 140G:2008-03-17

    Hose Assembly, Metal - Medium Pressure, Flareless, Welded, 45° to 90°

    80.30 EUR VAT included

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