Search Results

Standard

Insert - Thin Wall, Self-Locking, Metric Short and Long Length Installation and Removal of

2019-03-18

CURRENT

MA4811A

This SAE Metric Aerospace Standard (MA) provides minimum design, installation, and removal requirements for MA3520 and MA3521 thin wall inserts and is applicable when specified on engineering drawings or in procurement documents.

Standard

Identification and Coding of Fluid and Electrical Piping System Functions

2006-05-08

HISTORICAL

AIR1273A

This SAE Aerospace Information Report establishes a positive identification of the functions and, if applicable, the hazards and direction of flow of pipe, hose, tube, or electrical conduit lines.

Standard

IDENTIFICATION AND CODING OF FLUID AND ELECTRICAL PIPING SYSTEM FUNCTIONS

2011-08-09

HISTORICAL

AIR1273

Standard

Orientation of Engine Axis, Coordinate and Numbering Systems for Aircraft Gas Turbine Engines

2018-09-11

CURRENT

ARP246D

Orientation of the engine, engine axis and coordinate system referred to herein shall be the conventional terminology used in all references to aircraft gas turbine engines.

Standard

POSITION TERMS AND NUMBERING SYSTEM FOR AIRCRAFT GAS TURBINE ENGINES

1959-11-15

HISTORICAL

ARP246A

Numbering as provided herein is intended for convenience in locating a particular unit in a group of like or similar units.

Standard

ORIENTATION OF ENGINE AXIS, COORDINATE AND NUMBERING SYSTEMS FOR AIRCRAFT GAS TURBINE ENGINES

1995-05-01

HISTORICAL

ARP246B

Orientation of the engine, engine axis and coordinate system referred to herein shall be the conventional terminology used in all references to aircraft gas turbine engines.

Standard

Nut, Floating, Attached Retention Element (A.R.E.) - Hole Dimensions and Installation Requirements

2018-08-23

HISTORICAL

AS5133

This specification establishes the procedure for installing self-locking, floating, attached retention element (A.R.E.) nut assemblies and defines the necessary hole preparation.

Standard

Nut, Floating, Attached Retention Element (A.R.E.) - Hole Dimensions and Installation Requirements

2019-07-01

CURRENT

AS5133A

This specification establishes the procedure for installing self-locking, floating, attached retention element (A.R.E.) nut assemblies and defines the necessary hole preparation.

Standard

OPERATING INSTRUCTIONS FOR AIRCRAFT ENGINES

1944-05-01

HISTORICAL

AS177

This specification covers the requirements for the preparation of Operating Instructions in published form or in manuscript form suitable for publication as designated herein.

Standard

SURFACE FINISH

1942-11-01

HISTORICAL

AS107

This Standard provides a method for the application of surface finish control to aircraft engine parts. Recommendations for a Surface Roughness Standard are contained in A.S.A. publication B46 and this S.A.E. Aeronautical Standard contains a summary of information therein plus other information which has been compiled from current manufacturing practice.

Standard

SURFACE FINISH

1945-09-01

HISTORICAL

AS107A

This Standard provides a method for the application of surface finish control to aircraft engine parts. Recommendations for a Surface Roughness Standard are contained in A.S.A. publication B46 and this S.A.E. Aeronautical Standard contains a summary of information therein plus other information which has been compiled from current manufacturing practice.

Standard

SURFACE FINISH (RMS)

1995-05-01

HISTORICAL

AS107C

This standard provides a method for the application of surface finish control primarily to aircraft engine and propeller parts. Recommendations for a Surface Roughness Standard are contained in A.S.A. publication B46 and this S.A.E. Aeronautical Standard contains a summary of information therein plus other information which has been compiled from current manufacturing practice.

Standard

Surface Finish (RMS)

2006-05-04

HISTORICAL

AS107D

This standard provides a method for the application of surface finish control primarily to aircraft engine and propeller parts. Recommendations for a Surface Roughness Standard are contained in A.S.A. publication B46 and this S.A.E. Aeronautical Standard contains a summary of information therein plus other information which has been compiled from current manufacturing practice.

Standard

Surface Finish (RMS)

2013-01-04

CURRENT

AS107E

This standard provides a method for the application of surface finish control primarily to aircraft engine and propeller parts. Recommendations for a Surface Roughness Standard are contained in A.S.A. publication B46 and this S.A.E. Aeronautical Standard contains a summary of information therein plus other information which has been compiled from current manufacturing practice.

Standard

SURFACE ROUGHNESS (AA)

1963-05-15

HISTORICAL

AS291C

This standard provides a method of applying surface roughness, waviness and lay control. The data included herein also covers the method of applying surface roughness symbols and related designations to drawings and specifications of parts when applicable. This standard is based on the Arithmetical Average (AA) method of instrumentation. Data compiled are based on current manufacturing practices. It also includes a summary of data published in the American Standards Association publication ASA B46.1 - 1962 which may be referred to for supplementary data.

Standard

SURFACE TEXTURE, ROUGHNESS, WAVINESS AND LAY

1995-05-01

HISTORICAL

AS291D

This standard provides a method of applying surface roughness, waviness and lay control. The data included herein also covers the method of applying surface roughness symbols and related designations to drawings and specifications of parts when applicable. This standard is based on the Arithmetical Average (AA) method of instrumentation. Data compiled are based on current manufacturing practices. It also includes a summary of data published in the latest issue of the American Standards Association publication ASA B46.1.

Standard

SURFACE ROUGHNESS (AA)

1955-07-01

HISTORICAL

AS291A

This standard provides a method for the application of surface roughness control primarily to aircraft engine and propeller parts. ASA publication B46 may be used to supplement the information compiled herein. This standard contains a summary of the information in ASA B46 publication plus other information which has been compiled from current manufacturing practice.

Standard

SURFACE ROUGHNESS (AA)

1960-03-01

HISTORICAL

AS291B

This standard provides a method of applying surface roughness, waviness and lay control. The data included herein also covers the method of applying surface roughness symbols and related designations to drawings and specifications of parts when applicable. This standard is based on the Arithmetical Average (AA) method of instrumentation. Data compiled are based on current manufacturing practices. It also includes a summary of data published in the American Standards Association publication ASA B46.1 - 1955 which may be referred to for supplementary data.

Standard

Surface Texture, Roughness, Waviness and Lay

2006-05-04

HISTORICAL

AS291E

This standard provides a method of applying surface roughness, waviness and lay control. The data included herein also covers the method of applying surface roughness symbols and related designations to drawings and specifications of parts when applicable. This standard is based on the Arithmetical Average (AA) method of instrumentation. Data compiled are based on current manufacturing practices. It also includes a summary of data published in the latest issue of the American Standards Association publication ASA B46.1.

Standard

Surface Texture, Roughness, Waviness and Lay

2014-09-05

CURRENT

AS291F

This standard provides a method of applying surface roughness, waviness and lay control. The data included herein also covers the method of applying surface roughness symbols and related designations to drawings and specifications of parts when applicable. This standard is based on the Arithmetical Average (AA) method of instrumentation. Data compiled are based on current manufacturing practices. It also includes a summary of data published in the latest issue of the American Standards Association publication ASA B46.1.