Search Results

Standard

White Paper to Support Supersession of MIL-S-8879C With AS8879C

2018-08-23

HISTORICAL

AIR5926

This paper was prepared to support supersession of MIL-S-8879C with Screw Thread Conformity Task Force selected industry standard AS8879C, published by the Society of Automotive Engineers (SAE). Other documentation changes will be covered by separate papers. Separate papers are anticipated for thread gaging issues, and thread gage calibration procedures. The STC-TF decided that the thread design standard needed to be completed before thread gage definition could be addressed. Thread gage definition has to be known before calibration procedures can be addressed.

Standard

WIRE - STEEL, CORROSION AND HEAT RESISTANT, SAFETY, 1800 °F

2019-10-31

CURRENT

AS9226B

Standard

Undercuts for Straight Screw Threads - Metric

2019-06-19

CURRENT

AS1508A

This standard provides recommended dimensional data for screw thread undercuts for straight 'MJ' metric screw threads in accordance with AS1370.

Standard

Undercuts for Straight Screw Threads - Metric

2012-11-01

HISTORICAL

AS1508

This standard provides recommended dimensional data for screw thread undercuts for straight ‘MJ’ metric screw threads in accordance with AS1370.

Standard

Undercuts for Straight Screw Threads - Metric

2018-08-23

HISTORICAL

MA1508

This SAE Aerospace Standard (MA) provides recommended dimensional data for screw thread undercuts for straight “MJ” metric screw threads in accordance with MA1370.

Standard

Torque Tightening Threaded Fasteners

2012-10-19

HISTORICAL

AIR1471A

The purpose of this SAE Aerospace Information Report (AIR) is to provide the aerospace propulsion industry with recommended assembly torque limits for commonly used aircraft propulsion system threaded fasteners when a common torque value per size is the objective.

Standard

Torque Tightening Threaded Fasteners

2018-03-04

CURRENT

AIR1471B

The purpose of this SAE Aerospace Information Report (AIR) is to provide the aerospace propulsion industry with recommended assembly torque limits for commonly used aircraft propulsion system threaded fasteners when a common torque value per size is the objective.

Standard

Torque Tightening Metric Screw Threaded Fasteners

2006-05-03

HISTORICAL

AIR1551A

This AIR supplies information on recommended assembly torque limits for tension type nuts and bolts of the materials and plating combinations given in Table 1.

Standard

Torque Tightening Metric Screw Threaded Fasteners

2014-07-29

CURRENT

AIR1551B

This AIR supplies information on recommended assembly torque limits for tension type nuts and bolts of the materials and plating combinations given in Table 1.

Standard

TORQUE TIGHTENING THREADED FASTENERS

1995-05-01

HISTORICAL

AIR1471

To supply information on recommended assembly torque limits for tension type nuts and bolts of the following materials and plating combinations given in Table I.

Standard

TORQUE TIGHTENING METRIC SCREW THREADED FASTENERS

1982-11-01

HISTORICAL

AIR1551

This AIR supplies information on recommended assembly torque limits for tension type nuts and bolts of the materials and plating combinations given in Table I.

Standard

TABLES OF LIMITS AND LIMITS AND LUBRICATION CHARTS

1944-05-01

HISTORICAL

AS176

This specification covers the requirements for the preparation of Tables of Limits and Limits and Lubrication Charts in published form.

Standard

Studs, Steel, UNS S66286 Tensile Strength 130 ksi 1800 °F Solution Heat Treated, Aged Before Roll Threading Procurement Specification

2021-10-28

CURRENT

AS7482C

This specification covers studs made from a corrosion and heat resistant, precipitation hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286.

Standard

Studs, Steel, UNS S66286 Aged After Roll Threaded Procurement Specification For

2015-02-17

CURRENT

AS7481C

This procurement specification covers studs made from a corrosion and heat resistant age hardenable iron base alloy of the type identified under Unified Numbering System as UNS S66286 and of 130 ksi tensile strength at room temperature, with maximum test temperature of parts at 1200 °F.

Standard

Studs, Steel, Low Alloy, Heat-Resistant Normalized and Tempered, Roll Threaded 135000 psi Tensile Strength

2022-07-06

CURRENT

AS7458C

This procurement specification covers aircraft quality studs made from a low-alloy, heat-resistant steel of the type identified under the Unified Numbering System as UNS K14675.

Standard

Studs, Steel, Low Alloy, Heat Resistant Normalized and Tempered, Roll Threaded 135000 psi Tensile Strength

2016-01-15

HISTORICAL

AS7458B

This procurement specification covers aircraft quality studs made from a low alloy, heat resistant steel of the type identified under the Unified Numbering System as UNS K14675.

Standard

Studs, Steel, Low Alloy, Heat Resistant Normalized and Tempered, Roll Threaded 135 000 psi Tensile Strength

2006-05-08

HISTORICAL

AS7458

This procurement specification covers aircraft quality studs made from a low alloy, heat resistant steel of the type identified under the Unified Numbering System as UNS K14675, and of 135 000 psi tensile strength at room temperature.

Standard

Studs, Steel, Low Alloy, Heat Resistant Normalized and Tempered, Roll Threaded 135 000 psi Tensile Strength

2009-07-20

HISTORICAL

AS7458A

This procurement specification covers aircraft quality studs made from a low alloy, heat resistant steel of the type identified under the Unified Numbering System as UNS K14675.

Standard

Studs, Steel, Low Alloy Heat Treated, Roll Threaded

2006-05-08

HISTORICAL

AS7456

This procurement specification covers aircraft quality studs made from a low alloy steel of the type identified under the Unified Numbering System as UNS G87400, and of a series of room temperature tensile strengths ranging from 125 000 psi to 185 000 psi.

Standard

Studs, Steel, Low Alloy Heat Treated, Roll Threaded

2010-06-24

HISTORICAL

AS7456B

This procurement specification covers aircraft quality studs made from a low alloy steel of the type identified under the Unified Numbering System as UNS G87400, and of a series of room temperature tensile strengths ranging from 125 000 psi to 185 000 psi.