Standard
Water Compatibility of Aircraft Greases
1995-05-01
CURRENT
AIR39
Search Results
Standard
Washers, Spring Lock, Carbon Steel, Procurement Specification for
2015-02-24
CURRENT
AS7240A
This procurement specification covers plain helical lock washers fabricated from heat treated carbon steel.
Standard
Washers, Spring Lock, Carbon Steel, Procurement Specification for
2006-11-07
HISTORICAL
AS7240
This procurement specification covers plain helical lock washers fabricated from heat treated carbon steel.
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
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.
Standard
Studs, Steel, Low Alloy Heat Treated, Roll Threaded
2021-08-12
CURRENT
AS7456C
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 125000 to 185000 psi.
Standard
Studs, Steel, Low Alloy Heat Treated, Roll Threaded
2009-07-20
HISTORICAL
AS7456A
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, Corrosion and Heat Resistant Steel, UNS S66286, Tensile Strength 900 MPa, Procurement Specification, Metric
2024-01-22
CURRENT
MA3375E
This document covers metric studs made from a corrosion and heat resistant, age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286. The following specification designations and their properties are covered:
Standard
Studs, Corrosion and Heat Resistant Steel, UNS S66286 Tensile Strength 900 MPa, Procurement Specification, Metric
2011-08-08
HISTORICAL
MA3375C
This document covers metric studs made from a corrosion and heat resistant, age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286. The following specification designations and their properties are covered:
Standard
Studs, Corrosion and Heat Resistant Steel, UNS S66286 Tensile Strength 130 ksi 1800 °F Solution Heat Treated, Aged Before Roll Threading Procurement Specification
2015-04-29
HISTORICAL
AS7482B
This specification covers studs made from a corrosion and heat resistant, age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286. The following specification designations and their properties are covered:
Standard
Stud, Locked In, Ring Locked, Serrated, General Specification For
2007-07-05
HISTORICAL
AS45909
The specification covers the requirements for locked-in studs. The method of locking in the stud is by means of a serrated collar and an accessory lockring with matching serrations installed within the parent material to prevent rotation.
Standard
Stability of Aircraft Greases
1995-05-01
CURRENT
AIR41
The purpose of this information report is to summarize and document data regarding possible alternatives to the use of cadmium plating on hardware typical of the aerospace hose and fitting industry. To document and provide access to information obtained by an industry survey.
