Standard
BLADE OR VANE - DIMENSIONING OF TURBINE ENGINE AIRFOIL
1996-05-01
HISTORICAL
ARP265
Search Results
Standard
High Strength Elevated Temperature Bolting Practice
2018-08-23
HISTORICAL
ARP700B
This SAE Aerospace Recommended Practice (ARP) provides general information on the design and installation of threaded fasteners in high strength and high temperature applications in propulsion systems. Some of the more common definitions of fastener terminology are also provided.
Standard
High Strength Elevated Temperature Bolting Practice
2019-05-03
CURRENT
ARP700C
This SAE Aerospace Recommended Practice (ARP) provides general information on the design and installation of threaded fasteners in high strength and high temperature applications in propulsion systems. Some of the more common definitions of fastener terminology are also provided.
Standard
Nuts, Self-Locking, UNS S66286 Classification: 220 ksi/850 °F Procurement Specification
2006-10-11
HISTORICAL
AS4726
This specification establishes the requirements for self-locking nuts, wrenching type (i.e., hexagon, double hexagon, and spline drive), made of a corrosion and heat resistant steel of the type identified under the Unified Numbering System as UNS S66286.
Standard
Nuts, Self-Locking, UNS S66286 Classification: 220 ksi/850 °F Procurement Specification
2017-02-23
CURRENT
AS4726A
This specification establishes the requirements for self-locking nuts, wrenching type (i.e., hexagon, double hexagon, and spline drive), made of a corrosion and heat resistant steel of the type identified under the Unified Numbering System as UNS S66286.
Standard
Nut, Hex, Free Running, Procurement Specification For, Metric
2018-01-29
CURRENT
MA1937A
This procurement specification covers alloy steel and corrosion and heat resistant steel free running metric nuts of the following types, styles and classes.
Standard
Washer, Thermal Compensating, Metric Series
2019-02-18
CURRENT
AIR1754B
The purpose of this document is to define: - compensation washer application requirements - recommended materials - washer thickness determination - dimensioning
Standard
Washer, Thermal Compensating, Metric Series
2012-10-19
HISTORICAL
AIR1754A
The purpose of this document is to define: - compensation washer application requirements - recommended materials - washer thickness determination - dimensioning
Standard
WASHER, THERMAL COMPENSATING, METRIC SERIES
1995-05-01
HISTORICAL
AIR1754
The purpose of this document is to define: - compensation washer application requirements - recommended materials - washer thickness determination - dimensioning
Standard
Control Lever Connections (60° V Serrations)
2012-11-02
HISTORICAL
ARP260D
This SAE Aerospace Recommended Practice (ARP) provides the definition for a control lever connection with 60° "V" serrations for aircraft engine to aircraft power or control levers.
Standard
CONTROL LEVER CONNECTIONS (60° V SERRATIONS)
1995-05-01
HISTORICAL
ARP260C
Standard
Control Lever Connections (60° V Serrations)
2018-04-28
CURRENT
ARP260E
This SAE Aerospace Recommended Practice (ARP) provides the definition for a control lever connection with 60° "V" serrations for aircraft engine to aircraft power or control levers.
Standard
Nut, Self-Locking, Nickel Alloy, UNS N07001, 1400 °F, 180,000 psi, UNJ Thread Procurement Specification
2018-11-21
CURRENT
AS5878
This specification establishes the requirements for the following types of self-locking nuts in thread diameter sizes 0.1380 through 0.6250 inches: a Wrenching Nuts: i.e., hexagon, double hexagon and spline nuts. b Anchor Nuts: i.e., plate nuts, gang channel nuts, and shank nuts. The wrenching nuts, shank nuts, and nut elements of plate and gang channel nuts are made of a corrosion and heat resistant nickel-base alloy of the type identified under the Unified Numbering System as UNS N07001 and of 180,000 psi axial tensile strength at room temperature, with maximum conditioning of parts at 1400 °F prior to room temperature testing.
Standard
Rivets, Solid and Tubular, Nickel Alloy Corrosion and Heat Resistant 74Ni - 15.5Cr - 8.0Fe Procurement Specification For
2012-11-19
HISTORICAL
AS7232
This procurement specification covers aircraft quality solid rivets and tubular end rivets made from a corrosion and heat resistant nickel base alloy of the type identified under the Unified Numbering System as UNS N06600.
Standard
Rivets, Solid and Tubular, Nickel Alloy Corrosion and Heat Resistant 74Ni - 15.5Cr - 8.0Fe Procurement Specification For
2018-08-23
HISTORICAL
AS7232A
This procurement specification covers aircraft quality solid rivets and tubular end rivets made from a corrosion and heat resistant nickel base alloy of the type identified under the Unified Numbering System as UNS N06600.
Standard
Nuts, Self-Locking, Steel, Corrosion and Heat Resistant High Strength, All Metal 1200 °F Use, UNJ Thread Form
2020-02-03
CURRENT
AS7251C
This document covers all metal, self-locking wrenching nuts, plate nuts, shank nuts, and gang channel nuts made from a corrosion and heat resistant steel of the type identified under the Unified Numbering System as UNS S66286 and of 160 ksi tensile strength at room temperature, with maximum test temperature of parts at 1200 °F.
Standard
NUTS, SELF-LOCKING, STEEL, CORROSION AND HEAT RESISTANT HIGH STRENGTH, ALL METAL 1200 °F USE, UNJ THREAD FORM
1995-05-01
HISTORICAL
AS7251A
This document covers all metal, self-locking wrenching nuts, plate nuts, shank nuts, and gang channel nuts made from a corrosion and heat resistant steel of the type identified under the Unified Numbering System as UNS S66286 and of 160 ksi tensile strength at room temperature, with maximum test temperature of parts at 1200 °F.
Standard
Nuts, Self-Locking, Steel, Corrosion and Heat Resistant High Strength, All Metal 1200 °F Use, UNJ Thread Form
2006-10-11
HISTORICAL
AS7251B
This document covers all metal, self-locking wrenching nuts, plate nuts, shank nuts, and gang channel nuts made from a corrosion and heat resistant steel of the type identified under the Unified Numbering System as UNS S66286 and of 160 ksi tensile strength at room temperature, with maximum test temperature of parts at 1200 °F.
Standard
FASTENER TORQUE FOR THREADED APPLICATIONS, DEFINITIONS OF
1975-01-01
HISTORICAL
AS1310
Standard
FASTENER TORQUE FOR THREADED APPLICATIONS, DEFINITIONS OF
1994-10-01
HISTORICAL
AS1310A
This SAE Aerospace Standard (AS) is intended for use by those involved in the design of aircraft, missile, or space systems, and their support equipment to define the various types of fastener torque.
