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2014-07-21
WIP Standard
AIR4923A
This SAE Aerospace Information Report (AIR) provides a tabular listing of materials, procurement specifications, and mechanical properties for bolts and screws developed for use on aerospace propulsion systems designed using the U.S. customary system or the SI system.

The list is intended to give a brief overview of the various kinds of SAE aerospace procurement specifications available when developing bolt and screw part standards.

CURRENT
1996-05-01
Standard
AIR4923
This SAE Aerospace Information Report (AIR) provides a tabular listing of materials, procurement specifications, and mechanical properties for bolts and screws developed for use on aerospace propulsion systems designed using the U.S. customary system or the SI system.
CURRENT
2017-08-17
Standard
AMS7464D
This specification covers premium quality bolts and screws made from a low-alloy, heat-resistant steel and having threads of UNJ (MIL-S-8879) form.
HISTORICAL
1976-01-31
Standard
AMS7464C
This specification covers premium quality bolts and screws made from a low-alloy, heat-resistant steel and having threads of UNJ (MIL-S-8879) form.
CURRENT
2017-05-09
Standard
ARP1231B
This document establishes general gland design criteria for static and dynamic O-ring seal applications used in fluid systems and at fluid pressures common to the aerospace industry. Detailed discussion of design criteria and tables of recommended gland dimensions are contained in the documents listed in Table 1. SI unit conversions for U.S. customary units have been provided for reference purposes.
HISTORICAL
1943-07-01
Standard
ARP142
This specification covers a suggested procedure for the assembling of cadmium plated steel studs with rolled threads into cast or forged aluminum and magnesium.
CURRENT
2013-12-19
Standard
ARP142C
This document covers the recommended basics to be considered when assembling cadmium plated steel studs with rolled threads into cast, or forged, aluminum or magnesium parts.
HISTORICAL
1954-06-15
Standard
ARP142A
HISTORICAL
2004-02-23
Standard
ARP142B
This document covers the recommended basics to be considered when assembling cadmium plated steel studs with rolled threads into cast, or forged, aluminum or magnesium parts.
CURRENT
2017-07-26
Standard
AS123301D
CURRENT
2012-03-13
Standard
AS125701B
HISTORICAL
1974-05-01
Standard
AS125701A
HISTORICAL
1995-11-01
Standard
AS125701
HISTORICAL
1995-11-01
Standard
AS125251
HISTORICAL
1974-05-01
Standard
AS125251A
CURRENT
2001-10-01
Standard
ARP573D
This recommended practice covers design requirements for silver, copper and nickel brazed joints, primarily for tube connections, for aerospace propulsion systems. The environmental conditions stated herein, and those given in the applicable AMS specifications, provide the limitations of this ARP.
HISTORICAL
1979-11-01
Standard
ARP573C
This recommended practice covers design requirements for silver, copper and nickel brazed joints, primarily for tube connections, for aerospace propulsion systems. The environmental conditions stated herein, and those given in the applicable AMS specifications, provide the limitations of this ARP.
HISTORICAL
1969-08-15
Standard
ARP573B
This recommended practice covers design requirements for silver and copper brazed joints, primarily for tube connections, for aerospace propulsion systems. The environmental conditions stated herein, and those given in the applicable AMS specifications, provide the limitations of this ARP.
HISTORICAL
1960-11-15
Standard
ARP573A
This ARP provides data for silver, copper, and nickel alloy brazed joints, based on sound engineering principles currently used throughout the aerospace propulsion systems industry, and provides a recommended practice for appropriate design configurations, engine and propeller standard utility parts, as applicable, and other propulsion systems components. It further establishes a common standard practice for swaged tubing and a common standard for the inside diameter of the mating part of fittings for either silver, copper or nickel brazed joints. The purpose of establishing a common inside diameter for brazing applications is to facilitate manufacturing and to reduce the cost of related parts.
Viewing 1 to 30 of 295