Standard
Water Compatibility of Aircraft Greases
1995-05-01
CURRENT
AIR39
Search Results
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, 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
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
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
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.
Standard
STUD, LOCKED IN-RING LOCKED, SERRATED
2018-09-28
CURRENT
AS51989C
Standard
STUD, LOCKED IN-RING LOCKED, SERRATED
1999-04-01
HISTORICAL
AS51989
Standard
STUD, LOCKED IN-RING LOCKED, SERRATED
2014-04-24
HISTORICAL
AS51989A
Standard
STUD, LOCKED IN-RING LOCKED, SERRATED
2016-04-20
HISTORICAL
AS51989B
Standard
Performance, Nut, Self-Locking, Castellated, Prevailing Torque, UNJ 16 Pitch Thread Form
2024-01-16
CURRENT
AS4958B
This document covers all metal, castellated, self-locking nuts made from alloy steel of the types identified under the Unified Numbering System as UNS G41300 and UNS G43400.
Standard
Performance, Nut, Self-Locking, Castellated, Prevailing Torque, UNJ 16 Pitch Thread Form
2006-05-04
HISTORICAL
AS4958
This document covers all metal, castellated, self-locking nuts made from alloy steel of the types identified under the Unified Numbering System as UNS G41300 and UNS G43400.
Standard
PROPELLER SHAFT ENDS - DUAL ROTATION (ENGINE SUPPLIED BEARING)
1947-12-01
HISTORICAL
AIR18
Standard
PLUG, EXPANSION - TAPERED, AMS 5040
2002-02-13
HISTORICAL
AS91761
Standard
PIN, HINGE CORROSION RESISTANT STEEL UNS S30200, UNS S30400, OR UNS S31600
2014-01-09
HISTORICAL
AS20253A
Standard
PIN, HINGE
2012-11-01
HISTORICAL
AS20253
Standard
Operating Instructions for Aircraft Engines (Preparation of)
2018-09-11
CURRENT
AS177C
This specification covers the requirements for format and outline of contents of operating instructions in published form or in manuscript form suitable for publication.
Standard
Operating Instructions for Aircraft Engines (Preparation of)
2012-11-01
HISTORICAL
AS177B
This specification covers the requirements for format and outline of contents of operating instructions in published form or in manuscript form suitable for publication.
Standard
OPERATING INSTRUCTIONS FOR AIRCRAFT ENGINES (PREPARATION OF)
1995-05-01
HISTORICAL
AS177A
This specification covers the requirements for format and outline of contents of operating instructions in published form or in manuscript form suitable for publication.
