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Viewing 1 to 30 of 2470
CURRENT
1997-03-01
Standard
AIR1936A
This study addresses the adequacy of sockets, wrenches, and torque adapters conforming to AS954 to wrench 12 point fasteners with wrenching configurations conforming to AS870C. Reported wrenching problems with smaller sizes are investigated through examining the combined tolerances on the fasteners and wrenches, conducting torque testing on typical high strength lock nuts. Possible solutions to correct these wrenching problems are presented.
HISTORICAL
1985-03-01
Standard
AIR1936
This study addresses the adequacy of sockets, wrenches, and torque adapters conforming to AS954 to wrench 12 point fasteners with wrenching configurations conforming to AS870C. Reported wrenching problems with smaller sizes are investigated through examining the combined tolerances on the fasteners and wrenches, conducting torque testing on typical high strength lock nuts. Possible solutions to correct these wrenching problems are presented.
CURRENT
1988-01-01
Standard
AIR1758
This information report provides guidance when the ISO International metric tolerance system for limits and fits per ISO/R286 or ANSI B4.2-1978 is applied on a standard, and also provides a selected series of limits and fits for powerplant construction suitable for holes and shafts up to 500 mm. For holes or shafts over 500 mm or for limits and fits not shown, ISO/R286 should be consulted.
CURRENT
2003-03-19
Standard
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.
CURRENT
1983-11-01
Standard
AIR3260
This information report presents recommendations on part number marking which provides for the maximum identification on bolts and nuts while ensuring adequate readability.
2017-11-18
WIP Standard
AIR809B
Data are related to the dimensional changes with respect to room temperature and provide accuracy sufficient for use with most aerospace systems. Two basic methods of solution are presented with examples for steady state conditions involving uniform and non-uniform temperature distributions. The answers to the example problems are carried to the fifth place for a comparison of the results between methods I and II.
HISTORICAL
1970-11-01
Standard
AMS2373
HISTORICAL
1987-10-01
Standard
AMS2373A
CURRENT
1998-07-01
Standard
AMS2373B
This specification has been declared NONCURRENT by the Aerospace Materials Division, SAE, as of May, 1990.
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.
HISTORICAL
1999-08-01
Standard
AIR5065
Performed tensile and fatigue tests on bolts to determine if cutting of materials flow lines at the bolt underhead would degrade bolt integrity. Five different alloys used in aerospace industry fatigue critical applications were employed to fabricate 5/16 to 1/2 inch diameter bolts. These bolts were machined from bar stock producing fully cut material flow lines under their heads. Tensile testing with and without underhead washers was performed along with industry standard fatigue testing.
CURRENT
2012-05-09
Standard
AIR5065A
Performed tensile and fatigue tests on bolts to determine if cutting of materials flow lines at the bolt underhead would degrade bolt integrity. Five different alloys used in aerospace industry fatigue critical applications were employed to fabricate 5/16 to 1/2 inch diameter bolts. These bolts were machined from bar stock producing fully cut material flow lines under their heads. Tensile testing with and without underhead washers was performed along with industry standard fatigue testing.
HISTORICAL
1982-02-15
Standard
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.
2017-11-18
WIP Standard
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.
CURRENT
2000-04-01
Standard
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.
CURRENT
1999-09-01
Standard
AIR1397A
This report presents the material properties and test requirements for an injection molded thermoplastic compound utilized for fabrication of AS1396 clamp block assembly.
HISTORICAL
1976-05-01
Standard
AIR1397
CURRENT
2001-10-01
Standard
AIR809A
Data are related to the dimensional changes with respect to room temperature and provide accuracy sufficient for use with most aerospace systems. Two basic methods of solution are presented with examples for steady state conditions involving uniform and non-uniform temperature distributions. The answers to the example problems are carried to the fifth place for a comparison of the results between Methods I and II.
HISTORICAL
1964-03-01
Standard
AIR809
DATA ARE RELATED TO THE DIMENSIONAL CHANGES WITH RESPECT TO ROOM TEMPERATURE AND PROVIDE ACCURACY SUFFICIENT FOR USE WITH MOST AEROSPACE SYSTEMS. TWO BASIC METHODS OF SOLUTION ARE PRESENTED WITH EXAMPLES FOR STEADY STATE CONDITIONS INVOLVING UNIFORM AND NON-UNIFORM TEMPERATURE DISTRIBUTIONS. THE ANSWERS TO THE EXAMPLE PROBLEMS ARE CARRIED TO THE FIFTH PLACE FOR A COMPARISON OF THE RESULTS BETWEEN METHODS I AND II.
HISTORICAL
1952-11-01
Standard
AMS7205
This specification covers tubular-shaped pins, fabricated from carbon steel, having a full-length longitudinal slot to permit flexure when inserted into a hole.
HISTORICAL
1957-07-01
Standard
AMS7205A
This specification covers tubular-shaped pins, fabricated from carbon steel, having a full-length longitudinal slot to permit flexure when inserted into a hole.
HISTORICAL
1966-09-01
Standard
AMS7205C
This specification covers tubular-shaped pins, fabricated from carbon steel, having a full-length longitudinal slot to permit flexure when inserted into a hole.
HISTORICAL
1961-01-01
Standard
AMS7205B
This specification covers tubular-shaped pins, fabricated from carbon steel, having a full-length longitudinal slot to permit flexure when inserted into a hole.
HISTORICAL
1973-12-01
Standard
AMS7205D
This specification covers tubular-shaped pins, fabricated from carbon steel, having a full-length longitudinal slot to permit flexure when inserted into a hole.
HISTORICAL
1979-10-15
Standard
AMS7205E
This specification covers tabular-shaped pins, fabricated from carbon steel, having a full-length longitudinal slot to permit flexure when inserted into a hole.
HISTORICAL
2003-02-21
Standard
AMS7205F
This specification covers tubular-shaped pins, fabricated from carbon steel, having a full-length longitudinal slot to permit flexure when inserted into a hole.
CURRENT
2008-02-15
Standard
AMS7205G
This specification covers tubular-shaped pins, fabricated from carbon steel, having a full-length longitudinal slot to permit flexure when inserted into a hole.
Viewing 1 to 30 of 2470

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