Standard
ACCEPTANCE CRITERIA - MAGNETIC PARTICLE, FLUORESCENT PENETRANT, AND CONTRAST DYE PENETRANT INSPECTION
1995-05-01
HISTORICAL
AS3071A
Search Results
Standard
ACCEPTANCE CRITERIA - MAGNETIC PARTICLE, FLUORESCENT PENETRANT, AND CONTRAST DYE PENETRANT INSPECTION
1971-10-01
HISTORICAL
AS3071
Standard
ALUMINUM RIVETS, UNS A92117 2.5Cu - 0.3Mg (2117-T4)
1995-05-01
HISTORICAL
AS7222
This procurement specification covers rivets fabricated from an aluminum alloy designated as 2117-T4, solution treated.
Standard
AREAS FOR CALCULATING STRESS OR LOAD VALUES FOR METRIC MJ EXTERNALLY THREADED FASTENERS
2002-07-23
CURRENT
AS1520
Areas for the standard metric series of thread diameter-pitch combinations for aerospace externally threaded fasteners are established for the following conditions: a) Area for ultimate shear stress or load in unthreaded shank. b) Area for ultimate tensile stress or load in thread. c) Area for stress durability test load in thread. d) Area for stress-rupture test load at elevated temperature. e) Area for tension-tension fatigue test load.
Standard
ASSEMBLING OF STUDS IN ALUMINUM AND MAGNESIUM
1995-05-01
HISTORICAL
ARP142A
Standard
ASSEMBLY NUT AND CLIP, REMOVABLE SELF-LOCKING NUT, UNS S66286
2006-05-03
HISTORICAL
AS3547
Standard
ASSEMBLY NUT AND CLIP, REMOVABLE SELF-LOCKING NUT, UNS S66286
2016-07-22
HISTORICAL
AS3547A
Standard
ASSEMBLY NUT AND CLIP, REMOVABLE SELF-LOCKING NUT, UNS S66286, CLASS 160 KSI/1200 °F
2020-10-06
CURRENT
AS3547B
Standard
ASSEMBLY NUT, PLATE, REMOVABLE SELF-LOCKING NUT
2012-11-01
HISTORICAL
AS3550
Standard
Acceptance Criteria - Magnetic Particle, Fluorescent Penetrant, and Contrast Dye Penetrant Inspection
2018-10-26
CURRENT
AS3071C
To establish the acceptance criteria for discontinuities as revealed by magnetic particle or liquid penetrant examination of aircraft utility parts as in 1.2.
Standard
Acceptance Criteria - Magnetic Particle, Fluorescent Penetrant, and Contrast Dye Penetrant Inspection
2012-11-01
HISTORICAL
AS3071B
To establish the acceptance criteria for discontinuities as revealed by magnetic particle or liquid penetrant examination of aircraft utility parts as in 1.2.
Standard
Acceptance Criteria for Nuts - Magnetic Particle, Fluorescent Penetrant, and Visible Penetrant Examination
2018-08-23
HISTORICAL
AS5447
This standard establishes the acceptance criteria for surface discontinuities as revealed by magnetic particle or liquid penetrant examination of nuts.
Standard
Aluminum Rivets, UNS A91100, 99Al (1100-H14)
2006-05-04
HISTORICAL
AS7220
This procurement specification covers rivets fabricated from an aluminum alloy designated as 1100-H14, strain hardened.
Standard
Aluminum Rivets, UNS A91100, 99Al (1100-H14)
2022-03-30
CURRENT
AS7220A
This procurement specification covers rivets fabricated from an aluminum alloy designated as 1100-H14, strain hardened.
Standard
Aluminum Rivets, UNS A92117 2.5Cu - 0.3Mg (2117-T4) Procurement Specification
2018-11-21
HISTORICAL
AS7222A
This procurement specification covers rivets made from an aluminum alloy designated as 2117-T4, solution treated. The following specification designations and their rivet coatings are covered:
Standard
Areas for Calculating Stress or Load Values for Externally and Internally Threaded Fasteners
2018-08-23
HISTORICAL
AS5054A
This standard specifies the areas to be used in calculating stress or load values to be used in externally and internally threaded fastener procurement specifications for bolts, screws, nuts, and studs and for the information of designers.
Standard
Areas for Calculating Stress or Load Values for Externally and Internally Threaded UNJ Fasteners
2004-02-23
HISTORICAL
AS5054
This standard specifies the areas to be used in calculating stress or load values for use in externally and internally threaded fastener procurement specifications for bolts, nuts, and studs and for the information of designers.
Standard
Areas for Calculating Stress or Load Values for Metric MJ Externally Threaded Fasteners
2018-08-23
HISTORICAL
MA1520A
Areas for the standard metric series of thread diameter-pitch combinations for aerospace externally threaded fasteners are established for the following conditions: a Area for ultimate shear stress or load in unthreaded shank. b Area for ultimate tensile stress or load in thread. c Area for stress durability test load in thread. d Area for stress-rupture test load at elevated temperature. e Area for tension-tension fatigue test load.
Standard
Areas for Calculating Stress or Load Values for Metric MJ Externally Threaded Fasteners
2019-05-03
CURRENT
MA1520B
Areas for the standard metric series of thread diameter-pitch combinations for aerospace externally threaded fasteners are established for the following conditions: a Area for ultimate shear stress or load in unthreaded shank. b Area for ultimate tensile stress or load in thread. c Area for stress durability test load in thread. d Area for stress-rupture test load at elevated temperature. e Area for tension-tension fatigue test load.
Standard
Areas for Calculating Stress or Load Values for Metric MJ Internally Threaded Fasteners
2019-05-03
CURRENT
MA4284A
Areas for the standard metric series of threaded diameter-pitch combinations for aerospace internally threaded fasteners are established for the following conditions: a Area for shear stress or load in fastener thread b Area for ultimate tensile stress or load in thread
