Стандарты ASTM

ASTM E466-96(2002)e1

Заменен

Standard Practice for Conducting Force Controlled Constant Amplitude Axial Fatigue Tests of Metallic Materials — 5 стр.

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Ссылочные документы

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Standard Practice for Presentation of Constant Amplitude Fatigue Test Results for Metallic Materials — 6 стр.

ASTM E467-08

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ASTM E739-91(2004)e1

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ASTM E1823-09b

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ASTM E606-04e1

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ASTM E1012-05

Заменен

Standard Practice for Verification of Test Frame and Specimen Alignment Under Tensile and Compressive Axial Force Application — 11 стр.

ASTM E466-07

Заменен

Standard Practice for Conducting Force Controlled Constant Amplitude Axial Fatigue Tests of Metallic Materials — 5 стр.

ASTM E466-96

Заменен

Standard Practice for Conducting Force Controlled Constant Amplitude Axial Fatigue Tests of Metallic Materials — 5 стр.

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ASTM E466-07

Заменен

Standard Practice for Conducting Force Controlled Constant Amplitude Axial Fatigue Tests of Metallic Materials — 5 стр.

ASTM E466-96

Заменен

Standard Practice for Conducting Force Controlled Constant Amplitude Axial Fatigue Tests of Metallic Materials — 5 стр.

SAE AMS4351

Заменен

Aluminum Alloy, Plate (7065-T7651) 7.7Zn - 2.1Cu - 1.65Mg - 0.10Zr Solution Heat Treated, Stress-Relieved, and Overaged

SAE AMS4361

Заменен

Aluminum Alloy, Plate (7065-T7451) 7.7Zn - 2.1Cu - 1.65Mg - 0.10Zr Solution Heat Treated, Stress-Relieved, and Overaged

SAE AMS2355L

Заменен

Quality Assurance, Sampling and Testing Aluminum Alloys and Magnesium Alloy Wrought Products (Except Forging Stock), and Rolled, Forged, or Flash Welded Rings

SAE AMS2355K

Заменен

Quality Assurance, Sampling and Testing Aluminum Alloys and Magnesium Alloy Wrought Products (Except Forging Stock), and Rolled, Forged, or Flash Welded Rings

SAE AMS2355M

Действует

Quality Assurance, Sampling and Testing Aluminum Alloys and Magnesium Alloy Wrought Products (Except Forging Stock), and Rolled, Forged, or Flash Welded Rings

SAE AMS4351A

Действует

Aluminum Alloy, Plate (7065-T7651) 7.7Zn - 2.1Cu - 1.65Mg - 0.10Zr Solution Heat Treated, Stress-Relieved, and Overaged

SAE AMS4361A

Действует

Aluminum Alloy, Plate (7065-T7451) 7.7Zn - 2.1Cu - 1.65Mg - 0.10Zr Solution Heat Treated, Stress-Relieved, and Overaged

SAE AMS4050K

Действует

Aluminum Alloy, Plate 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T7451) Solution Heat Treated, Stress Relieved, and Overaged

SAE AMS4050G

Заменен

Aluminum Alloy, Plate 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T7451) Solution Heat Treated, Stress Relieved, and Overaged

SAE AMS4050H

Заменен

Aluminum Alloy, Plate 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T7451) Solution Heat Treated, Stress Relieved, and Overaged

SAE AMS4050J

Заменен

Aluminum Alloy, Plate 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T7451) Solution Heat Treated, Stress Relieved, and Overaged

SAE AMS2355J

Заменен

Quality Assurance, Sampling and Testing Aluminum Alloys and Magnesium Alloy Wrought Products (Except Forging Stock), and Rolled, Forged, or Flash Welded Rings

SAE AIR4498A

Действует

Aus-Bay Quenching of 300M Steel (Stabilized: May 2012)

SAE AIR4498

Заменен

AUS-BAY QUENCHING OF 300M STEEL

SAE AMS4249B

Действует

Aluminum Alloy Castings 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated (Requiring Fatigue and Fracture Toughness Testing)

SAE AMS4249A

Заменен

Aluminum Alloy Castings 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated (Requiring Fatigue and Fracture Toughness Testing)

SAE AMS4249

Заменен

ALUMINUM ALLOY CASTINGS 7.0Si - 0.58Mg - 0.15Ti - 0.06Be (D357.0-T6) Solution and Precipitation Heat Treated (Requiring Fatigue and Fracture Toughness Testing)

SAE MA4872

Заменен

Paint Stripping of Commercial Aircraft - Evaluation of Materials and Processes

SAE MA4872A

Действует

Paint Stripping of Commercial Aircraft - Evaluation of Materials and Processes

SAE AMS4211B

Заменен

Aluminum Alloy, Plate 6.2Zn - 1.9Cu - 2.1Mg - 0.10Zr (7040-T7451) Solution Heat Treated, Stress Relieved, and Overaged

SAE AMS4211A

Заменен

Aluminum Alloy, Plate 6.2Zn - 1.9Cu - 2.1Mg - 0.10Zr (7040-T7451) Solution Heat Treated, Stress Relieved, and Overaged

SAE AMS4211C

Действует

Aluminum Alloy, Plate 6.2Zn - 1.9Cu - 2.1Mg - 0.10Zr (7040-T7451) Solution Heat Treated, Stress Relieved, and Overaged

SAE AS7101C

Действует

National Aerospace and Defense Contractors Accreditation Program (NADCAP) General Requirements for Materials Test Laboratory Accreditation Program

SAE AS7101B

Заменен

NATIONAL AEROSPACE AND DEFENSE CONTRACTORS ACCREDITATION PROGRAM (NADCAP) GENERAL REQUIREMENTS FOR MATERIALS TEST LABORATORY ACCREDITATION PROGRAM

SAE AS7101A

Заменен

NATIONAL AEROSPACE AND DEFENSE CONTRACTORS ACCREDITATION PROGRAM (NADCAP) GENERAL REQUIREMENTS FOR MATERIALS TESTING LABORATORY ACCREDITATION PROGRAM

SAE AMS4050F

Заменен

Aluminum Alloy, Plate 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T7451) Solution Heat Treated, Stress Relieved, and Overaged

SAE AMS4211

Заменен

Aluminum Alloy, Plate 6.2Zn - 1.9Cu - 2.1Mg - 0.10Zr (7040-T7451) Solution Heat Treated, Stress Relieved, and Overaged