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SAE
SAE AMSS6049B
Действует
Steel, Chrome-Nickel-Molybdenum (8740) Bars and Reforging Stock (Aircraft Quality)
Описание
Изменения
Ссылки
Версии
Ссылочные документы
SAE AMS2251J
Действует
Tolerances Low-Alloy Steel Bars
SAE AMS2301L
Действует
Steel Cleanliness, Aircraft Quality Magnetic Particle Inspection Procedure
SAE AMS2640K
Действует
MAGNETIC PARTICLE INSPECTION
SAE AMSS6049A
Заменен
Steel, Chrome-Nickel-Molybdenum (8740) Bars and Reforging Stock (Aircraft Quality) (Noncurrent: Sep 2002)
На этот документ ссылаются
SAE AMSS6049A
Заменен
Steel, Chrome-Nickel-Molybdenum (8740) Bars and Reforging Stock (Aircraft Quality) (Noncurrent: Sep 2002)
SAE AMSS6049
Заменен
Steel, Chrome-Nickel-Molybdenum (8740) Bars and Reforging Stock (Aircraft Quality)
SAE AMS6327M
Действует
Steel Bars and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 125 ksi (862 MPa) Tensile Strength
SAE AMS6327J
Заменен
Steel Bars and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 125 ksi (862 MPa) Tensile Strength
SAE AMS6327L
Заменен
Steel Bars and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 125 ksi (862 MPa) Tensile Strength
SAE AMS6327H
Заменен
Steel Bars and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 125 ksi (862 MPa) Tensile Strength
SAE AMS6327K
Заменен
Steel Bars and Forgings 0.50Cr - 0.55Ni - 0.25Mo (0.38 - 0.43C) (SAE 8740) Heat Treated, 125 ksi (862 MPa) Tensile Strength