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СтандартыSAE

SAE AMS2487C

Действует
Anodic Treatment of Titanium and Titanium Alloys, Solution pH 12.4 Maximum
ОписаниеИзмененияСсылкиВерсии

Ссылочные документы

SAE AMS3084C
Действует
Lubricant, Solid Film Minimal Outgassing (Stabilized: Sep 2016)
SAE AMS4001J
Действует
Aluminum Sheet and Plate, 0.12Cu (1100-0), Annealed
SAE AMS4911T
Действует
Titanium Alloy, Sheet, Strip, and Plate, 6Al - 4V, Annealed
SAE AMS4928X
Действует
Titanium Alloy Bars, Wire, Forgings, Flash-Welded Rings, and Drawn Shapes, 6Al - 4V Annealed
ASTM B117-97
Заменен
Standard Practice for Operating Salt Spray (Fog) Apparatus — 8 стр.
ASTM B244-97(2002)
Заменен
Standard Test Method for Measurement of Thickness of Anodic Coatings on Aluminum and of Other Nonconductive Coatings on Nonmagnetic Basis Metals with Eddy-Current Instruments — 3 стр.
ASTM D2579-93e1
Отменен
Standard Test Method for Total Organic Carbon in Water (Withdrawn 2002) — 5 стр.
ASTM D2714-94(2019)
Заменен
Standard Test Method for Calibration and Operation of the Falex Block-on-Ring Friction and Wear Testing Machine — 4 стр.
SAE MAM4911B
Действует
Titanium Alloy, Sheet, Strip, and Plate, 6al 4v, Annealed
SAE AMS2487A
Заменен
Anodic Treatment of Titanium and Titanium Alloys Solution pH 12.4 Maximum

На этот документ ссылаются

SAE J2271M_201508
Действует
Ship Systems and Equipment - Part Standard for Studs - Continuous and Double End (Metric) (Stabilized: Aug 2015)
SAE J2295_199608
Заменен
SHIP SYSTEMS AND EQUIPMENT—FASTENERS—PART NUMBERS
SAE J2655_201509
Действует
Fastener Part Standard - Washers and Lockwashers (Inch Dimensioned)
SAE J2295_200404
Заменен
Fastener Part Standard—Caps Screws, Hex Bolts, and Hex Nuts (inch Dimensioned)
SAE J2596_200410
Заменен
Fastener Part Standard—Tapping Screws and Metallic Drive Screws (Inch Dimensioned)
SAE J2656_201611
Действует
Fastener Part Standard - Hexagon Socket, Square Head, and Slotted Headless Set Screws - Inch Dimensioned
SAE J2295M_201905
Действует
Fasteners - Part Standard - Cap Screws, Hex Bolts, and Hex Nuts (Metric) (Stabilized: May 2019)
SAE J2656_200309
Заменен
Fastener Part Standard – Hexagon Socket, Square Head, and Slotted Headless Set Screws - Inch Dimensioned
SAE J2271_200901
Заменен
Ship Systems and Equipment—Part Standard for Studs—Continuous and Double End (Inch Series)
SAE J2271M_199606
Заменен
SHIP SYSTEMS AND EQUIPMENT—PART STANDARD FOR STUDS—CONTINUOUS AND DOUBLE END (METRIC)
SAE J2295_199810
Заменен
Fasteners—Part Standard—Cap Screws, Hex Bolts, and Hex Nuts
SAE J2484_200207
Заменен
Fastener Part Standard—Machine Screws
SAE J2271_200406
Заменен
Ship Systems and Equipment - Part Standard for Studs - Continuous and Double End (Inch Series)
SAE J2271_199606
Заменен
SHIP SYSTEMS AND EQUIMENT—PART STANDARD FOR STUDS—CONTINOUS AND DOUBLE END (INCH SERIES)
SAE J2485_200301
Заменен
Fastener Part Standard - Machine Screw Nuts (Metric and Inch)
SAE AMS2487
Заменен
ANODIC TREATMENT OF TITANIUM AND TITANIUM ALLOYS Solution pH 12.4 maximum
SAE AMS2487A
Заменен
Anodic Treatment of Titanium and Titanium Alloys Solution pH 12.4 Maximum
SAE AS5951C
Заменен
Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 5080 psi (35,000 kPa), 275 °F (135 °C), Aircraft Hydraulic Systems
SAE AS5951D
Действует
Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 5080 psi (35000 kPa), 275 °F (135 °C), Aircraft Hydraulic Systems
SAE AS5951
Заменен
Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 5080 psi (35,000 kPa), 275 °F (135 °C), Aircraft Hydraulic Systems
SAE AS5951B
Заменен
Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 5080 psi (35,000 kPa), 275 °F (135 °C), Aircraft Hydraulic Systems
SAE AS5960B
Заменен
Hose Assembly, Polytetrafluoroethylene, Metallic Braid Reinforced, 5080 psi (35 000 kPa), 400 °F (204 °C), Aircraft Hydraulic Systems
SAE AS5951A
Заменен
Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 5080 psi (35,000 kPa), 275 °F (135 °C), Aircraft Hydraulic Systems
SAE AS5960C
Действует
Hose Assembly, Polytetrafluoroethylene, Metallic Braid Reinforced, 5080 psi (35000 kPa), 400 °F (204 °C), Aircraft Hydraulic Systems