ASTM D 4636 : 2017 : REDLINE
Current
The latest, up-to-date edition.
Standard Test Method for Corrosiveness and Oxidation Stability of Hydraulic Oils, Aircraft Turbine Engine Lubricants, and Other Highly Refined Oils
English
06-01-2017
CONTAINED IN VOL. 05.02, 2017 Describes the testing of hydraulic oils, aircraft turbine engine lubricants, and other highly refined oils to determine their resistance to oxidation and corrosion degradation and their tendency to corrode various metals.
Committee |
D 02
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DocumentType |
Redline
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Pages |
14
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PublisherName |
American Society for Testing and Materials
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Status |
Current
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1.1This test method covers the testing of hydraulic oils, aircraft turbine engine lubricants, and other highly refined oils to determine their resistance to oxidation and corrosion degradation and their tendency to corrode various metals. Petroleum and synthetic fluids may be evaluated using moist or dry air with or without metal test specimens.
1.2This test method consists of a standard test procedure, an alternative Procedure 1, and an alternative Procedure 2. As there are variations possible with this test method, it will be up to the particular specification to establish the conditions required. In addition to temperature, the variables to specify if other than those of the standard procedure or alternative Procedure 1 or 2 are: test time, air flow and humidity, sample frequency, test fluid quantity, and metal specimen(s).
1.3The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard.
1.3.1Exception—The values in parentheses in some of the figures are provided for information only for those using old equipment based on non-SI units.
1.4This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.
1.5This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
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MIL-PRF-83282 Revision D:1997 | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 |
MIL H 87257 : 0 | HYDRAULIC FLUID, FIRE RESISTANT, LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT & MISSILE |
MIL C 87252 : B | COOLANT FLUID, HYDROLYTICALLY STABLE, DIELECTRIC |
BS ISO 9940:2015 | Aerospace series. Fluid, hydraulic, phosphate ester-base, fire resistant. Technical specification |
MIL-PRF-8188 Revision D:1997 | CORROSION-PREVENTIVE, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE |
BS ISO 8068:2006 | Lubricants, industrial oils and related products (class L). Family T (turbines). Specification for lubricating oils for turbines |
MIL-PRF-6083 Revision G:2013 | HYDRAULIC FLUID, PETROLEUM BASE, FOR PRESERVATION AND OPERATION |
MIL-DTL-53131 Revision A:1998 | LUBRICATING OIL, PRECISION ROLLING ELEMENT BEARING, POLYALPHAOLEFIN BASED |
MIL H 5606 : G | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE |
MIL-PRF-27601 Revision C:1998 | HYDRAULIC FLUID, FIRE RESISTANT, HYDROGENATED POLYALPHAOLEFIN BASE, HIGH TEMPERATURE, FLIGHT VEHICLE, METRIC |
MIL-PRF-6081 Revision E:2014 | Lubricating Oil, Jet Engine |
MIL-PRF-32538 Base Document:2015 | LUBRICATING OIL, HELICOPTER TRANSMISSION SYSTEM, SYNTHETIC BASE, NATO CODE NUMBER: O-165 |
MIL-DTL-32353 Revision A:2012 | HYDRAULIC & LUBRICATING OIL, SYNTHETIC HYDROCARBON BASE |
MIL-PRF-6085 Revision E:2011 | LUBRICATING OIL, INSTRUMENT, AIRCRAFT, LOW VOLATILITY |
SAE AIR81D | Importance of Physical and Chemical Properties of Aircraft Hydraulic Fluids |
12/30234431 DC : 0 | BS ISO 9940 - AEROSPACE - FIRE RESISTANT HYDRAULIC FLUIDS |
MIL-DTL-83767 Revision C:2007 | Lubricating Oil, Vacuum Pump, Mechanical |
MIL-PRF-7808 Revision L:1997 | LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE |
14/30302298 DC : 0 | BS ISO 9940 - AEROSPACE SERIES - FLUID, HYDRAULIC, PHOSPHATE ESTER-BASE, FIRE RESISTANT - TECHNICAL SPECIFICATION |
MIL-PRF-87100 Revision A:1997 | LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, POLYPHENYL ETHER BASE |
MIL-PRF-87257 Revision C:2017 | HYDRAULIC FLUID, FIRE RESISTANT, LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT AND MISSILE |
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MIL-PRF-87252 Revision D:2015 | COOLANT FLUID, HYDROLYTICALLY STABLE, DIELECTRIC |
SAE AS5780D | Specification for Aero and Aero-Derived Gas Turbine Engine Lubricants |
05/30098184 DC : DRAFT MAY 2005 | ISO 8068 - LUBRICANTS, INDUSTRIAL OILS AND RELATED PRODUCTS (CLASS L) - FAMILY T (TURBINES) - SPECIFICATIONS FOR LUBRICATING OILS FOR TURBINES |
MIL-PRF-7870 Revision E:2015 | LUBRICATING OIL: GENERAL PURPOSE, LOW-TEMPERATURE (NATO O-142) |
MIL-PRF-46170 Revision E:2013 | HYDRAULIC FLUID, RUST INHIBITED, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, NATO CODE NO. H-544 |
MIL-PRF-5606 Revision H:2002 | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE |
ISO 8068:2006 | Lubricants, industrial oils and related products (class L) — Family T (Turbines) — Specification for lubricating oils for turbines |
MIL H 27601 : B | HYDRAULIC FLUID, FIRE RESISTANT, HYDROGENATED POLYALPHAOLEFIN BASE, HIGH TEMPERATURE, FLIGHT VEHICLE, METRIC |
13/30290460 DC : 0 | BS ISO 9940 - AEROSPACE SERIES - FLUID, HYDRAULIC, PHOSPHATE ESTER-BASE, FIRE RESISTANT - TECHNICAL SPECIFICATION |
MIL-PRF-23699 Revision G:2014 | Lubricating Oil, Aircraft Turbine Engine, Synthetic Base, NATO Code Numbers: O-152, O-154, O-156, and O-167 |
MIL-PRF-32033 Revision A:2016 | LUBRICATING OIL, GENERAL PURPOSE, PRESERVATIVE (WATER-DISPLACING, LOW TEMPERATURE) |
NF ISO 8068 : 2006 | LUBRICANTS, INDUSTRIAL OILS AND RELATED PRODUCTS (CLASS L) - FAMILY T (TURBINES) - SPECIFICATIONS FOR LUBRICATING OILS FOR TURBINES |
SAE ARP 6179 : 2011 | EVALUATION OF GAS TURBINE ENGINE LUBRICANT COMPATIBILITY WITH ELASTOMER O-RINGS |
ISO 9940:2015 | Aerospace series Fluid, hydraulic, phosphate ester-base, fire resistant Technical specification |
QQ-C-576 Revision B:1961 | COPPER FLAT PRODUCTS WITH SLIT, SLIT AND EDGE-ROLLED, SHEARED, SAWED OR MACHINED EDGES, (PLATE, BAR, SHEET, AND STRIP) |
MIL-S-13282 Revision B:1973 | SILVER AND SILVER ALLOYS |
SAE AMS4616F | Silicon Bronze Bars, Rods, Forgings, and Tubing 92Cu - 3.2Si - 2.8Zn - 1.5Fe Stress Relieved |
SAE AMS6490H | Steel Bars, Forgings, and Tubing 4.0Cr - 4.2Mo - 1.0V (0.77 - 0.85C) (M-50) Premium Aircraft-Quality for Bearing Applications Consumable Electrode Vacuum Melted |
ASTM D 91 : 2002 : R2007 | Standard Test Method for Precipitation Number of Lubricating Oils |
SAE AMS4908G | Titanium Alloy Sheet and Strip 8mn Annealed, 110 Ksi (760 Mpa) Yield Strength |
QQ-M-44 Revision B:1964 | MAGNESIUM ALLOY PLATE AND SHEET (AZ31B) |
FED-STD-791 Revision D:2007 | TESTING METHOD OF LUBRICANTS, LIQUID FUELS, AND RELATED PRODUCTS |
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