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ASTM D 4636 : 2017 : REDLINE

Current

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

Available format(s)

PDF

Language(s)

English

Published date

01-06-2017

€74.48
Excluding VAT

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
DocumentType
Redline
Pages
14
PublisherName
American Society for Testing and Materials
Status
Current

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.

MIL L 6085 : C LUBRICATING OIL, INSTRUMENT, AIRCRAFT, LOW VOLATILITY
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
MIL L 53131 : 0 LUBRICATING OIL, PRECISION ROLLING ELEMENT BEARING, POLYALPHAOLEFIN BASED
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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