Standard Test Method for Viscosity and Viscosity Change After Standing at Low Temperature of Aircraft Turbine Lubricants

SIGNIFICANCE AND USE
5.1 Aircraft turbine lubricants, upon standing at low temperatures for prolonged periods of time, may show an increase in kinematic viscosity. This increase may cause lubrication problems in aircraft engines. Thus, this test method is used to ensure that the kinematic viscosity does not exceed the maximum kinematic viscosity in certain specifications for aircraft turbine lubricants.
SCOPE
1.1 This test method covers the determination of the kinematic viscosity of aircraft turbine lubricants at low temperature, and the percent change of viscosity after a 3 h and a 72 h standing period at low temperature.  
1.1.1 The range of kinematic viscosities covered by this test method is from 7700 mm2/s to 14 000 mm2/s at –40 °C and from 7000 mm2/s to 17 500 mm2/s at –51 °C. The precision has only been determined for those materials, kinematic viscosity ranges, and temperatures as shown in the precision section. Kinematic viscosities and percent change of viscosity may be measured and reported at other temperatures and other thermal soak period intervals as agreed by the contracting parties.  
1.2 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard.  
1.2.1 The SI unit used in this test method for Kinematic Viscosity is mm2/s. For user reference, 1 mm2/s = 10-6 m2/s = 1 cSt.  
1.3 Warning—Mercury has been designated by many regulatory agencies as a hazardous substance that can cause serious medical issues. Mercury, or its vapor, has been demonstrated to be hazardous to health and corrosive to materials. Use caution when handling mercury and mercury-containing products. See the applicable product Safety Data Sheet (SDS) for additional information. The potential exists that selling mercury or mercury-containing products, or both, is prohibited by local or national law. Users must determine legality of sales in their location.  
1.4 This 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, health, and environmental practices and determine the applicability of regulatory limitations prior to use. For specific hazard statements, see Section 7.  
1.5 This 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.

General Information

Status
Published
Publication Date
30-Nov-2022
Drafting Committee
D02.07 - Flow Properties

Relations

Effective Date
01-Apr-2024
Effective Date
01-Mar-2024
Effective Date
15-Dec-2023
Effective Date
01-Dec-2023
Effective Date
01-Nov-2023
Effective Date
01-Nov-2023
Effective Date
01-Jul-2023
Effective Date
01-Dec-2019
Effective Date
01-Nov-2019
Effective Date
01-May-2019
Effective Date
15-Dec-2016
Effective Date
01-May-2016
Effective Date
01-Apr-2016
Effective Date
01-Jun-2015
Effective Date
01-Jul-2014

Overview

ASTM D2532-22 is the internationally recognized standard test method for determining the viscosity and viscosity change of aircraft turbine lubricants after standing at low temperatures. Developed and maintained by ASTM International, this method is critical for the aviation industry to ensure the reliability and performance of turbine lubricants, especially under prolonged, cold storage or operational conditions. The standard outlines procedures for assessing both initial kinematic viscosity and how viscosity may increase after the lubricant is kept at low temperatures for durations of 3 hours and 72 hours, covering test temperatures at –40 °C and –51 °C.

Key Topics

  • Kinematic Viscosity Measurement: This standard focuses on the accurate measurement of kinematic viscosity, expressed in mm²/s (or centistokes, cSt), at specified low temperatures. Proper viscosity is essential for the safe and effective lubrication of aircraft turbine engines.
  • Viscosity Change After Standing: ASTM D2532-22 specifies procedures to determine the percentage change in viscosity of turbine oils after being held at low temperatures for both short (3-hour) and long (72-hour) periods. Such changes can signal potential performance issues in lubrication.
  • Temperature Range: The method is applicable to viscosities ranging from 7700 mm²/s to 14,000 mm²/s at –40 °C, and 7000 mm²/s to 17,500 mm²/s at –51 °C, suitable for most synthetic turbine lubricants used in aviation.
  • Safety and Environmental Considerations: The standard addresses potential hazards, especially concerning the use of mercury-containing devices. Users are reminded to consult Safety Data Sheets (SDS) and comply with local regulations regarding hazardous materials.
  • Precision: Pass/fail limits for reproducibility are based on interlaboratory studies, ensuring consistency and repeatability between different laboratories and operators.

Applications

  • Aircraft Turbine Lubricant Quality Assurance: The primary application of ASTM D2532-22 is to ensure aircraft turbine lubricants maintain acceptable viscosity levels during storage and service at low temperatures. This minimizes the risk of lubrication failures that could compromise engine safety or performance.
  • Specification Compliance: The method is commonly referenced in procurement and compliance testing for turbine oils conforming to military and industry specifications (such as MIL-PRF-23699 and MIL-PRF-7808).
  • Product Development and Certification: Lubricant manufacturers use the test to develop, qualify, and certify products for use in aerospace applications.
  • Routine Condition Monitoring: Airline and maintenance operations may utilize this standard for ongoing quality checks of lubricant batches, especially for equipment that may be exposed to extreme cold.

Related Standards

  • ASTM D445 - Test Method for Kinematic Viscosity of Transparent and Opaque Liquids: The principal reference for viscosity measurement procedures incorporated in D2532-22.
  • ASTM D446 - Specifications and Operating Instructions for Glass Capillary Kinematic Viscometers: Outlines requirements for viscometers used in these determinations.
  • ASTM D4175 - Terminology Relating to Petroleum Products, Liquid Fuels, and Lubricants: Provides definitions for terminology utilized in D2532-22.
  • MIL-PRF-23699 and MIL-PRF-7808 - Military specifications for synthetic base turbine engine oils, which reference this standard for viscosity requirements.
  • ASTM E1, E563, E644, E1137, E1750, E2593, E2877 - Standards on temperature measurement tools crucial for test accuracy.

Keywords: ASTM D2532-22, aircraft turbine lubricants, viscosity, low temperature, kinematic viscosity, lubricant testing, aviation lubricant standards, MIL-PRF-23699, aircraft engine oil, oil viscosity test.

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Frequently Asked Questions

ASTM D2532-22 is a standard published by ASTM International. Its full title is "Standard Test Method for Viscosity and Viscosity Change After Standing at Low Temperature of Aircraft Turbine Lubricants". This standard covers: SIGNIFICANCE AND USE 5.1 Aircraft turbine lubricants, upon standing at low temperatures for prolonged periods of time, may show an increase in kinematic viscosity. This increase may cause lubrication problems in aircraft engines. Thus, this test method is used to ensure that the kinematic viscosity does not exceed the maximum kinematic viscosity in certain specifications for aircraft turbine lubricants. SCOPE 1.1 This test method covers the determination of the kinematic viscosity of aircraft turbine lubricants at low temperature, and the percent change of viscosity after a 3 h and a 72 h standing period at low temperature. 1.1.1 The range of kinematic viscosities covered by this test method is from 7700 mm2/s to 14 000 mm2/s at –40 °C and from 7000 mm2/s to 17 500 mm2/s at –51 °C. The precision has only been determined for those materials, kinematic viscosity ranges, and temperatures as shown in the precision section. Kinematic viscosities and percent change of viscosity may be measured and reported at other temperatures and other thermal soak period intervals as agreed by the contracting parties. 1.2 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard. 1.2.1 The SI unit used in this test method for Kinematic Viscosity is mm2/s. For user reference, 1 mm2/s = 10-6 m2/s = 1 cSt. 1.3 Warning—Mercury has been designated by many regulatory agencies as a hazardous substance that can cause serious medical issues. Mercury, or its vapor, has been demonstrated to be hazardous to health and corrosive to materials. Use caution when handling mercury and mercury-containing products. See the applicable product Safety Data Sheet (SDS) for additional information. The potential exists that selling mercury or mercury-containing products, or both, is prohibited by local or national law. Users must determine legality of sales in their location. 1.4 This 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, health, and environmental practices and determine the applicability of regulatory limitations prior to use. For specific hazard statements, see Section 7. 1.5 This 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.

SIGNIFICANCE AND USE 5.1 Aircraft turbine lubricants, upon standing at low temperatures for prolonged periods of time, may show an increase in kinematic viscosity. This increase may cause lubrication problems in aircraft engines. Thus, this test method is used to ensure that the kinematic viscosity does not exceed the maximum kinematic viscosity in certain specifications for aircraft turbine lubricants. SCOPE 1.1 This test method covers the determination of the kinematic viscosity of aircraft turbine lubricants at low temperature, and the percent change of viscosity after a 3 h and a 72 h standing period at low temperature. 1.1.1 The range of kinematic viscosities covered by this test method is from 7700 mm2/s to 14 000 mm2/s at –40 °C and from 7000 mm2/s to 17 500 mm2/s at –51 °C. The precision has only been determined for those materials, kinematic viscosity ranges, and temperatures as shown in the precision section. Kinematic viscosities and percent change of viscosity may be measured and reported at other temperatures and other thermal soak period intervals as agreed by the contracting parties. 1.2 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard. 1.2.1 The SI unit used in this test method for Kinematic Viscosity is mm2/s. For user reference, 1 mm2/s = 10-6 m2/s = 1 cSt. 1.3 Warning—Mercury has been designated by many regulatory agencies as a hazardous substance that can cause serious medical issues. Mercury, or its vapor, has been demonstrated to be hazardous to health and corrosive to materials. Use caution when handling mercury and mercury-containing products. See the applicable product Safety Data Sheet (SDS) for additional information. The potential exists that selling mercury or mercury-containing products, or both, is prohibited by local or national law. Users must determine legality of sales in their location. 1.4 This 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, health, and environmental practices and determine the applicability of regulatory limitations prior to use. For specific hazard statements, see Section 7. 1.5 This 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.

ASTM D2532-22 is classified under the following ICS (International Classification for Standards) categories: 49.025.99 - Other materials. The ICS classification helps identify the subject area and facilitates finding related standards.

ASTM D2532-22 has the following relationships with other standards: It is inter standard links to ASTM D445-24, ASTM D6300-24, ASTM D4175-23a, ASTM D6300-23a, ASTM E1750-23, ASTM D445-23, ASTM D4175-23e1, ASTM D6300-19a, ASTM E644-11(2019), ASTM E2877-12(2019), ASTM D445-16, ASTM E1750-10(2016), ASTM D6300-16, ASTM D6300-15, ASTM D445-14. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.

ASTM D2532-22 is available in PDF format for immediate download after purchase. The document can be added to your cart and obtained through the secure checkout process. Digital delivery ensures instant access to the complete standard document.

Standards Content (Sample)


This 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.
Designation: D2532 − 22
Standard Test Method for
Viscosity and Viscosity Change After Standing at Low
Temperature of Aircraft Turbine Lubricants
This standard is issued under the fixed designation D2532; the number immediately following the designation indicates the year of
original adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval. A
superscript epsilon (´) indicates an editorial change since the last revision or reapproval.
This standard has been approved for use by agencies of the U.S. Department of Defense.
1. Scope* 1.4 This standard does not purport to address all of the
safety concerns, if any, associated with its use. It is the
1.1 This test method covers the determination of the kine-
responsibility of the user of this standard to establish appro-
matic viscosity of aircraft turbine lubricants at low
priate safety, health, and environmental practices and deter-
temperature, and the percent change of viscosity after a 3 h and
mine the applicability of regulatory limitations prior to use.
a 72 h standing period at low temperature.
For specific hazard statements, see Section 7.
1.1.1 The range of kinematic viscosities covered by this test
1.5 This international standard was developed in accor-
2 2
method is from 7700 mm /s to 14 000 mm /s at –40 °C and
dance with internationally recognized principles on standard-
2 2
from 7000 mm /s to 17 500 mm /s at –51 °C. The precision
ization established in the Decision on Principles for the
has only been determined for those materials, kinematic
Development of International Standards, Guides and Recom-
viscosity ranges, and temperatures as shown in the precision
mendations issued by the World Trade Organization Technical
section. Kinematic viscosities and percent change of viscosity
Barriers to Trade (TBT) Committee.
may be measured and reported at other temperatures and other
thermal soak period intervals as agreed by the contracting
2. Referenced Documents
parties.
2.1 ASTM Standards:
1.2 The values stated in SI units are to be regarded as
D445 Test Method for Kinematic Viscosity of Transparent
standard. No other units of measurement are included in this
and Opaque Liquids (and Calculation of Dynamic Viscos-
standard.
ity)
1.2.1 The SI unit used in this test method for Kinematic
D446 Specifications and Operating Instructions for Glass
2 2 -6 2
Viscosity is mm /s. For user reference, 1 mm/s=10 m /s =
Capillary Kinematic Viscometers
1 cSt.
D4175 Terminology Relating to Petroleum Products, Liquid
Fuels, and Lubricants
1.3 Warning—Mercury has been designated by many regu-
D6300 Practice for Determination of Precision and Bias
latory agencies as a hazardous substance that can cause serious
Data for Use in Test Methods for Petroleum Products,
medicalissues.Mercury,oritsvapor,hasbeendemonstratedto
Liquid Fuels, and Lubricants
be hazardous to health and corrosive to materials. Use caution
E1 Specification for ASTM Liquid-in-Glass Thermometers
when handling mercury and mercury-containing products. See
E563 Practice for Preparation and Use of an Ice-Point Bath
the applicable product Safety Data Sheet (SDS) for additional
as a Reference Temperature
information. The potential exists that selling mercury or
E644 Test Methods for Testing Industrial Resistance Ther-
mercury-containing products, or both, is prohibited by local or
mometers
national law. Users must determine legality of sales in their
E1137 SpecificationforIndustrialPlatinumResistanceTher-
location.
mometers
E1750 Guide for Use of Water Triple Point Cells
This test method is under the jurisdiction of ASTM Committee D02 on
Petroleum Products, Liquid Fuels, and Lubricants and is the direct responsibility of
Subcommittee D02.07 on Flow Properties. For referenced ASTM standards, visit the ASTM website, www.astm.org, or
Current edition approved Dec. 1, 2022. Published December 2022. Originally contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
approved in 1966. Last previous edition approved in 2017 as D2532 – 17. DOI: Standards volume information, refer to the standard’s Document Summary page on
10.1520/D2532-22. the ASTM website.
*A Summary of Changes section appears at the end of this standard
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
D2532 − 22
NOTE 1—Consult Specifications D446 regarding calibration constant
E2593 Guide for Accuracy Verification of Industrial Plati-
correction for the actual test temperature when using Specifications D446
num Resistance Thermometers
viscometers that are not suspended level types.
E2877 Guide for Digital Contact Thermometers
6.3 Drying Tubes—Fit the viscometer openings with drying
2.2 Other Documents:
tubes filled with indicating silica gel, using cotton at top and
MIL-PRF-7808 Lubricating Oil, Aircraft Turbine Engine,
bottom to hold the loosely packed desiccant in place. Provide
Synthetic Base
a cross-connection on the viscometer side of the drying tubes
MIL-PRF-23699 Lubricating Oil, Aircraft Turbine Engine,
(whichcanbeclosedbyapinchclamporstopcockwhileliquid
Synthetic Base, NATO Code Number O-156
is being drawn into the efflux bulb) so that the restriction to air
3. Terminology flow will not cause error. Replace the silica gel when a
lavender color is noticeable.
3.1 Definitions:
3.1.1 For definitions of terms used in this test method, refer
6.4 Viscosity Temperature Bath—The constant-temperature
to Terminology D4175.
bath must be capable of holding several viscometers at once. It
3.1.2 digital contact thermometer (DCT), n—an electronic
must have adequate stirring of the liquid medium (Note 2) and
device consisting of a digital display and associated tempera-
balance between heat losses such that the bath temperature can
ture sensing probe.
be maintained at the required temperature 60.03 °C.
3.1.2.1 Discussion—This device consists of a temperature
NOTE 2—Isopropanol or other clear, low-freezing point liquid may be
sensor connected to a measuring instrument; this instrument
used as a bath liquid.
measures the temperature-dependent quantity of the sensor,
6.5 Temperature Measuring Device—Use either a digital
computes the temperature from the measured quantity, and
contact thermometer as described in 6.5.2 with equal or better
provides a digital output. This digital output goes to a digital
accuracy or a calibrated ASTM Kinematic Viscosity Test
displayand/orrecordingdevicethatmaybeinternalorexternal
Thermometer such as 73C (–40 °C) or 74C or 43C (–51 °C)
to the device. These devices are sometimes referred to as
conforming to the requirements as prescribed in Specification
“digital thermometers.”
E1 which have an accuracy after correction of 60.03 °C or
3.1.2.2 Discussion—PET is an acronym for portable elec-
better. The ASTM 74C thermometer has a specification be-
tronic thermometers, a subset of digital contact thermometers
tween –55.4 °C and –52.6 °C but is available from some
(DCT).
suppliers with the scale expanded to cover –51 °C. The 43C
thermometer is only graduated in 0.1 °C increments so inter-
4. Summary of Test Method
pretation at midpoints between the lines may be required.
4.1 Kinematic viscosity and percent change is determined at
6.5.1 When using liquid-in-glass thermometers, use a mag-
low temperature using apparatus defined in Test Method D445
nifying device to read the thermometer to the nearest ⁄5
and Specifications D446 at time intervals of 3 h and 72 h
division (for example, 0.02 °C on thermometers graduated in
following an initial measurement at 35 min.
0.1 °C increments) to ensure that the required test temperature
and temperature control capabilities are met.
5. Significance and Use
6.5.1.1 Check the thermometer’s ice point at least annually
5.1 Aircraft turbine lubricants, upon standing at low tem-
using an ice bath or a constant temperature bath against a
peratures for prolonged periods of time, may show an increase
reference thermometer. If the corrected temperature reading
in kinematic viscosity. This increase may cause lubrication
error is greater than the temperature tolerance, then the
problems in aircraft engines. Thus, this test method is used to
thermometer must be recalibrated.
ensure that the kinematic viscosity does not exceed the
6.5.2 When using a digital contact thermometer (DCT), the
maximum kinematic viscosity in certain specifications for
following requirements shall apply:
aircraft turbine lubricants.
Criteria Minimum Requirements
DCT E2877 Class A
6. Apparatus
Display resolution 0.01 °C, recommended 0.001 °C
Display accuracy ±30 mK (±0.03 °C) for combined probe and
6.1 Viscometers, drying tubes, low-temperature bath,
sensor
thermometer, timer, secondary viscosity standard, filter, and
Sensor type RTD, such as a PRT or thermistor
Drift less than 10 mK (0.01 °C) per year
cleaning supplies are described in detail in Test Method D445.
Response time less than or equal to6sas defined in Speci-
6.2 Viscometer—The viscometer shall meet the require-
fication E1137
Linearity 10 mK over range of intended use
ments ofTest Method D445 and Specifications D446 and be of
Calibration Report The DCT shall have a report of temperature
the type in which the sample can be rerun without cleaning the
calibration traceable to a national calibration
viscometer. Suitable holders should be used. For convenience
or metrology standards body issued by a
competent calibration laboratory with demon-
it is recommended that the viscometer size be chosen to keep
strated competency in temperature calibra-
the efflux time between 200 s and 1000 s.
tion. An ISO 17025 accredited laboratory with
temperature calibration in its accreditation
scope would meet this requirement.
Calibration Data The calibration report shall include at least 3
Available from Standardization Documents Order Desk, DODSSP, Bldg. 4,
calibration temperatures at least 5 °C apart
Section D, 700 Robbins Ave., Philadelphia, PA 19111-5098, http://
which are appropriate for its intended use.
dodssp.daps.dla.mil.
D2532 − 22
6.5.2.1 For a constant temperature bath employed, the DCT essential that strong alkaline cleaning solutions are not used as
probe shall be immersed by more than its minimum immersion changes in the viscometer calibration can occur.
depth in a constant temperature bath so that the center of the
7.2.1 Rinse viscometer inside and out with distilled water
probe’s sensing region is at the same level as the lower half of until all traces of the cleaning solution are completely re-
the working capillary provided the probe’s minimum immer-
moved. Allow to drain for 5 min.
siondepthismetandisnolessthanindicatedonthecalibration
7.2.2 Dry with filtered dry air, a vacuum line, or in an oven
certificate.Theendoftheprobesheathshallnotextendpastthe
at approximately 100 °C for approximately 30 min until all
bottom of the v
...


This document is not an ASTM standard and is intended only to provide the user of an ASTM standard an indication of what changes have been made to the previous version. Because
it may not be technically possible to adequately depict all changes accurately, ASTM recommends that users consult prior editions as appropriate. In all cases only the current version
of the standard as published by ASTM is to be considered the official document.
Designation: D2532 − 17 D2532 − 22
Standard Test Method for
Viscosity and Viscosity Change After Standing at Low
Temperature of Aircraft Turbine Lubricants
This standard is issued under the fixed designation D2532; the number immediately following the designation indicates the year of
original adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval. A
superscript epsilon (´) indicates an editorial change since the last revision or reapproval.
This standard has been approved for use by agencies of the U.S. Department of Defense.
1. Scope*
1.1 This test method covers the determination of the kinematic viscosity of aircraft turbine lubricants at low temperature, and the
percent change of viscosity after a 3 h and a 72 h standing period at low temperature.
2 2
1.1.1 The range of kinematic viscosities covered by this test method is from 7700 mm /s to 14 000 mm /s at –40 °C and from 7000
2 2
mm /s to 17 500 mm /s at –51 °C. The precision has only been determined for those materials, kinematic viscosity ranges, and
temperatures as shown in the precision section. Kinematic viscosities and percent change of viscosity may be measured and
reported at other temperatures and other thermal soak period intervals as agreed by the contracting parties.
1.2 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard.
2 2 -6 2
1.2.1 The SI unit used in this test method for Kinematic Viscosity is mm /s. For user reference, 1 mm /s = 10 m /s = 1 cSt.
1.3 Warning—Mercury has been designated by many regulatory agencies as a hazardous materialsubstance that can cause central
nervous system, kidney and liver damage. serious medical issues. Mercury, or its vapor, may has been demonstrated to be
hazardous to health and corrosive to materials. Caution should be taken Use caution when handling mercury and mercury
containing mercury-containing products. See the applicable product Material Safety Data Sheet (MSDS) for details and EPA’s
website—http://www.epa.gov/mercury/faq.htm—for additional information. Users should be aware (SDS) for additional informa-
tion. The potential exists that selling mercury and/or mercury containing products into your state or country may be prohibited by
law.or mercury-containing products, or both, is prohibited by local or national law. Users must determine legality of sales in their
location.
1.4 This 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 safety, health, and healthenvironmental practices and determine the
applicability of regulatory limitations prior to use. For specific hazard statements, see Section 7.
1.5 This 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.
This test method is under the jurisdiction of ASTM Committee D02 on Petroleum Products, Liquid Fuels, and Lubricants and is the direct responsibility of Subcommittee
D02.07 on Flow Properties.
Current edition approved May 1, 2017Dec. 1, 2022. Published May 2017December 2022. Originally approved in 1966. Last previous edition approved in 20162017 as
D2532 – 16.D2532 – 17. DOI: 10.1520/D2532-17.10.1520/D2532-22.
*A Summary of Changes section appears at the end of this standard
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
D2532 − 22
2. Referenced Documents
2.1 ASTM Standards:
D445 Test Method for Kinematic Viscosity of Transparent and Opaque Liquids (and Calculation of Dynamic Viscosity)
D446 Specifications and Operating Instructions for Glass Capillary Kinematic Viscometers
D4175 Terminology Relating to Petroleum Products, Liquid Fuels, and Lubricants
D6300 Practice for Determination of Precision and Bias Data for Use in Test Methods for Petroleum Products, Liquid Fuels, and
Lubricants
E1 Specification for ASTM Liquid-in-Glass Thermometers
E563 Practice for Preparation and Use of an Ice-Point Bath as a Reference Temperature
E644 Test Methods for Testing Industrial Resistance Thermometers
E1137 Specification for Industrial Platinum Resistance Thermometers
E1750 Guide for Use of Water Triple Point Cells
E2593 Guide for Accuracy Verification of Industrial Platinum Resistance Thermometers
E2877 Guide for Digital Contact Thermometers
2.2 Other Documents:
MIL-PRF-7808 Lubricating Oil, Aircraft Turbine Engine, Synthetic Base
MIL-PRF-23699 Lubricating Oil, Aircraft Turbine Engine, Synthetic Base, NATO Code Number O-156
3. Terminology
3.1 Definitions:
3.1.1 For definitions of terms used in this test method, refer to Terminology D4175.
3.1.2 digital contact thermometer (DCT), n——anan electronic device consisting of a digital display and associated temperature
sensing probe.
3.1.2.1 Discussion—
This device consists of a temperature sensor connected to a measuring instrument; this instrument measures the temperature-
dependent quantity of the sensor, computes the temperature from the measured quantity, and provides a digital output. This digital
output goes to a digital display and/or recording device that may be internal or external to the device. These devices are sometimes
referred to as “digital thermometers.”
3.1.2.2 Discussion—
PET is an acronym for portable electronic thermometers, a subset of digital contact thermometers (DCT).
4. Summary of Test Method
4.1 Kinematic viscosity and percent change is determined at low temperature using apparatus defined in Test Method D445 and
Specifications D446 at time intervals of 3 h and 72 h following an initial measurement at 35 min.
5. Significance and Use
5.1 Aircraft turbine lubricants, upon standing at low temperatures for prolonged periods of time, may show an increase in
kinematic viscosity. This increase may cause lubrication problems in aircraft engines. Thus, this test method is used to ensure that
the kinematic viscosity does not exceed the maximum kinematic viscosity in certain specifications for aircraft turbine lubricants.
6. Apparatus
6.1 Viscometers, drying tubes, low-temperature bath, thermometer, timer, secondary viscosity standard, filter, and cleaning
supplies are described in detail in Test Method D445.
6.2 Viscometer—The viscometer shall meet the requirements of Test Method D445 and Specifications D446 and be of the type in
which the sample can be rerun without cleaning the viscometer. Suitable holders should be used. For convenience it is
recommended that the viscometer size be chosen to keep the efflux time between 200 s and 1000 s.
For referenced ASTM standards, visit the ASTM website, www.astm.org, or contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM Standards
volume information, refer to the standard’s Document Summary page on the ASTM website.
Available from Standardization Documents Order Desk, DODSSP, Bldg. 4, Section D, 700 Robbins Ave., Philadelphia, PA 19111-5098, http://dodssp.daps.dla.mil.
D2532 − 22
NOTE 1—Consult Specifications D446 regarding calibration constant correction for the actual test temperature when using Specifications D446
viscometers that are not suspended level types.
6.3 Drying Tubes—Fit the viscometer openings with drying tubes filled with indicating silica gel, using cotton at top and bottom
to hold the loosely packed desiccant in place. Provide a cross-connection on the viscometer side of the drying tubes (which can
be closed by a pinch clamp or stopcock while liquid is being drawn into the efflux bulb) so that the restriction to air flow will not
cause error. Replace the silica gel when a lavender color is noticeable.
6.4 Viscosity Temperature Bath—The constant-temperature bath must be capable of holding several viscometers at once. It must
have adequate stirring of the liquid medium (Note 2) and balance between heat losses such that the bath temperature can be
maintained at the required temperature 60.03 °C.
NOTE 2—Isopropanol or other clear, low-freezing point liquid may be used as a bath liquid.
6.5 Temperature Measuring Device—Use either a digital contact thermometer as described in 6.5.2 with equal or better accuracy
or a calibrated ASTM Kinematic Viscosity Test Thermometer such as 73C (–40 °C) or 74C or 43C (–51 °C) conforming to the
requirements as prescribed in Specification E1 which have an accuracy after correction of 60.03 °C or better. The ASTM 74C
thermometer has a specification between –55.4 °C and –52.6 °C but is available from some suppliers with the scale expanded to
cover –51 °C. The 43C thermometer is only graduated in 0.1 °C increments so interpretation at midpoints between the lines may
be required.
6.5.1 When using liquid-in-glass thermometers, use a magnifying device to read the thermometer to the nearest ⁄5 division (for
example, 0.02 °C on thermometers graduated in 0.1 °C increments) to ensure that the required test temperature and temperature
control capabilities are met.
6.5.1.1 Check the thermometer’s ice point at least annually using an ice bath or a constant temperature bath against a reference
thermometer. If the corrected temperature reading error is greater than the temperature tolerance, then the thermometer must be
recalibrated.
6.5.2 When using a digital contact thermometer (DCT), the following requirements shall apply:
Criteria Minimum Requirements
DCT E2877 Class A
Display resolution 0.01 °C, recommended 0.001 °C
Display accuracy ±30 mK (±0.03 °C) for combined probe and
sensor
Sensor type RTD, such as a PRT or thermistor
Drift less than 10 mK (0.01 °C) per year
Response time less than or equal to 6 s as defined in Speci-
fication E1137
Linearity 10 mK over range of intended use
Calibration Report The DCT shall have a report of temperature
calibration traceable to a national calibration
or metrology standards body issued by a
competent calibration laboratory with demon-
strated competency in temperature calibra-
tion. An ISO 17025 accredited laboratory with
temperature calibration in its accreditation
scope would meet this requirement.
Calibration Data The calibration report shall include at least 3
calibration temperatures at least 5 °C apart
which are appropriate for its intended use.
6.5.2.1 For a constant temperature bath employed, the DCT probe shall be immersed by more than its minimum immersion depth
in a constant temperature bath so that the center of the probe’s sensing region is at the same level as the lower half of the working
capillary provided the probe’s minimum immersion depth is met and is no less than indicated on the calibration certificate. The
end of the probe sheath shall not extend past the bottom of the viscometer. It is preferable for the center of the sensing element
to be located at the same level as the lower half of the working capillary as long as the minimum immersion requirements are met.
NOTE 3—With respect to DCT probe immersion depth, a procedure is available in Test Methods E644, Section 7 (Minimum Immersion Length Test), for
determining
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