MIL-PRF-23699 Revision G:2014
Current
Current
The latest, up-to-date edition.
Lubricating Oil, Aircraft Turbine Engine, Synthetic Base, NATO Code Numbers: O-152, O-154, O-156, and O-167
Available format(s)
PDF
Language(s)
English
Published date
13-03-2014
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. VERIFICATION
5. PACKAGING
6. NOTES
APPENDIX A - Method For Determining Corrosion
Preventative Properties of Synthetic Gas
Turbine Lubricants
Specifies four classes of gas turbine engine lubricating oils, primarily used for aircraft engines, which have a nominal viscosity of 5 centistokes at 100 degrees C and which are typically made with neopentyl polyol ester base stocks.
| DevelopmentNote |
Supersedes MIL L 23699 (E). (03/2014)
|
| DocumentType |
Standard
|
| Pages |
31
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| Supersedes |
This specification covers four classes of gas turbine engine lubricating oils, primarily used for aircraft engines, which have a nominal viscosity of 5 centistokes at 100 °C and which are typically made with neopentyl polyol ester base stocks. This oil is identified by NATO Code Numbers O-152, O-154, O-156, and O-167.
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| EN 3155-040:2007 | Aerospace series - Electrical contacts used in elements of connection - Part 040: Contacts, electrical, coaxial, size 12, male, type D, solder, class R - Product standard |
| EN 3155-068:2009 | Aerospace series - Electrical contacts used in elements of connection - Part 068: Contacts, electrical, coaxial, size 08, female, type D, solder, class R - Product standard |
| EN 3155-025:2006 | Aerospace series - Electrical contacts used in elements of connection - Part 025: Contacts, electrical, triaxial, size 8, female, type D, crimp, class S - Product standard |
| EN 3155-067:2009 | Aerospace series - Electrical contacts used in elements of connection - Part 067: Contacts, electrical, coaxial, size 08, male, type D, solder, class R - Product standard |
| EN 3733-001:2009 | Aerospace series - Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature up to 150 °C continuous - Part 001: Technical specification |
| EN 3218-001:2006 | Aerospace series - Connectors, rectangular, with metallic shells and screw-locking - Part 001: Technical specification |
| EN 4814:2017 | Aerospace series - Flange couplings up to 21 000 kPa - Technical specification - Inch series |
| EN 3155-041:2007 | Aerospace series - Electrical contacts used in elements of connection - Part 041: Contacts, electrical, coaxial, size 12, female, type D, solder, class R - Product standard |
| EN 3716-001:2006 | Aerospace series - Connector, single-way, with triaxial interface, for transmission of digital data - Part 001: Technical specification |
| EN 3545-001:2008 | Aerospace series - Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures - 55 °C to 175 °C - Part 001: Technical specification |
| EN 4816:2017 | Aerospace series - Flange couplings - Gasket seal with nickel alloy C seal - Technical specification - Inch series |
| EN 3155-069:2009 | Aerospace series - Electrical contacts used in elements of connection - Part 069: Contacts, electrical, coaxial, size 16, female, type D, solder, class P - Product standard |
| EN 3155-039:2007 | Aerospace series - Electrical contacts used in elements of connection - Part 039: Contacts, electrical, coaxial, size 16, female, type D, solder, class R - Product standard |
| EN 3155-024:2006 | Aerospace series - Electrical contacts used in elements of connection - Part 024: Contacts, electrical, triaxial, size 8, male, type D, crimp, class S - Product standard |
| MIL-PRF-81733 Revision D:1998 | SEALING AND COATING COMPOUND, CORROSION INHIBITIVE |
| SAE AIR 5693 : 2014 | COMPATIBILITY OF PTFE HOSE ASSEMBLIES WITH TYPICAL FLUIDS FOUND IN AEROSPACE APPLICATIONS |
| MIL-PRF-81904 Revision C:2011 | COATING COMPOUND, THERMAL-INSULATION |
| I.S. EN 4816:2017 | AEROSPACE SERIES - FLANGE COUPLINGS - GASKET SEAL WITH NICKEL ALLOY C SEAL - TECHNICAL SPECIFICATION - INCH SERIES |
| SAE AMS 3085 : 2016 | FLUID, REFERENCE FOR TESTING AS5780 HPC CLASS (POLYOL) RESISTANT MATERIAL (ALSO KNOWN AS EASTMAN REFERENCE OIL 300) |
| 14/30298727 DC : 0 | BS EN 3155-024 - AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 024: CONTACTS, ELECTRICAL, TRIAXIAL, SIZE 8, MALE, TYPE D, CRIMP, CLASS S - PRODUCT STANDARD |
| I.S. EN 6059-303:2017 | AEROSPACE SERIES - ELECTRICAL CABLES, INSTALLATION - PROTECTION SLEEVES - TEST METHODS - PART 303: RESISTANCE TO FLUIDS |
| MIL-DTL-28804 Revision D:1998 | CONNECTORS, PLUG AND RECEPTACLE, ELECTRIC, RECTANGULAR, HIGH DENSITY, POLARIZATION CENTER JACKSCREW - GENERAL SPECIFICATION FOR |
| 16/30350073 DC : 0 | BS EN 3155-025 - AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 025 - CONTACTS, ELECTRICAL, TRIAXIAL, SIZE 8, FEMALE, TYPE D, CRIMP, CLASS S - PRODUCT STANDARD |
| SAE AS 506 : 2004 | HIGH TEMPERATURE INSULATED TERMINALS & SPLICES |
| I.S. EN 4689:2012 | AEROSPACE SERIES - PAINTS AND VARNISHES - TWO COMPONENTS COLD CURING POLYURETHANE FINISH - HIGH FLEXIBILITY AND CHEMICAL AGENT RESISTANCE FOR MILITARY APPLICATION |
| SAE AS 81511 : 2016 | CONNECTORS, ELECTRICAL, CIRCULAR, HIGH DENSITY, QUICK DISCONNECT, ENVIRONMENT RESISTING AND ACCESSORIES, GENERAL SPECIFICATION FOR |
| MIL-PRF-85582 Revision E:2012 | PRIMER COATINGS: EPOXY, WATERBORNE |
| BS EN 4688:2012 | Aerospace series. Paints and varnishes. Corrosion inhibiting two components cold curing primer for military application |
| MIL-DTL-25677 Revision G:2016 | ADAPTER, CAP, AND NOZZLE, PRESSURE LUBRICATING OIL SERVICING, AIRCRAFT, GENERAL SPECIFICATION FOR |
| PREN 3155-024 : 200P1 | AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 024: CONTACTS, ELECTRICAL, TRIAXIAL, SIZE 8, MALE, TYPE D, CRIMP, CLASS S - PRODUCT STANDARD |
| MIL DTL 17 : J | CABLES, RADIO FREQUENCY, FLEXIBLE AND SEMIRIGID, GENERAL SPECIFICATION FOR |
| SAE AS 5258 : 2012 | INSULATING COMPONENT, MOLDED, ELECTRICAL, HEAT SHRINKABLE, CONNECTOR AND CABLE ACCESSORY, SEALING STRAIN RELIEF, GENERAL SPECIFICATION FOR |
| SAE AS 81824 : 2016 | SPLICE, ELECTRIC, CRIMP, COPPER, ENVIRONMENT RESISTANT |
| SAE AS 83519 : 2015 | SHIELD TERMINATION, SOLDER STYLE, INSULATED, HEAT-SHRINKABLE, ENVIRONMENT RESISTANT GENERAL SPECIFICATION FOR |
| PREN 3155-069 : 200P1 | AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 069: CONTACTS, ELECTRICAL, COAXIAL, SIZE 16, FEMALE, TYPE D, SOLDER, CLASS P - PRODUCT STANDARD |
| SAE AMS 3144 : 2012 | PRIMER, ANODIC ELECTRODEPOSITION FOR AIRCRAFT APPLICATIONS |
| SAE AS 83248/2 : 2016 | O-RING MOLDED FROM AMS7259 MATERIAL |
| SAE AS 6224 : 2015 | WRAP-AROUND INSULATION REPAIR AND PROTECTION SLEEVE, PERMANENT, ELECTRIC, ENVIRONMENT RESISTANT |
| I.S. EN 4814:2017 | AEROSPACE SERIES - FLANGE COUPLINGS UP TO 21000 KPA - TECHNICAL SPECIFICATION - INCH SERIES |
| SAE AMS 3379 : 2013(R2018) | SEALING COMPOUND, POLYSULFIDE RUBBER PREFORMED STRIPS FOR SEALING REMOVABLE DOORS, SKINS, AND PANELS |
| SAE AS 83485 : 2016 | O-RING MOLDED FROM AMS7287 MATERIAL |
| SAE AMS 7287 : 2012 | FLUOROCARBON ELASTOMER (FKM) HIGH TEMPERATURE/HTS OIL RESISTANT/FUEL RESISTANT LOW COMPRESSION SET/70 TO 80 HARDNESS, LOW TEMPERATURE TG -22 DEGREES F (-30 DEGREES C) FOR SEALS IN OIL/FUEL/SPECIFIC HYDRAULIC SYSTEMS |
| SAE AS 81714 : 2014 | TERMINAL JUNCTION SYSTEM (TJS), ENVIRONMENT RESISTANT, GENERAL SPECIFICATION FOR |
| ASTM D 4304 : 2017 : REDLINE | Standard Specification for Mineral and Synthetic Lubricating Oil Used in Steam or Gas Turbines |
| I.S. EN 3155-067:2009 | AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 067: CONTACTS, ELECTRICAL, COAXIAL, SIZE 08, MALE, TYPE D, SOLDER, CLASS R - PRODUCT STANDARD |
| BS EN 3218-001:2006 | Aerospace series. Connectors, rectangular, with metallic shells and screw-locking Technical specification |
| DSCC 89065 : C | GENERAL SPECIFICATION FOR HIGH PERFORMANCE, HIGH DENSITY, TWO PIECE, PRINTED CIRCUIT BOARD CONNECTOR |
| SAE AMS3379A:2013(S2023) | Sealing Compound, Polysulfide Rubber Performed Strips for Sealing Removable Doors, Skins, and Panels(STABILIZED Aug 2023) |
| SAE AS4958B:2013(S2024) | Performance, Nut, Self-Locking, Castellated, Prevailing Torque, UNJ 16 Pitch Thread Form |
| PREN 3155-040 : 200P1 | AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 040: CONTACTS, ELECTRICAL, COAXIAL, SIZE 12, MALE, TYPE D, SOLDER, CLASS R - PRODUCT STANDARD |
| PREN 3155-039 : 200P1 | AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 039: CONTACTS, ELECTRICAL, COAXIAL, SIZE 16, FEMALE, TYPE D, SOLDER, CLASS R - PRODUCT STANDARD |
| PREN 3155-041 : 200P1 | AEROSPACE SERIES - ELECTRICAL CONTACTS USED IN ELEMENTS OF CONNECTION - PART 041: CONTACTS, ELECTRICAL, COAXIAL, SIZE 12, FEMALE, TYPE D, SOLDER, CLASS R - PRODUCT STANDARD |
| SAE ARP 5088 : 2014 | TEST METHOD FOR THE DETERMINATION OF TOTAL ACIDITY IN POLYOL ESTER AND DIESTER GAS TURBINE LUBRICANTS BY AUTOMATIC POTENTIOMETRIC TITRATION |
| MIL-DTL-85694 Revision A:2013 | Spectrometric Oil Standards |
| SAE AMS 3217/4 : 2017 | Test Slabs, Fluoroelastomer (FKM) 65 - 75 |
| ASTM D 892 : 2013-07 | TEST METHOD FOR FOAMING CHARACTERISTICS OF LUBRICATING OILS |
| MIL-PRF-7808 Revision L:1997 | LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE |
| SAE AMS7276H | RUBBER: FLUOROCARBON (FKM) HIGH-TEMPERATURE-FLUID RESISTANT LOW COMPRESSION SET FOR SEALS IN FUEL SYSTEMS AND SPECIFIC ENGINE OIL SYSTEMS |
| SAE AMS 3217/5 : 2013 | TEST SLABS, FLUOROSILICONE (FVMQ), 55-65 |
| ASTM D 5950 : 2014 : REDLINE | Standard Test Method for Pour Point of Petroleum Products (Automatic Tilt Method) |
| SAE ARP 6166 : 2016 | MINISIMULATOR METHOD |
| SAE AMS R 83485 : 2014 | RUBBER, FLUOROCARBON ELASTOMER, IMPROVED PERFORMANCE AT LOW TEMPERATURES |
| ASTM D 6595 : 2017 : REDLINE | Standard Test Method for Determination of Wear Metals and Contaminants in Used Lubricating Oils or Used Hydraulic Fluids by Rotating Disc Electrode Atomic Emission Spectrometry |
| DOD-PRF-85734 Revision A:2004 | LUBRICATING OIL, HELICOPTER TRANSMISSION SYSTEM, SYNTHETIC BASE |
| ASTM D 4636 : 2017 : REDLINE | Standard Test Method for Corrosiveness and Oxidation Stability of Hydraulic Oils, Aircraft Turbine Engine Lubricants, and Other Highly Refined Oils |
| ASTM D 972 : 2016 : REDLINE | Standard Test Method for Evaporation Loss of Lubricating Greases and Oils |
| SAE ARP 6179 : 2011 | EVALUATION OF GAS TURBINE ENGINE LUBRICANT COMPATIBILITY WITH ELASTOMER O-RINGS |
| ASTM D 5949 : 2016 : REDLINE | Standard Test Method for Pour Point of Petroleum Products (Automatic Pressure Pulsing Method) |
| SAE AMS 3085 : 2016 | FLUID, REFERENCE FOR TESTING AS5780 HPC CLASS (POLYOL) RESISTANT MATERIAL (ALSO KNOWN AS EASTMAN REFERENCE OIL 300) |
| SAE AMS 3217/1 : 2013 | TEST SLABS, ACRYLONITRILE BUTADIENE (NBR-H) - MEDIUM-HIGH ACRYLONITRILE, 65-75 |
| FED-STD-791 Revision D:2007 | TESTING METHOD OF LUBRICANTS, LIQUID FUELS, AND RELATED PRODUCTS |
| ASTM D 471 : 2016-02 | TEST METHOD FOR RUBBER PROPERTY - EFFECT OF LIQUIDS |
| SD 6 : 20140201 | PROVISIONS GOVERNING QUALIFICATION: QUALIFIED PRODUCTS LIST AND QUALIFIED MANUFACTURERS LISTS |
| SAE AMS4900P | TITANIUM SHEET, STRIP, AND PLATE, COMMERCIALLY PURE, ANNEALED, 55.0 KSI (379 MPA) YIELD STRENGTH |
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