SAE J1966_201108
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
LUBRICATING OILS, AIRCRAFT PISTON ENGINE (NON-DISPERSANT MINERAL OIL)
30-10-2020
22-08-2011
1 Scope
2 References
3 Requirements
4 Quality Assurance Provisions
5 Packaging (For Military Procurements)
6 Notes
APPENDIX A BASE STOCK CRUDE OIL SOURCE AND PROCESSING
DESCRIPTIONS
Specifies the requirements for lubricating oils containing ashless dispersant additives to be used in four-stroke cycle, reciprocating piston aircraft engines.
Committee |
E-38
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DocumentType |
Standard
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PublisherName |
SAE International
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Status |
Superseded
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SupersededBy | |
Supersedes |
MIL-DTL-25038 Revision J:2012 | WIRE, ELECTRICAL, HIGH TEMPERATURE, FIRE RESISTANT, AND FLIGHT CRITICAL |
SAE J549_201503 | PREIGNITION RATING OF SPARK PLUGS |
DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/17(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-DTL-8790 Revision F:2007 | Hose Assemblies, Rubber, Hydraulic, High Pressure 3,000 PSI, Operating Temperature Range -65 Degrees F to +275 Degrees F, Field Attachable |
DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-PRF-32002 Revision D:2008 | Cover Material, Vehicle, Coated Tactical and Combat, Heavy-Duty Waterproof |
MIL-DTL-3702 Revision F:2012 | CABLE, POWER, ELECTRICAL: IGNITION, HIGH-TENSION |
SAE ARP 1400 : 1999 | RECOMMENDED PRACTICES FOR LUBRICATING OIL FILTERS, GENERAL AVIATION RECIPROCATING ENGINE (PISTON TYPE) AIRCRAFT |
SAE AS 6399 : 1999 | HOSE, RUBBER, WIRE-WOUND, SYNTHETIC, ICE ELIMINATING SYSTEM |
MIL-PRF-7907 Revision C:2007 | Cleaning Compound, Decontaminating (for Soiled and Radioactive Contaminated Surfaces) |
MIL-DTL-8794 Revision F:2007 | HOSE, SYNTHETIC RUBBER - HYDRAULIC FLUID, FUEL, AND OIL RESISTANT |
MIL-PRF-6864 Revision F:2010 | CLEANING COMPOUND, SOLVENT, OIL COOLER |
MIL-PRF-46147 Revision D:2008 | LUBRICANT, SOLID FILM, AIR CURED, CORROSION INHIBITING |
MIL-DTL-8795 Revision G:2014 | Hose Assemblies, Elastomeric, Hydraulic, Fuel, Coolant, and Oil Resistant, General Specification for |
MIL-STD-3004 Revision D:2014 | QUALITY ASSURANCE/SURVEILLANCE FOR FUELS, LUBRICANTS AND RELATED PRODUCTS |
SAE J304_201606 | ENGINE OIL TESTS |
SAE AMSS4383B | SEALING COMPOUND, TOPCOAT, FUEL TANK BUNA-N TYPE |
MIL-DTL-85694 Revision A:2013 | Spectrometric Oil Standards |
FED-STD-791 Revision D:2007 | TESTING METHOD OF LUBRICANTS, LIQUID FUELS, AND RELATED PRODUCTS |
MIL-DTL-5070 Revision F:2006 | ADAPTER, HOSE TO TUBE, PIPE AND FLANGE, REUSABLE - HYDRAULIC, FUEL, AND OIL LINES, GENERAL SPECIFICATION FOR |
MIL-STD-2161 Revision C:2014 | Paint Schemes and Exterior Markings for U.S. Navy and Marine Corps Aircraft |
MIL-DTL-8789 Revision G:2015 | FITTING END, ATTACHABLE, HYDRAULIC, HIGH PRESSURE (3,000 PSI), GENERAL SPECIFICATION FOR |
MIL-DTL-5846 Revision D:2008 | Chromel and Alumel Thermocouple Electrical Wire |
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