MIL L 46010 : D
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING
Available format(s)
PDF
Superseded date
26-05-1997
Superseded by
Language(s)
English
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.NO CONTENTS SECTION
Specifies two types of heat cured solid film lubricants to reduce wear and prevent corrosion, galling and seizure of metals.
| Committee |
FSC 9150
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| DocumentType |
Standard
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| Pages |
22
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Superseded
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| SupersededBy | |
| Supersedes |
| MIL-N-85615-10 Base Document:1989 | Nut, Self-Sealing, Self-Locking, CRES, 160 KSI FTU, 250 Deg. F and 450 Deg. F |
| MIL-A-55674 Revision A:1969 | ANTENNA GROUP AN/TRA-37() |
| MIL-B-85667-6 Revision A:1991 | BOLT, SLEEVE, 100 DEGREES REDUCED FLUSH HEAD, STRAIGHT SHANK, CRES 304 SLEEVE, NICKEL ALLOY 718 PIN, 125 KSI FSU, 450 DEGREES F |
| MIL C 28748/6 : D | CONNECTOR, ELECTRICAL, RECTANGULAR, RACK AND PANEL, SOLDER TYPE SOCKET CONTACTS, SIZE 2O |
| MIL-STD-193 Revision L:1991 | PAINTING PROCEDURES AND MARKING FOR VEHICLES, CONSTRUCTION EQUIPMENT, MATERIAL HANDLING EQUIPMENT, AND SPARE PARTS |
| MIL-B-85667 Revision A:1991 | BOLT, SLEEVE, STRAIGHT SHANK, PROTRUDING AND FLUSH HEAD GENERAL SPECIFICATION FOR |
| MIL B 85667/3 : A | BOLT, SLEEVE, PROTRUDING HEAD, STRAIGHT SHANK, CRES 304 SLEEVE, CRES PH 13-8MO PIN, 220 KSI FTU |
| PREN 3244 : 200P2 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREES 30 MINUTES IN TITANIUM ALLOY - UNIONS, DOUBLE ENDED |
| PREN 3248 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREES 30 MINUTES IN TITANIUM ALLOY - ADAPTERS, REDUCED PIPE END WITH LOCKING RING |
| PREN 3266 : 200P2 | AEROSPACE SERIES - PIPE COUPLING IN TITANIUM ALLOY - BULKHEAD NUTS |
| MIL-B-85667-2 Revision A:1991 | BOLT, SLEEVE, 100 DEG. REDUCED FLUSH HEAD, STRAIGHT SHANK, CRES 304 SLEEVE, CRES PH 13-8MO PIN, 125 KSI FSU |
| PREN 4233 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREES 30 MINUTES IN TITANIUM ALLOY - UNIONS, WELDED, THREADED |
| PREN 3246 : 200P2 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREES 30 MINUTES IN TITANIUM ALLOY - UNIONS, BULKHEAD |
| PREN 4022 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30' IN TITANIUM ALLOY - ELBOWS 90 DEGREE, BULKHEAD, WELDED |
| PREN 4193 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30' IN TITANIUM ALLOY - TEES, REDUCED, BULKHEAD LONG |
| PREN 4189 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30' IN TITANIUM ALLOY - TEES, BULKHEAD BRANCH, LONG |
| PREN 4194 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30' IN TITANIUM ALLOY - TEES, REDUCED, BULKHEAD |
| PREN 4192 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30' IN TITANIUM ALLOY - TEES, REDUCED, BULKHEAD BRANCH |
| PREN 4185 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30' IN TITANIUM ALLOY - TEES, BULKHEAD LONG |
| PREN 4027 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30' IN TITANIUM ALLOY - TEES, BRANCH WITH SWIVEL NUT |
| PREN 4026 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30' IN TITANIUM ALLOY - TEES |
| PREN 4021 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30' IN TITANIUM ALLOY - ELBOWS 90 DEGREE, BULKHEAD |
| PREN 4186 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30' IN TITANIUM ALLOY - CROSS UNIONS |
| SAE J2271M_201508 | Ship Systems and Equipment - Part Standard for Studs - Continuous and Double End (Metric) |
| ASTM D 2510 : 1994 : R2012 | Standard Test Method for Adhesion of Solid Film Lubricants |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-N-45938 Revision A:1995 | NUT, PLAIN, CLINCH AND NUT, SEL-LOCKING, CLINCH GENERAL SPECIFICATION FOR |
| MIL-B-23964 Revision D:1981 | BOLT, SELF-RETAINING, POSITIVE LOCKING |
| MIL-F-81177 Revision E:1984 | FASTENERS, BLIND, HIGH STRENGTH, INSTALLATION FORMED ALLOY STEEL, GENERAL SPECIFICATION FOR |
| MIL-DTL-1222 Revision J:2000 | STUDS, BOLTS, SCREWS AND NUTS FOR APPLICATIONS WHERE A HIGH DEGREE OF RELIABILITY IS REQUIRED; GENERAL SPECIFICATION FOR |
| 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)/7(2011) : 2011 | 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)/13(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 |
| MIL-N-85730 Base Document:1988 | NUT, SELF-LOCKING, SPLINE DRIVE, ASSEMBLED WASHER, NICKEL ALLOY 718, 220 KSI FTU, 900 DEGREES F, GENERAL SPECIFICATION FOR |
| MIL-C-6818 Revision D:1973 | CLAMP, INSTRUMENT MOUNTING AIRCRAFT |
| MIL-F-8975 Revision B:1982 | FASTENER, BLIND, HIGH STRENGTH, INSTALLATION FORMED CORROSION RESISTANT STEEL, HEAT RESISTANT STEEL AND TITANIUM, GENERAL SPECIFICATION FOR |
| MS20604 Revision K:1995 | RIVET, BLIND, NONSTRUCTURAL, UNIVERSAL HEAD, CLASS 1 |
| 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)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-F-8961 Revision A:1992 | Fastener Element, Self-Locking, Externally Threaded, 450 Degrees Fahrenheit and 1,200 Degrees Fahrenheit |
| MIL-STD-1250 Revision A:1992 | CORROSION PREVENTION AND DETERIORATION CONTROL IN ELECTRONIC COMPONENTS AND ASSEMBLIES |
| MIL C 28748/5 : D | CONNECTOR, ELECTRICAL, RECTANGULAR, RACK AND PANEL, SOLDER TYPE PIN CONTACTS, SIZE 2O |
| MIL-HDBK-1250 Revision A:1995 | CORROSION PREVENTION AND DETERIORATION CONTROL IN ELECTRONIC COMPONENTS AND ASSEMBLIES |
| ASTM D 2510 : 1994 : R1998 | Standard Test Method for Adhesion of Solid Film Lubricants |
| MIL-STD-2131 Revision A:1991 | LAUNCHER, EJECTION GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
| SAE J2270_201606 | Ship Systems and Equipment - Threaded Fasteners - Inspection, Test, and Installation Guidance |
| PREN 3245 : 200P2 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREES 30 MINUTES IN TITANIUM ALLOY - UNIONS, REDUCER |
| MIL-F-7179 Revision G:1993 | FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM |
| PREN 3566 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30 MINUTES IN TITANIUM ALLOY - ADAPTERS WITH LOCKING RING |
| PREN 4029 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30' IN TITANIUM ALLOY - TEES BULKHEAD BRANCH |
| PREN 4028 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30' IN TITANIUM ALLOY - TEES, SWIVEL NUT ON RUN |
| 96/712318 DC : DRAFT SEP 1996 | PREN 3079 - AEROSPACE SERIES - ADAPTORS WITH LOCKING RING UP TO 2800 KPA - TECHNICAL SPECIFICATION |
| DOD-N-70333 Base Document:1985 | NUT, PLAIN AND SELF-LOCKING, CLINCH, METRIC (SELF-CLINCHING, KNURLED COLLAR) FIXED AND FLOATING, GENERAL SPECIFICATION FOR |
| MIL-B-85667-10 Base Document:1991 | BOLT, SLEEVE, 100 DEGREES TENSION FLUSH HEAD, STRAIGHT SHANK, CRES 304 SLEEVE, CRES A-286 PIN, 160 KSI FTU, 450 DEGREES F |
| MIL-N-85615-8 Base Document:1989 | Nut, Self-Sealing, Self-Locking, Alloy Steel, 125 KSI FTU, 250 Deg. F and 450 Deg. F |
| NASA KSC TM 584 : 1994 | CORROSION CONTROL AND TREATMENT MANUAL |
| MIL-I-45914 Revision A:1991 | INSERT, SCREW THREAD - LOCKED IN, KEY LOCKED |
| PREN 3270 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREES 30 MINUTES IN TITANIUM ALLOY - BLANKING PLUGS WITH LOCKING RING |
| MIL-B-10122 Revision E:1991 | BARGE, LIQUID CARGO: NONPROPELLED, STEEL, OFFSHORE, 4,160-BARREL, 120-FOOT, DESIGN 231C |
| MIL-C-3580 Revision E:1991 | CRANES AND CRANE SHOVELS, TRUCK, CRAWLER, AND WHEEL MOUNTED FULL REVOLVING AND THEIR ATTACHMENTS, PACKAGING OF |
| SAE AMS2488D | Anodic Treatment - Titanium and Titanium Alloys Solution pH 13 or Higher |
| PREN 3247 : 200P2 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREES 30 MINUTES IN TITANIUM ALLOY - UNIONS, BULKHEAD, WELDED |
| PREN 3690 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREES 30 MINUTES IN TITANIUM ALLOY - UNIONS, BULKHEAD, LONG |
| NASA MSFC STD 486 : 1992 | STANDARD, THREADED FASTENERS, TORQUE LIMITS FOR |
| EN 4175:2005 | Aerospace series - Collars, flanged swage locking, sheartype, in titanium TI-P99002, metric series |
| MIL-STD-186 Revision F:2002 | PROTECTIVE FINISHING SYSTEMS FOR ROCKETS, GUIDED MISSILES, SUPPORT EQUIPMENT AND RELATED MATERIALS |
| MIL B 85667/7 : A | BOLT, SLEEVE, PROTRUDING HEAD, STRAIGHT SHANK, CRES 304 SLEEVE, NICKEL ALLOY 718 PIN, 125 KSI FSU, 220 KSI FTU, 450 DEG F. |
| MIL-F-18280 Revision F:1995 | FITTING, FLARELESS TUBE, FLUID CONNECTION |
| SAE ARP5824 | Recommended Solid Film Lubricants for Fluid System Components |
| SAE AS4444 | Fittings, 24° Cone Flareless, Fluid Connection, 5000 psi |
| MIL-G-762 Revision E:1990 | GRADER, ROAD, PACKAGING OF |
| DWA-M 143-20:2018 | TEST METHOD FOR DROP IMPACT RESISTANCE OF BLOW-MOLDED THERMOPLASTIC CONTAINERS |
| MIL-B-85667-9 Base Document:1991 | BOLT, SLEEVE, PROTRUDING HEAD, STRAIGHT SHANK, CRES 304 SLEEVE, CRES A-286 PIN, 95 KSI FSU, 160 KSI FTU, 450 DEGREES F |
| PREN 4188 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30' IN TITANIUM ALLOY - ELBOWS 90 DEGREE, BULKHEAD, LONG, WELDED |
| PREN 4191 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30' IN TITANIUM ALLOY - TEES, REDUCED, BULKHEAD BRANCH, LONG |
| PREN 4187 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30' IN TITANIUM ALLOY - ELBOWS 90 DEGREE, BULKHEAD, LONG |
| SAE MA1975 | Hose Assemblies, Polytetrafluoroethylene, Aramid Reinforced, 135 °C, Standard Duty, 28 000/21 000 kPa, Hydraulic, Aircraft Systems |
| BS EN 4175:2005 | Aerospace series. Collars, flanged swage locking, sheartype, in titanium TI-P99002, metric series |
| MIL-A-14295 Revision C:1985 | ALIGNMENT EQUIPMENT, WHEEL, FOR MILITARY WHEELED VEHICLES |
| PREN 4175 : 200P1 | AEROSPACE SERIES - COLLARS, FLANGED SWAGE LOCKING, SHEARTYPE, IN TITANIUM TI-P99002, METRIC SERIES |
| MIL-C-85049-94 Base Document:1993 | CONNECTOR ACCESSORIES, ELECTRICAL, MOUNTING DEVICE FLANGE TYPE, FULL MOUNTING PERIMETER DEVICE, TYPE I (HEAVY DUTY) |
| MIL B 85667/12 : 0 | BOLT, SLEEVE 100 DEGREE TENSION FLUSH HEAD, STRAIGHT SHANK, CRES 304 SLEEVE, TITANIUM ALLOY PIN, 95 KSI FSU, 160 KSI FTU |
| PREN 6046 : 200P1 | AEROSPACE SERIES - BEARINGS, SPHERICAL PLAIN, IN CORROSION RESISTING STEEL-NARROW SERIES DIMENSIONS AND LOADS - INCH SERIES |
| PREN 4182 : 200P1 | PIPE COUPLING 8 DEGREE 30' IN TITANIUM ALLOY - TEE, REDUCED |
| PREN 4030 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30' IN TITANIUM ALLOY - TEES, BULKHEAD RUN |
| PREN 4190 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30' IN TITANIUM ALLOY - TEES, REDUCED, WITH SWIVEL NUT ON RUN |
| PREN 4019 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30' IN TITANIUM ALLOY - ELBOWS 90 DEGREE, WELDED |
| PREN 4017 : 200P1 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30' IN TITANIUM ALLOY - ELBOWS 90 DEGREE |
| SAE AS85421A | Fittings, Tube, Fluid Systems, Separable, Beam Seal, 3000/4000 psi, General Specification For |
| ASTM D 2510 : 1994 : R2006 | Standard Test Method for Adhesion of Solid Film Lubricants |
| ASTM D 2510 : 1994 : R2017 | Standard Test Method for Adhesion of Solid Film Lubricants |
| DIN EN 4233:2002-08 | AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30 MINUTES IN TITANIUM ALLOY - UNIONS, WELDED, THREADED |
| TT-N-95 Revision B:1967 | |
| MIL H 46170 : B | HYDRAULIC FLUID, RUST INHIBITED, FIRE-RESISTANT, SYNTHETIC HYDROCARBON BASE |
| ASTM D 1400 : 2000 | Standard Test Method for Nondestructive Measurement of Dry Film Thickness of Nonconductive Coatings Applied to a Nonferrous Metal Base (Withdrawn 2006) |
| MIL L 23699 : E | LUBRICATING OIL, AIRCRAFT TURBINE ENGINES, SYNTHETIC BASE |
| ASTM D 1141 : 1998 : EDT 1 | Standard Practice for the Preparation of Substitute Ocean Water |
| MIL L 63460 : D | LUBRICANT, CLEANER AND PRESERVATIVE FOR WEAPONS AND WEAPONS SYSTEMS (METRIC) |
| DOD L 85336 : A | LUBRICANT, ALL WEATHER (AUTOMATIC WEAPONS) |
| MIL-STD-290 Revision H:2013 | PACKAGING AND MARKING OF PETROLEUM AND RELATED PRODUCTS |
| MIL L 46000 : C | LUBRICANT, SEMI-FLUID (AUTOMATIC WEAPONS) |
| ASTM F 22 : 2013 : REDLINE | Standard Test Method for Hydrophobic Surface Films by the Water-Break Test |
| VV-D-1078 Revision B:1983 | DAMPING FLUID, SILICONE BASE (DIMETHYL POLYSILOXANE) |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| ASTM D 1186 : 2001 | Standard Test Methods for Nondestructive Measurement of Dry Film Thickness of Nonmagnetic Coatings Applied to a Ferrous Base (Withdrawn 2006) |
| MIL T 83133 : D | TURBINE FUELS, AVIATION, KEROSENE TYPES, NATO F-34 (JP-8) AND NATO F-35 |
| MIL-A-8243 Revision D:1985 | ANTI-ICING AND DEICING-DEFROSTING FLUIDS |
| QQ-A-250-5 Revision F:1971 | ALUMINUM ALLOY ALCLAD 2024, PLATE AND SHEET |
| MIL L 14107 : C | LUBRICATING OIL, WEAPONS, LOW TEMPERATURE |
| FED-STD-791 Revision D:2007 | TESTING METHOD OF LUBRICANTS, LIQUID FUELS, AND RELATED PRODUCTS |
| DOD P 16232 : F | PHOSPHATE COATING, HEAVY, MANGANESE OR ZINC BASE (FOR FERROUS METALS) |
| MIL C 372 : C | CLEANING COMPOUND, SOLVENT FOR BORE OF SMALL ARMS AND AUTOMATIC AIRCRAFT WEAPONS |
| ASTM D 1475 : 2013 : REDLINE | Standard Test Method For Density of Liquid Coatings, Inks, and Related Products |
| MIL-STD-105 Revision E:1989 | SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES |
| FED-STD-595 Revision C:2008 | COLORS USED IN GOVERNMENT PROCUREMENT |
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