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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING
Available format(s)
PDF
Superseded date
05-26-1997
Language(s)
English
Publisher
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Superseded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 DEGREES F & 450 DEGREES 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 J 2271M : 2015 | 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 DEGREE F AND 1,200 DEGREE F |
| 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 J 2270 : 2016 | 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 DEGREES F & 450 DEGREES 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 AMS 2488 : 2011 | 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 ARP 5824 : 2013 | RECOMMENDED SOLID FILM LUBRICANTS FOR FLUID SYSTEM COMPONENTS |
| SAE AS 4444 : 2013 | FITTINGS, 24 DEGREE 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 MA 1975 : 2015 | HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID REINFORCED, 135 DEGREE C, STANDARD DUTY, 28000/21000 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 AS 85421 : 2015 | 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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