MIL-STD-838 Revision C:1983
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
LUBRICATION OF MILITARY EQUIPMENT
03-12-1997
Provisions for selection and application of lubricants required for flight and surface vehicles and their associated equipment, electronic and shipboard equipment.
DocumentType |
Standard
|
Pages |
16
|
PublisherName |
US Military Specs/Standards/Handbooks
|
Status |
Superseded
|
SupersededBy |
MIL-T-38034 Revision E:1970 | TIMER, FIRE CONTROL, BOMBING, DUAL |
MIL-STD-2156 Base Document:1983 | LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
MIL-A-53100 Base Document:1990 | ARCTIC FUEL SYSTEM SUPPLY POINT (AFSSP) |
MIL-HDBK-113 Revision C:1989 | GUIDE FOR THE SELECTION OF LUBRICANTS, FUNCTIONAL FLUIDS, PRESERVATIVES AND SPECIALITY PRODUCTS FOR USE IN GROUND EQUIPMENT SYSTEMS |
MIL-M-8555 Revision C:1984 | MISSILE, GUIDED, DESIGN AND CONSTRUCTION, GENERAL SPECIFICATION |
MIL I 25688 : A | INDICATOR, ELECTRICAL TACHOMETER ERU-3/A. CRANKSHAFT SPEED 500-4,000 RPM, 3 1/4 INCH SIZE |
MIL-C-52980 Revision B:1988 | COMPRESSOR, RECIPROCATING AND ROTARY, GASOLINE ENGINE DRIVEN, AIR |
MIL H 81014 : A NOTICE 1 | HOOK, HELICOPTER, EXTERNAL CARGO, 20,000 POUND CAPACITY, TYPE C |
MIL-B-385 Revision G:1985 | BREAKERS, PAVING, PNEUMATIC-POWERED (7/8-INCH HEXAGON BY 2-3/4-INCH CHUCK AND 7/8-INCH HEXAGON BY 3-1/4-INCH CHUCK) |
MIL-D-8684 Revision B:1959 | DATA AND TESTS, ENGINEERING, CONTACT REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE SYSTEMS |
MIL-I-27202 Revision A:1980 | INDICATOR, ELECTRICAL TACHOMETER, 0-110 PERCENT RPM 2-INCH SIZE, INTEGRALLY LIGHTED |
MIL-A-23121 Revision C:1970 | AIRCREW ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM, GENERAL SPECIFICATION FOR |
DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-P-52327 Revision C:1990 | PUMPS, CENTRIFUGAL, ELECTRIC-MOTOR-DRIVEN, POSITIVE PRIME, PETROLEUM PRODUCTS, AIRFIELD DEFUELLING AND RECEIVING |
MIL-C-13874 Revision K:1992 | COMPRESSORS, RECIPROCATING AND ROTARY, AIR, ELECTRIC MOTOR DRIVEN |
MIL-HDBK-1587 Base Document:1996 | MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEM |
MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-A-81973 Base Document:1974 | AIRCREW AUTOMATED ESCAPE SYSTEMS, TEST VEHICLES FOR GROUND TRACK PERFORMANCE TESTING, ROCKET AND/OR JET ENGINE PROPELLED; GENERAL SPECIFICATION FOR |
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)/11(2013) : 2013 | 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)/12(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 |
MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-R-85880 Base Document:1988 | ROCKET, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
MIL-C-0052980 Revision C:1994 | COMPRESSORS, RECIPROCATING AND ROTARY, AIR DIESEL-ENGINE-DRIVEN, OR GASOLINE-ENGINE-DRIVEN |
GG-T-35 Revision C:1989 | TABLE; DRAWING, TRACING, AND SCRIBING |
MIL-T-52942 Revision C:1996 | TRUCK, FIRE FIGHTING: PUMPER, 1000 GPM; LADDER/WATER TOWER COMBINATION |
MIL-C-13899 Revision F:1985 | COMPRESSOR UNIT, ROTARY: AIR, WHEELBARROW-FRAME-MOUNTED, TWO PNEUMATIC TIRES, GASOLINE-ENGINE-DRIVEN, 60-CFM, 6.5-PSIG |
MIL C 7958 : A | CONTROL, PUSH PULL, FLEXIBLE AND RIGID |
MIL-M-25393 Revision A:1969 | MANUAL, TECHNICAL, INTERMEDIATE MAINTENANCE INSTRUCTIONS (AIRBORNE EQUIPMENT) |
MIL M 38797 : NOTICE 1 | MANUAL, TECHNICAL, OPERATION INSTRUCTIONS AND MAINTENANCE INSTRUCTIONS (FOR VARIOUS TYPES OF EQUIPMENT) |
MIL T 38170 : F | TANK, MOBILE STORAGE, LIQUID OXYGEN TMU 27/M |
MIL-STD-1250 Revision A:1992 | CORROSION PREVENTION AND DETERIORATION CONTROL IN ELECTRONIC COMPONENTS AND ASSEMBLIES |
MIL H 81529 : 0 | HOOK, HELICOPTER EXTERNAL CARGO, 6,000 POUND CAPACITY TYPE A |
MIL-P-5994 Revision D:1972 | PUMP, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY, GENERAL SPECIFICATION FOR |
MIL-T-25363 Revision D:1973 | TANK, PNEUMATIC PRESSURE, AIRCRAFT, GLASS FIBER |
MIL-A-27195 Revision A:1989 | ACCELEROMETER, AIRCRAFT, MECHANICAL ABU-6/A |
MIL G 26611 : D | GENERATOR, TACHOMETER GEU-7/A, MINIATURE |
MIL S 25057 : B | SCREEN SYSTEM, AIR INLET, AIRCRAFT TURBINE ENGINE, GENERAL SPECIFICATION FOR |
MIL-I-5133 Revision C:1953 | INDICATOR, ATTITUDE TYPE J 8 |
MIL-S-8512 Revision D:1974 | SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
MIL-HDBK-1250 Revision A:1995 | CORROSION PREVENTION AND DETERIORATION CONTROL IN ELECTRONIC COMPONENTS AND ASSEMBLIES |
MIL-S-6150 Revision D:1987 | STARTER, ENGINE, ELECTRICAL, DIRECT CRANKING, AIRCRAFT 28 VOLT DC |
MIL-STD-2131 Revision A:1991 | LAUNCHER, EJECTION GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
MIL L 58085 : A | LIGHT, BEACON, ANTI COLLISION AIRCRAFT |
MIL-S-83129 Revision A:1972 | SPECTROMETER, FLUID ANALYSIS A/E35U-3 |
MIL-C-52037 Revision F:1990 | COMPRESSOR UNIT, RECIPROCATING, POWER DRIVEN, AIR, 15 CFM 3,500 PSI |
MIL-B-45022 Revision F:1992 | BLAST CLEANING CABINETS |
MIL C 4928 : A | CHARGER, BATTERY, SILICON DIODE, TYPE A-1 |
MIL-DTL-85110 Revision B:1997 | BAR, REPEATABLE RELEASE HOLDBACK (RRHB), AIRCRAFT LAUNCHING, GENERAL REQUIREMENT FOR |
MIL I 25689 : A NOTICE 1 | INDICATOR, ELECTRICAL TACHOMETER |
MIL-E-87235 Base Document:1985 | EMERGENCY ESCAPE, AIRCRAFT (REQUEST FOR ISSUE MUST BE SENT VIA ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
MIL-M-38789 Revision A:1970 | MANUAL, TECHNICAL, OVERHAUL INSTRUCTIONS AND OVERHAUL INSTRUCTIONS WITH ILLUSTRATED PARTS BREAKDOWN (FOR VARIOUS EQUIPMENT AND ACCESSORIES) |
MIL-S-18471 Revision G:1983 | |
MIL-T-18232 Revision B:1968 | TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR |
MIL-B-467 Revision E:1988 | BREAKER, PAVING: PNEUMATIC |
MIL-I-25863 Revision D:1990 | INDICATOR, ELECTRICAL TACHOMETER 0-110 PERCENT RPM, 2-INCH SIZE, INTEGRALLY LIGHTED |
MIL-D-7106 Revision C:1987 | DRIFTMETER, ELECTRICALLY DRIVEN GYRO STABILIZED |
MIL S 25073 : 0 | |
MIL G 6162 : B | GENERATOR AND STARTER GENERATOR, ELECTRIC DIRECT CURRENT, NOMINAL 30 VOLTS AIRCRAFT GENERAL SPECIFICATION |
GGG-L-795 Revision E:1990 | LUBRICATING UNIT, POWER OPERATED, AND PUMPING UNITS, PRESSURE LUBRICATING, DRUM MOUNTING |
JSSG-2006 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
MIL-M-5166 Revision D:1983 | MANUAL, TECHNICAL, ASSEMBLY, SERVICING AND ORGANIZATIONAL MAINTENANCE INSTRUCTIONS, [FOR GUIDED MISSILES AND PILOTLESS AIRCRAFT] |
MIL-I-85889 Base Document:1988 | IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
MIL-S-26547 Revision C:1985 | STARTER-GENERATOR ENGINE STU-6A |
MIL G 8360 : A | GAGE, PRESSURE, DIAL INDICATING, MANIFOLD PRESSURE, 10-75 IN MERCURY TYPE MB 1 |
MIL-I-26689 Revision C:1981 | INDICATOR, HORIZONTAL SITUATION, AQU-2/A |
MIL-I-58067 Revision A:1977 | INDICATOR, VERTICAL VELOCITY, RAPID RESPONSE ACCELERATION SENSITIVE, GENERAL SPECIFICATION FOR |
MIL-S-6551 Revision A:1981 | |
MIL-A-25915 Revision A:1980 | ACCELEROMETER, AIRCRAFT, PILOTS WARNING, TYPE MA-2 |
MIL M 9864 : B | MANUALS, TECHNICAL: ORGANIZATIONAL MAINTENANCE (MISSILE AND SPACE SYSTEMS) |
MIL A 25088 : C | |
MIL-P-52405 Revision C:1990 | PUMPS, CENTRIFUGAL, ELECTRIC-MOTOR-DRIVEN (FOR WATER) |
MIL-H-27269 Revision A:1977 | HORIZONTAL SITUATION INDICATOR GROUP AF A24J AND 1 |
DOD-HDBK-791 Base Document:1988 | MAINTAINABILITY DESIGN TECHNIQUES |
MIL-S-81771 Revision A:1975 | Seat System; Aircrew, Crash Resistant; General Specification for |
MIL-C-8412 Revision B:1969 | COMPASS, MAGNETIC, SLAVED GYRO, TYPE J-4 |
MIL-P-83126 Revision A:1980 | PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
MIL-P-85034 Base Document:1976 | POWER PACKAGE, EMERGENCY AC/DC GENERATOR, RAM AIR TURBINE DRIVEN |
MIL-M-25394 Revision A:1969 | MANUAL, TECHNICAL, OVERHAUL INSTRUCTIONS AND INTERMEDIATE MAINTENANCE INSTRUCTIONS (FOR ENGINES) |
ADS-13F-HDBK : 1997 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
MIL-E-38453 Revision A:1971 | ENVIRONMENTAL CONTROL, ENVIRONMENTAL PROTECTION, AND ENGINE BLEED AIR SYSTEMS, AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-I-38391 Base Document:1965 | INDICATOR, ELECTRICAL TACHOMETER, ERU-12/A 0-350 RPM (ROTOR), 0-7000 RPM (ENGINE) |
MIL-P-85573 Base Document:1983 | POWER UNIT AIRCRAFT AUXILIARY, GAS TURBINE, GENERAL SPECIFICATION FOR |
MIL-W-26217 Revision B:1985 | WINCH, DRUM, POWER OPERATED AF E24H 1, CARGO LOADING, 4OOO POUND CAPACITY, VARIABLE SPEED, 28V DC PORTABLE |
MIL-A-27261 Revision A:1966 | ACCELEROMETER, AIRCRAFT |
MIL-HDBK-275 Revision A:1976 | GUIDE FOR SELECTION OF LUBRICANTS, FLUIDS AND COMPOUNDS FOR USE IN FLIGHT VEHICLES AND COMPONENTS |
MIL-G-23083 Revision C:1972 | GYROSCOPE, RATE SWITCHING MS 17399 |
MIL-I-25479 Revision A:1987 | INDICATOR, MACH NUMBER, SENSITIVE, SERVOED, RANGE .5 TO 1.O, TYPE ME-5 |
MIL-A-27330 Revision B:1987 | ACCELEROMETER, ELECTRICAL, LINEAR TRU-3/A |
MIL T 83174 : B (3) | TRANSMITTER, ACCELEROMETER, AXIAL |
MIL-G-26988 Revision C:1971 | GAGE, LIQUID QUANTITY, CAPACITOR TYPE TRANSISTORIZED, GENERAL SPECIFICATION FOR |
MIL-I-27680 Revision C:1973 | INDICATOR, ATTITUDE, ARU-12/A, REMOTE |
MIL-I-27623 Revision C:1972 | INDICATOR, ATTITUDE, REMOTE STANDBY, 2 INCH |
MIL-I-83117 Revision B:1975 | INDICATOR, ANGLE OF ATTACK |
MIL-I-25941 Revision D:1986 | INDICATOR, TURN AND SLIP, 2-INCH SIZE, INTEGRALLY LIGHTED |
MIL-I-25645 Revision D:1970 | INDICATOR, LIQUID OXYGEN QUANTITY, CAPACITANCE TYPE, GENERAL SPECIFICATION FOR |
MIL-I-27848 Revision B:1994 | INDICATOR, HORIZONTAL SITUATION AQU-4/A |
MIL-I-38258 Base Document:1965 | INDICATOR, ATTITUDE ARU 18/A DIRECTOR |
MIL-M-63038 Revision D:1993 | MANUAL. TECHNICAL, ORGANIZATION OR AVIATION UNIT, DIRECT SUPPORT OR AVIATION INTERMEDIATE, AND GENERAL SUPPORT MAINTENANCE |
MIL-I-27619 Revision G:1974 | INDICATORS, ATTITUDE DIRECTOR |
MIL-A-53099 Base Document:1990 | ARCTIC FORWARD AREA REFUELLING EQUIPMENT (AFARE) |
MIL-W-5013 Revision L:1991 | WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL T 25627 : C | TRANSMITTER, SYNCHRO, ANGLE OF ATTACK OR SIDESLIP |
MS15720 Base Document:1954 | FITTINGS, LUBRICATION (HYDRAULIC) THROAT OR SURFACE CHECK, 1/4-28 TAPER THREADS, CORROSION RESISTANT STEEL, TYPE 7 |
MIL-HDBK-275 Revision A:1976 | GUIDE FOR SELECTION OF LUBRICANTS, FLUIDS AND COMPOUNDS FOR USE IN FLIGHT VEHICLES AND COMPONENTS |
MS15001 Revision A:1959 | FITTINGS, LUBRICATION (HYDRAULIC) SURFACE CHECK, 1/4-28 TAPER THREADS, STEEL, TYPE 1 |
MIL-STD-143 Revision B:1969 | STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF |
MIL-HDBK-113 Revision C:1989 | GUIDE FOR THE SELECTION OF LUBRICANTS, FUNCTIONAL FLUIDS, PRESERVATIVES AND SPECIALITY PRODUCTS FOR USE IN GROUND EQUIPMENT SYSTEMS |
MIL-HDBK-267 Revision A:1987 | GUIDE FOR SELECTION OF LUBRICANTS & HYDRAULIC FLUIDS FOR USE IN SHIPBOARDS EQUIPMENT |
MIL-F-3541 Revision C:1989 | FITTING, LUBRICATION, GENERAL SPECIFICATION FOR |
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