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MIL-STD-838 Revision C:1983

Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

LUBRICATION OF MILITARY EQUIPMENT
Available format(s)

PDF

Superseded date

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Superseded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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