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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
LUBRICATION OF MILITARY EQUIPMENT
Available format(s)
PDF
Superseded date
03-12-1997
Superseded by
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.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Superseded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 | System, Aircrew Automated Escape, Ejection Seat Type, General Specification For |
| 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, 4,000 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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