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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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LUBRICATION OF MILITARY EQUIPMENT
Available format(s)
PDF
Publisher
Superseded date
03-12-1997
Superseded by
£15.19
Excluding VAT
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Superseded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 (NO S/S DOCUMENT) |
| 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) (No S/S Document) |
| 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 for (No S/S Document) |
| 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) (S/S by A-A-52558) |
| MIL-D-8684 Revision B:1959 | Data and Tests, Engineering, Contact Requirements for Air Launched Guided Missile Systems (No S/S Document) |
| 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 (No S/S Document) |
| 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 Defueling and Receiving (No S/S Document) |
| 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 Weapons Systems (S/S by MIL-STD-1587) |
| 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 (No S/S Document) |
| 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 (No S/S Document) |
| GG-T-35 Revision C:1989 | TABLES; DRAWING, TRACING, AND SCRIBING (NO S/S DOCUMENT) |
| MIL-T-52942 Revision C:1996 | TRUCK, FIRE FIGHTING: PUMPER, 1000 GPM; LADDER/WATER TOWER COMBINATION (NO S/S DOCUMENT) |
| 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 | Manuals, Technical: Intermediate Maintenance Instructions (S/S by MIL-M-6675) |
| 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 (S/S BY MIL-HDBK-1250) |
| MIL H 81529 : 0 | HOOK, HELICOPTER EXTERNAL CARGO, 6,000 POUND CAPACITY TYPE A |
| MIL-P-5994 Revision D:1972 | Pump Units, Hydraulic, Electric Motor Driven, Variable Delivery, General Specification for (No S/S Document) |
| MIL-T-25363 Revision D:1973 | Accumulator, Pneumatic, Aircraft, Glass Fiber (S/S by MIL-R-8573) |
| 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 (No S/S Document) |
| 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 (S/S by AS12500) |
| MIL-S-6150 Revision D:1987 | STARTER: ENGINE, ELECTRICAL, DIRECT CRANKING AIRCRAFT, 28 VOLTS DC (NO S/S DOCUMENT) |
| 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 (NO S/S DOCUMENT) |
| 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 (No S/S Document) |
| 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 (S/S by AFGS-87235) |
| MIL-M-38789 Revision A:1970 | Manuals, Technical: Overhaul Instructions and Overhaul Instructions with Illustrated Parts Breakdown (for Various Equipment and Accessories) (S/S by MIL-M-87929 and MIL-M-81928) |
| MIL-S-18471 Revision G:1983 | System, Aircrew Automated Escape, Ejection Seat Type, General Specification For |
| MIL-T-18232 Revision B:1968 | Targets, Aerial, Powered, Design and Construction of General Specification for (No S/S Document) |
| MIL-B-467 Revision E:1988 | Breakers, Paving: Pneumatic (S/S by A-A-52599) |
| 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 (No S/S Document) |
| 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 | Aircraft Structures |
| MIL-M-5166 Revision D:1983 | Manual, Technical: Assembly, Servicing, and Field Maintenance Instructions, with Illustrated Parts Breakdown (for Guided Missiles and Pilotless Aircraft) (S/S by MIL-M-87929) |
| 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 (No S/S Document) |
| MIL-I-58067 Revision A:1977 | Indicator, Vertical Velocity, Rapid Response Acceleration Sensitive, General Specification for (No S/S Document) |
| MIL-S-6551 Revision A:1981 | Seat, Crew, Downward Ejection, Aircraft |
| MIL-A-25915 Revision A:1980 | Accelerometer, Aircraft, Pilot\'s Warning, Type MA-2 (No S/S Document) |
| MIL M 9864 : B | MANUALS, TECHNICAL: ORGANIZATIONAL MAINTENANCE (MISSILE AND SPACE SYSTEMS) |
| MIL A 25088 : C | |
| MIL-P-52405 Revision C:1990 | Pumps, Centrifugal, Electronic-Motor-Driven (For Water) |
| MIL-H-27269 Revision A:1977 | Horizontal Situation Indicator Group AF/A24J-1 (No S/S Document) |
| DOD-HDBK-791 Base Document:1988 | Maintainability Design Techniques Metric |
| 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 (No S/S Document) |
| 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 (NO S/S DOCUMENT) |
| MIL-M-25394 Revision A:1969 | Manuals, Technical: Overhaul Instructions and Intermediate Maintenance Instructions (for Engines) (S/S by MIL-M-87929) |
| 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 (S/S by MIL-E-87145) |
| MIL-I-38391 Base Document:1965 | Indicator, Electrical Tachometer, ERU-12/A 0-350 RPM (Rotor), 0-7000 RPM (Engine) (No S/S Document) |
| 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 1.0, Type ME-5 (No S/S Document) |
| 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 (No S/S Document) |
| MIL-I-27680 Revision C:1973 | Indicator, Altitude ARU-12/A, Remote (No S/S Document) |
| MIL-I-27623 Revision C:1972 | Indicator, Attitude, Remote Standby, 2 Inch (No S/S Document) |
| MIL-I-83117 Revision B:1975 | Indicator, Angle of Attack (No S/S Document) |
| 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 (No S/S Document) |
| MIL-M-63038 Revision D:1993 | MANUALS, TECHNICAL: UNIT OR AVIATION UNIT, DIRECT SUPPORT, AVIATION INTERMEDIATE, AND GENERAL SUPPORT MAINTENANCE, REQUIREMENTS FOR (S/S BY MIL-STD-40051) |
| MIL-I-27619 Revision G:1974 | Indicators, Attitude Director |
| MIL-A-53099 Base Document:1990 | Arctic Forward Area Refueling Equipment (AFARE) (No S/S Document) |
| 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 VII (S/S BY SAE-AS15720) |
| 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 I (S/S BY SAE-AS15001) |
| MIL-STD-143 Revision B:1969 | STANDARDS & SPECIFICATIONS, ORDER OF PRECEDENCE FOR THE SELECTION OF (S/S BY MIL-STD-970) |
| 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 and Hydraulic Fluids for usein Shipboard Equipment |
| MIL-F-3541 Revision C:1989 | Fittings, Lubrication, General Specification for (S/S by SAE-AS35411) |
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