MIL-M-3171 Revision C:1966
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
MAGNESIUM ALLOY PROCESSES FOR PRETREATMENT AND PREVENTION OF CORROSION
Available format(s)
PDF
Superseded date
07-05-1998
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.Describes processing of magnesium base alloys to increase corrosion resistance and produce surfaces suitable for organic paint finish systems.
| Committee |
AREA MFFP
|
| DocumentType |
Standard
|
| Pages |
45
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| Standards | Relationship |
| SAE AMS2475G | Similar to |
| SAE AMS M 3171 : 1998 | Similar to |
| SAE AMS M 3171 : 2011 | Similar to |
| MIL-I-8580 Revision B:1965 | INDICATOR, TACHOMETER, HELICOPTER, 0-4000 RPM TYPE MA 1 |
| MIL-M-8609 Revision B:1965 | MOTOR, DC 28 VOLT SYSTEM AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-A-83577 Revision B:1988 | ASSEMBLIES, MOVING MECHANICAL, FOR SPACE AND LAUNCH VEHICLES, GENERAL SPECIFICATION FOR |
| DWA-M 143-20:2018 | TEST METHOD FOR DROP IMPACT RESISTANCE OF BLOW-MOLDED THERMOPLASTIC CONTAINERS |
| MIL-C-19853 Revision D:1994 | CARBON REMOVING COMPOUND (FOR USE IN AGITATED TANK) |
| MIL C 53072 : B | CHEMICAL AGENT RESISTANT COATING (CARC) SYSTEM APPLICATION PROCEDURES AND QUALITY CONTROL INSPECTION |
| MIL M 46039 : A | MAGNESIUM ALLOY BAR, ROD AND SPECIAL SHAPED SECTIONS, EXTRUDED (ZK21A) |
| MIL I 7627 : F | INDICATOR, TURN AND SLIP 28V DC |
| MIL-A-8243 Revision D:1985 | ANTI-ICING AND DEICING-DEFROSTING FLUIDS |
| SAE ARP1481A | Corrosion Control and Electrical Conductivity in Enclosure Design |
| MIL-C-27298 Revision B:1980 | CLOCK, AIRCRAFT, MECHANICAL ABU AND 9-A |
| MIL-PRF-3043 Revision C:1998 | RESIN COATING, PERMANENT, FOR ENGINE COMPONENTS AND METAL PARTS |
| MIL-STD-193 Revision L:1991 | PAINTING PROCEDURES AND MARKING FOR VEHICLES, CONSTRUCTION EQUIPMENT, MATERIAL HANDLING EQUIPMENT, AND SPARE PARTS |
| MIL P 85582 : B | PRIMER COATINGS: EPOXY, WATERBORNE |
| MIL-B-8568 Revision B:1967 | BINOCULAR, PRISMATIC, HAND-HELD [FOR AERONAUTICAL USE] 7 X 50 AND 6 X 42 WIDE FIELD [ASG] |
| MIL-C-7135 Revision F:1967 | Compressor, Pneumatic, 3,000 PSI -- 2 SCFM Aero 2A (*), Aero 2A-1 (*), Aero 2B (*), and Aero 2B-1 (*) |
| MIL-I-81186 Base Document:1966 | INDICATOR, RATE OF FUEL FLOW SYNCHRO TYPE, M590360 |
| MIL-I-21206 Revision B:1960 | Indicator, Rate of Flow, Fuel; EFU-7/A (300-5000-15000 PPH) |
| MIL-PRF-87978 Revision A:1996 | REMOVER, PAINT, EPOXY AND POLYURETHANE SYSTEMS, TANK TYPE, AMBIENT TEMPERATURE, FOR AIRCRAFT WHEELS AND LANDING GEAR COMPONENTS |
| TT-R-2918 Revision A:2001 | REMOVAL, PAINT, NO HAZARDOUS AIR POLLUTANTS (HAPS) |
| MIL R 87978 : LATEST | REMOVER, PAINT, EPOXY AND POLYURETHANE SYSTEMS, TANK TYPE: AMBIENT TEMPERATURE, FOR AIRCRAFT WHEELS AND LANDING GEAR COMPONENTS |
| MIL G 9398 : C | GENERATOR, TACHOMETER, TWO POLE HIGH TEMPERATURE AIRCRAFT |
| DOD-E-83578 Revision A:1987 | EXPLOSIVE ORDNANCE FOR SPACE VEHICLES, GENERAL SPECIFICATION FOR (METRIC) |
| MIL-P-43116 Revision A:1964 | PIKE,WIRE AND PIKES, POLE |
| MIL-C-23367 Base Document:1963 | Computer, Flight Director, Aircraft |
| ASTM D 2651 : 2001 : R2008 | Standard Guide for Preparation of Metal Surfaces for Adhesive Bonding |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-A-23121 Revision C:1970 | AIRCREW ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM, 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 |
| MIL-PRF-25134 Revision C:1996 | REMOVER, PAINT AND LACQUER, SOLVENT TYPE |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | 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 |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL T 28800 : E | TEST EQUIPMENT FOR USE WITH ELECTRICAL AND ELECTRONIC EQUIPMENT GENERAL SPECIFICATION FOR |
| 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)/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-DTL-1716 Revision J:1997 | POLE, TENT, TELESCOPIC, ADJUSTABLE 5 FEET TO 9 FEET, MAGNESIUM |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| SAE AMSC19853 | Carbon Removing Compound (For Use in Agitated Tank) |
| MIL-S-26547 Revision C:1985 | STARTER-GENERATOR ENGINE STU-6A |
| MIL S 5002 : D | SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS SYSTEMS |
| MIL-T-22913 Revision C:1971 | TIMER (FOR TORPEDO MARK 37 MOD 2) |
| MIL F 18264 : D | FINISHES: ORGANIC, WEAPONS SYSTEM, APPLICATION AND CONTROL OF |
| MIL-P-21415 Revision C:1973 | PROTECTIVE FINISH AND PAINTING FOR POLARIS FLEET BALLISTIC MISSILE |
| SAE ARP 6256 : 2014 | MAGNESIUM ALLOYS IN AIRCRAFT SEATS - ENGINEERING DESIGN AND FABRICATION RECOMMENDED PRACTICES |
| MIL C 7907 : A | CLEANING COMPOUND, DECONTAMINATING [FOR SOILED AND RADIOACTIVE CONTAMINATED SURFACES] |
| MIL-C-87936 Revision A:1985 | CLEANING COMPOUNDS, AIRCRAFT EXTERIOR SURFACES, WATER DILUTABLE |
| MIL M 8917 : A NOTICE 2 | MAGNESIUM ALLOY SHEET AND PLATE [HM 21A - TB] [ASG] |
| MIL I 82356 : NOTICE 1 | INSTRUMENTS, SIMULATED, FOR AIRCRAFT TRAINING DEVICES; GENERAL SPECIFICATION FOR |
| MIL G 26611 : D | GENERATOR, TACHOMETER GEU-7/A, MINIATURE |
| MIL-G-23337 Base Document:1962 | GAGE - PRESSURE, DIAL INDICATING |
| MIL-P-514 Revision D:1966 | PLATE, IDENTIFICATION, INSTRUCTION AND MARKING BLANK |
| MIL P 26517 : A | POWER SUPPLY, TRANSFORMER-RECTIFIER, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL S 25057 : B | SCREEN SYSTEM, AIR INLET, AIRCRAFT TURBINE ENGINE, GENERAL SPECIFICATION FOR |
| MIL-STD-649 Revision C:1976 | ALUMINUM AND MAGNESIUM PRODUCTS PREPARATION FOR SHIPMENT AND STORAGE |
| MIL-C-43616 Revision C:1981 | CLEANING COMPOUND, AIRCRAFT SURFACE |
| MIL-STD-1516 Revision B:1990 | UNIFIED CODE FOR COATINGS AND FINISHES FOR DOD MATERIAL |
| MIL-T-21578 Revision A:1966 | TEST EQUIPMENT, HAZARDOUS LOCATION, INSTALLED, BASIC REQUIREMENTS FOR |
| MIL-S-6150 Revision D:1987 | STARTER, ENGINE, ELECTRICAL, DIRECT CRANKING, AIRCRAFT 28 VOLT DC |
| MIL-M-45202 Revision C:1981 | MAGNESIUM ALLOY, ANODIC TREATMENT OF |
| MIL-T-704 Revision K:1992 | Treatment and Painting of Material |
| MIL R 46963 : A | ROCKET MOTOR, M42A1, BOOSTER |
| MIL C 4928 : A | CHARGER, BATTERY, SILICON DIODE, TYPE A-1 |
| MIL C 15370 : F | COUPLERS, DIRECTIONAL GENERAL SPECIFICATION FOR |
| ASTM B 879 : 1997 | Standard Practice for Applying Non-Electrolytic Conversion Coatings on Magnesium and Magnesium Alloys |
| ASTM B 879 : 1997 : R2008 : EDT 1 | Standard Practice for Applying Non-Electrolytic Conversion Coatings on Magnesium and Magnesium Alloys |
| MIL P 21698 : A | PAINT, FLUORESCENT, FOR AIRCRAFT, PROCESS FOR APPLICATION OF |
| MIL-C-22751 Revision D:1971 | COATING SYSTEM, EPOXY-POLYAMIDE, CHEMICAL AND SOLVENT RESISTANT, PROCESS FOR APPLICATION OF |
| MIL-M-26696 Base Document:1959 | MAGNESIUM ALLOY BAR, ROD AND SPECIAL SHAPED SECTIONS EXTRUDED (P)ZK6OB |
| MIL-C-83873 Revision A:1993 | CLEANING COMPOUND, PRECOATING SURFACE, AIRCRAFT & AEROSPACE GROUND EQUIPMENT (AGE) |
| TT-R-248 Revision B:1981 | REMOVER, PAINT AND LACQUER, SOLVENT TYPE |
| MIL-S-85510 Base Document:1981 | Seats, Helicopter Cabin, Crashworthy, General Specification for |
| MIL-S-7852 Revision B:1968 | SEAT, AIRCREW, ADJUSTABLE SWIVEL TYPE E-1 |
| MIL-B-26793 Revision B:1958 | BLOWER, GASOLINE ENGINE DRIVEN, TYPE A-1 |
| MIL-A-26107 Revision D:1960 | AIR CONDITIONER, TRAILER-MOUNTED, FREON CYCLE, 11-1/2 TON REFRIGERATING CAPACITY, TYPE MA-3 |
| MIL-I-27273 Revision A:1965 | Inverter, Power, Static, General Specification for |
| MIL-R-19750 Revision A:1958 | REGULATOR; VOLTAGE, 28 V, 120 DEGREE C, FOR 30 V DIRECT-CURRENT GENERATOR, GENERAL SPECIFICATION FOR |
| MIL-I-19028 Revision E:1971 | INVERTER (FOR TORPEDO MARK 37 MODS O, O)M(, 1, 2, AND 3) |
| MIL-M-26075 Revision D:1969 | MAGNESIUM-ALLOY SHEET AND PLATE (HK31A) |
| MIL-M-46143 Base Document:1988 | MAGNESIUM LITHIUM ALLOY CASTINGS (LS141A AND LZ145A) |
| QQ-M-38 Revision B:1969 | MAGNESIUM ALLOY DIE CASTINGS (AZ91A) |
| MIL-V-5461 Revision C:1977 | VALVE, VACUUM BREAKING |
| WW-T-825 Revision B:1971 | TUBE, MAGNESIUM-ALLOY, EXTRUDED |
| MIL-PRF-83936 Revision C:1996 | REMOVER, PAINT, TANK TYPE - FOR AIRCRAFT WHEELS, LANDING GEAR COMPONENTS AND OTHER AIRCRAFT AND SUPPORT EQUIPMENT |
| MIL-I-22075 Revision C:1984 | Indicator, Bearing-Distance-Heading ID-663D/U |
| ASTM B 879 : 1997 : R2003 : EDT 1 | Standard Practice for Applying Non-Electrolytic Conversion Coatings on Magnesium and Magnesium Alloys |
| MIL-STD-808 Revision A:1983 | FINISH, MATERIALS AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN SUPPORT EQUIPMENT |
| MIL S 25073 : 0 | |
| MIL T 25439 : A (1) | TRANSMITTER, RATE OF FLOW, IN-FLIGHT REFUELLING, 0-10,000 PPM, TYPE MB-3 |
| QQ-M-44 Revision B:1964 | MAGNESIUM ALLOY PLATE AND SHEET (AZ31B) |
| QQ-M-56 Revision B:1960 | MAGNESIUM ALLOY, SAND CASTINGS |
| MIL-PRF-85704 Revision C:1998 | CLEANING COMPOUND, TURBINE ENGINE GAS PATH |
| ASTM B 90M : 1990 | Specification for Magnesium-Alloy Sheet and Plate (Metric) (Withdrawn 1993) |
| NASA MSFC HDBK 3697 : 2014 | ELECTRICAL BONDING DESIGN GUIDE HANDBOOK |
| MIL G 6162 : B | GENERATOR AND STARTER GENERATOR, ELECTRIC DIRECT CURRENT, NOMINAL 30 VOLTS AIRCRAFT GENERAL SPECIFICATION |
| MIL-I-18804 Revision B:1964 | INDICATOR, VERTICAL SPEED, 0 - 6000 FPM, 2 INCH |
| NASA MSFC SPEC 250 : 1963 | PROTECTIVE FINISHES FOR SPACE VEHICLE STRUCTURES AND ASSOCIATED FLIGHT EQUIPMENT GENERAL SPECIFICATION FOR |
| MIL-R-24358 Base Document:1968 | RESTORATION SHIPBOARD ELECTRONIC EQUIPMENT F, 1N AND 2N COGNIZANCE |
| MIL S 9479 : C | |
| MIL-I-58067 Revision A:1977 | INDICATOR, VERTICAL VELOCITY, RAPID RESPONSE ACCELERATION SENSITIVE, GENERAL SPECIFICATION FOR |
| MIL-S-3151 Revision A:1967 | SOUND LEVEL MEASURING AND ANALYZING EQUIPMENT |
| MIL-S-6551 Revision A:1981 | |
| MIL-G-81168 Base Document:1964 | GYROSCOPE, RATE INTEGRATING |
| MIL-C-81991 Base Document:1975 | CONVERTER, AIRCRAFT DC TO DC, BOOST GENERAL SPECIFICATION FOR |
| MIL-I-22126 Revision B:1972 | INDICATOR, TORQUEMETER, ENGINE, TURBOPROP |
| MIL-R-23761 Revision B:1975 | Regulators, Voltage, and Control Panels Aircraft, Direct Current Generator, General Specification for |
| MIL-I-23366 Revision B:1987 | Indicator, Horizontal Situation ID-1013(*)/A |
| MIL R 83936 : B | REMOVER, PAINT, TANK TYPE, FOR AIRCRAFT WHEELS, LANDING GEAR COMPONENTS, AND OTHER AIRCRAFT AND AGE COMPONENTS |
| MIL-G-23723 Base Document:1964 | Gyroscope, Rate Switching CN-495/AJB-3 |
| SAE AMSM45202B | Magnesium Alloys, Anodic Treatment of |
| MIL G 23701 : 0 | MILITARY SPECIFICATION GYROSCOPE, RATE SWITCHING AN/ASN-52 |
| DOD-E-8983 Revision C:1977 | ELECTRONIC EQUIPMENT, AEROSPACE, EXTENDED SPACE ENVIRONMENT, GENERAL SPECIFICATION FOR |
| P-C-444 Revision B:1983 | CLEANING COMPOUND, SOLVENT SOLUBLE, GREASE EMULSIFYING |
| MIL-C-22542 Revision B:1987 | CLEANING COMPOUND, HIGH PRESSURE CLEANER, LIQUID |
| MIL-P-85034 Base Document:1976 | POWER PACKAGE, EMERGENCY AC/DC GENERATOR, RAM AIR TURBINE DRIVEN |
| ADS-13F-HDBK : 1997 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
| MIL-H-9896 Revision C:1988 | HARDWARE, UNIVERSAL LOAD CARRYING SLING |
| MIL-PRF-29607 Base Document:1996 | CLEANING COMPOUND, AVIONICS COMPONENTS, NON-OZONE DEPLETING |
| MIL STD 194 : A NOTICE 2 | SYSTEM FOR PAINTING AND FINISHING FIRE-CONTROL MATERIEL |
| MIL-B-23072 Base Document:1961 | BLOWER, ANTI-EXPOSURE SUIT VENTILATION, GENERAL SPECIFICATION FOR |
| MIL C 87937 : B | CLEANING COMPOUND, AEROSPACE EQUIPMENT |
| MIL-B-2481 Revision E:1973 | BULLS EYES, RIGGING, 5/16 INCH INSIDE DIAMETER |
| MIL-A-22424 Revision A:1967 | ADAPTERS, COMPENSATING, MS281O7, MA-1 COMPASS SYSTEM |
| MIL-STD-2110 Base Document:1979 | RESTORATION, OVERHAUL, AND REPAIR OF ELECTRONIC EQUIPMENT |
| MIL-R-81294 Revision D:1990 | REMOVER, PAINT, EPOXY, POLYSULPHIDE AND POLYURETHANE SYSTEMS |
| SAE AS8568A | Binoculars, Prismatic, Hand-Held (for Aeronautical Use) (7 × 50 and 6 × 42 (Wide Field)) |
| MIL-F-8378 Revision B:1975 | FREQUENCY METERS, AIRCRAFT 380 TO 420 HERTZ AND 350 TO 450 HERTZ |
| MIL-W-18326 Revision A:1956 | WELDING OF MAGNESIUM ALLOYS, GAS AND ARC, MANUAL AND MACHINE PROCESSES FOR |
| MIL-R-81835 Base Document:1971 | REMOVER, ORGANIC COATING, HOT TANK TYPE |
| MIL-T-23142 Revision B:1977 | TAPE, PRESSURE-SENSITIVE ADHESIVE, FOR DISSIMILAR METAL SEPARATION |
| DOD-HDBK-343 Base Document:1986 | DESIGN, CONSTRUCTION, & TESTING REQUIREMENTS FOR ONE OF A KIND SPACE EQUIPMENT |
| MIL-HDBK-1568 Base Document:1996 | MATERIAL AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS |
| MIL P 47115 : A | PAINT, EPOXY, ABRASION, HEAT AND CORROSION RESISTANT |
| MIL-T-25485 Revision C:1974 | TRANSMITTER, THRUST, SINGLE SYNCHRO STYLE, PRESSURE RATIO, TYPE MK-2 |
| MIL G 5413 : D NOTICE 1 | GENERATOR, TACHOMETER, FOUR POLE |
| MIL-I-5415 Revision C:1987 | INDICATOR, AIR SPEED, PITOT STATIC PRESSURE GENERAL SPECIFICATION FOR |
| MIL-T-5583 Revision C:1987 | Transmitter, Position, 28 Volts DC |
| MIL-M-7969 Revision C:1965 | Motors, Alternating Current, 400-Cycle, 115/200-Volt System, Aircraft, General Specification for |
| MIL G 21480 : A | GENERATOR SYSTEM, 400 HERTZ ALTERNATING CURRENT, AIRCRAFT GENERAL SPECIFICATION FOR |
| MIL-P-6906 Revision B:1969 | PLATE, IDENTIFICATION AIRCRAFT |
| MIL-I-23524 Revision A:1986 | INDICATOR, ATTITUDE DIRECTOR, REMOTE, ID 1329A (V) |
| MIL R 3043 : B | RESIN COATING, UNPIGMENTED FOR ENGINE COMPONENTS AND METAL PARTS |
| MIL-I-26299 Revision G:1990 | INDICATORS, RATE OF FLOW, 0-5,000 PPH, INTEGRALLY LIGHTED |
| MIL-I-23832 Revision A:1980 | Indicator, Tachometer, Triple Pointer, Helicopter |
| MIL-I-81049 Revision A:1972 | INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, VOLTAGE COMPENSATED, MULTIFUNCTION |
| MIL R 6466 : B NOTICE 1 | RELAY, ARMATURE, EXCITER PROTECTION, TYPE A-1 |
| MIL C 85570 : B (1) | CLEANING COMPOUND, AIRCRAFT, EXTERIOR |
| ASTM D 2651 : 2001 | Standard Guide for Preparation of Metal Surfaces for Adhesive Bonding |
| MIL F 14072 : D | FINISHES FOR GROUND BASED ELECTRONIC EQUIPMENT |
| SAE AMSR81835 | Remover, Organic Coating, Hot Tank Type |
| ASTM B 879 : 1997 : R2013 | Standard Practice for Applying Non-Electrolytic Conversion Coatings on Magnesium and Magnesium Alloys |
| ASTM D 2651 : 2001 : R2016 | Standard Guide for Preparation of Metal Surfaces for Adhesive Bonding |
| MIL M 46080 : LATEST | MAGNESIUM CASTINGS; PROCESS FOR ANODIC CLEANING AND SURFACE SEALING OF |
| MIL-STD-105 Revision E:1989 | SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.