MIL-F-7179 Revision G:1993
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM
Available format(s)
PDF
Superseded date
15-11-1997
Superseded by
Publisher
NO CONTENTS SECTION
Provides requirements for finishes, coatings and sealants for protection of aerospace weapons systems.
| Committee |
FSC MFFP
|
| DevelopmentNote |
Supersedes NAS 459. (04/2005)
|
| DocumentType |
Standard
|
| Pages |
29
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| MIL-M-87113 Revision A:1993 | MASK, OXYGEN, MBU-10/P |
| MIL-I-83294 Base Document:1971 | INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR |
| MIL-T-5842 Revision B:1985 | TRANSPARENT AREAS ON AIRCRAFT SURFACES [WINDSHIELDS AND CANOPIES] RAIN REMOVING AND WASHING SYSTEMS FOR, DEFROSTING, DEICING, DEFOGGING, GENERAL SPECIFICATION FOR |
| MIL-STD-2156 Base Document:1983 | LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
| MIL-A-83577 Revision B:1988 | ASSEMBLIES, MOVING MECHANICAL, FOR SPACE AND LAUNCH VEHICLES, GENERAL SPECIFICATION FOR |
| MIL STD 001303 : C | PAINTING OF NAVAL ORDNANCE EQUIPMENT |
| MIL-M-8555 Revision C:1984 | MISSILE, GUIDED, DESIGN AND CONSTRUCTION, GENERAL SPECIFICATION |
| MIL-A-85055 Base Document:1979 | Avionics System Performance Specification for A-4M/AV-8 Bombing Set, Angle Rate AN/ASB-19(V) |
| MIL-R-8236 Revision F:1995 | REEL, SHOULDER HARNESS, INERTIA LOCK |
| MIL-STD-7080 Base Document:1994 | SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
| MIL-I-82787 Base Document:1990 | IGNITER ASSEMBLY, ROCKET MOTOR MK 104 |
| MIL-L-50794 Base Document:1973 | Linear Shaped Charge Assembly |
| MIL-D-8684 Revision B:1959 | DATA AND TESTS, ENGINEERING, CONTACT REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE SYSTEMS |
| MIL-D-82687 Base Document:1980 | DEVICE, ARMING FIRING, ROCKET MOTOR MARK 298 MOD O |
| DOD-E-83578 Revision A:1987 | EXPLOSIVE ORDNANCE FOR SPACE VEHICLES, GENERAL SPECIFICATION FOR (METRIC) |
| 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 |
| 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 |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| 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)/11(2013) : 2013 | 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-N-8984 Base Document:1972 | NUT, SELF-LOCKING, STEEL, 260 KS1 FTU 450 DEGREES F |
| MIL-N-8985 Base Document:1972 | NUT, SELF-LOCKING STEEL, 180 KS1 FTU 450 DEGREES F |
| 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-H-8891 Revision A:1978 | HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR |
| MIL F 18264 : D | FINISHES: ORGANIC, WEAPONS SYSTEM, APPLICATION AND CONTROL OF |
| MIL-H-5440 Revision H:1993 | HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
| MIL-A-19736 Revision A:1960 | AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR |
| MIL-E-50796 Base Document:1973 | EXPANDING SHIELDED MILD DETONATING CORD ASSEMBLY |
| MIL-STD-1250 Revision A:1992 | CORROSION PREVENTION AND DETERIORATION CONTROL IN ELECTRONIC COMPONENTS AND ASSEMBLIES |
| MIL-M-25047 Revision C:1968 | MARKINGS AND EXTERIOR FINISH COLORS FOR AIRPLANES, AIRPLANE PARTS, AND MISSILES (BALLISTIC MISSILES EXCLUDED) |
| MIL-A-83469 Base Document:1976 | ADJUSTER, LAP BELT, 1-3/4 INCH WEBBING |
| MIL S 25057 : B | SCREEN SYSTEM, AIR INLET, AIRCRAFT TURBINE ENGINE, GENERAL SPECIFICATION FOR |
| MIL-B-81365 Base Document:1966 | BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR |
| MIL-E-7080 Revision B:1962 | ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF |
| MIL-HDBK-1250 Revision A:1995 | CORROSION PREVENTION AND DETERIORATION CONTROL IN ELECTRONIC COMPONENTS AND ASSEMBLIES |
| MIL-STD-1516 Revision B:1990 | UNIFIED CODE FOR COATINGS AND FINISHES FOR DOD MATERIAL |
| MIL-I-82826 Base Document:1985 | IGNITER ASSEMBLY |
| MIL-STD-2131 Revision A:1991 | LAUNCHER, EJECTION GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
| MIL-D-8685 Revision B:1967 | DATA AND TESTS, ENGINEERING, CONTRACT REQUIREMENTS FOR GUIDED MISSILE TARGET SYSTEMS |
| MIL-DTL-85110 Revision B:1997 | BAR, REPEATABLE RELEASE HOLDBACK (RRHB), AIRCRAFT LAUNCHING, GENERAL REQUIREMENT FOR |
| SAE AS8700 | Installation and Test of Electronic Equipment in Aircraft, General Specification for |
| MIL-C-22751 Revision D:1971 | COATING SYSTEM, EPOXY-POLYAMIDE, CHEMICAL AND SOLVENT RESISTANT, PROCESS FOR APPLICATION OF |
| MIL-S-83576 Base Document:1974 | SOLAR CELL ARRAYS, SPACE VEHICLE, DESIGN AND TESTING, GENERAL SPECIFICATION FOR |
| MIL-C-18187 Revision A:1965 | COATING, PROTECTIVE, APPLICATION TO FABRIC SURFACE OF AIRCRAFT |
| MIL-STD-1303 Revision B:1975 | PAINTING OF NAVAL ORDNANCE EQUIPMENT |
| MIL-I-8673 Base Document:1955 | INSTALLATION AND TEST OF AIRCRAFT FLEXIBLE WEAPONS SYSTEMS |
| MIL-C-81907 Base Document:1972 | COATING SYSTEM, POLYURETHANE, ALIPHATIC, WEATHER RESISTANT, PROCESS FOR APPLICATION OF |
| MIL-C-8507 Revision D:1963 | Coating, Wash Primer (Pretreatment) for Metals, Application of (for Aeronautical Use) |
| MIL-I-8700 Revision A:1970 | INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
| JSSG-2006 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
| MIL-I-85889 Base Document:1988 | IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
| MIL-S-81771 Revision A:1975 | Seat System; Aircrew, Crash Resistant; General Specification for |
| MIL-R-7051 Revision A:1966 | RELAY BANK, BOMB SALVO CIRCUIT 3 UNIT, 28 VOLT DC TYPE A 1 |
| DOD-E-8983 Revision C:1977 | ELECTRONIC EQUIPMENT, AEROSPACE, EXTENDED SPACE ENVIRONMENT, GENERAL SPECIFICATION FOR |
| MIL-STD-805 Revision B:1987 | TOWING FITTING AND PROVISIONS FOR FIXED WING AIRCRAFT, DESIGN, REQUIREMENTS FOR |
| MIL-P-83126 Revision A:1980 | PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
| MIL-R-23139 Revision B:1965 | ROCKET MOTORS, SURFACE LAUNCHED, DEVELOPMENT AND QUALIFICATION REQUIREMENTS FOR |
| ADS-13F-HDBK : 1997 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
| MIL-T-18232 Revision B:1968 | TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR |
| JSSG-2010-12 Base Document:1998 | Crew Systems Deployable Aerodynamic Decelerator (DAD) Systems Handbook |
| MIL-S-48405 Base Document:1973 | Shielded and Confined Mild Detonating Cord Assemblies |
| MIL-C-18263 Revision F:1971 | COLOR, EXTERIOR, NAVAL AIRCRAFT, REQUIREMENTS FOR |
| MIL-T-81838 Base Document:1971 | Tank, Fuel, Aircraft, Auxiliary External 300 Gallon, Type AERO-1D |
| MIL-W-18326 Revision A:1956 | WELDING OF MAGNESIUM ALLOYS, GAS AND ARC, MANUAL AND MACHINE PROCESSES FOR |
| 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 D 83753 : NOTICE 2 | DISPENSER, BOMB, TYPE SUU-21/A |
| MIL-I-8672 Revision B:1969 | INSTALLATION AND TEST OF AIRCRAFT PYROTECHNIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR [ASG] |
| MIL-C-8779 Revision E:1988 | COLOR, INTERIOR, AIRCRAFT, REQUIREMENTS FOR |
| MIL-T-5955 Revision C:1970 | TRANSMISSION SYSTEM, VTOL-STOL GENERAL REQUIREMENTS FOR |
| MIL-W-5013 Revision L:1991 | WHEEL AND BRAKE ASSEMBLIES - AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL C 81309 : E | CORROSION PREVENTIVE COMPOUND, WATER DISPLACING ULTRA-THIN FILM |
| MIL C 16173 : E | CORROSION PREVENTIVE COMPOUND, SOLVENT CUTBACK, COLD APPLICATION |
| MIL C 53072 : B | CHEMICAL AGENT RESISTANT COATING (CARC) SYSTEM APPLICATION PROCEDURES AND QUALITY CONTROL INSPECTION |
| MIL P 53022 : B | PRIMER, EPOXY COATING, CORROSION INHIBITING, LEAD & CHROMATE FREE |
| MIL C 85322 : B | COATING ELASTOMERIC, POLYURETHANE, RAIN EROSION RESISTANT, FOR EXTERIOR AIRCRAFT USE |
| MIL-A-46146 Revision B:1990 | ADHESIVE-SEALANTS, SILICONE, RTV, NONCORROSIVE (FOR USE WITH SENSITIVE METALS AND EQUIPMENT) |
| TT-L-190 Revision D:1976 | LINSEED OIL, BOILED, (FOR USE IN ORGANIC COATING) |
| MIL-STD-970 Base Document:1987 | STANDARDS AND SPECIFICATIONS, ORDER OF PREFERENCE FOR THE SELECTION OF |
| TT-P-2756 Revision A:1996 | POLYURETHANE COATING - SELF-PRIMING TOPCOAT, LOW VOLATILE ORGANIC COMPOUND (VOC) CONTENT |
| MIL P 85582 : B | PRIMER COATINGS: EPOXY, WATERBORNE |
| MIL-C-83445 Revision A:1980 | COATING SYSTEM, POLYURETHANE, NON-YELLOWING WHITE, RAIN EROSION RESISTANT, THERMALLY REFLECTIVE |
| MIL-A-9962 Revision A:1966 | ABRASIVE MATS, NON-WOVEN, NON-METALLIC |
| MIL-A-83377 Revision B:1978 | ADHESIVE BONDING (STRUCTURAL) FOR AEROSPACE AND OTHER SYSTEMS, REQUIREMENTS FOR |
| TT-P-1757 Revision B:1997 | PRIMER COATING, ALKYD BASE, ONE COMPONENT |
| MIL L 63460 : D | LUBRICANT, CLEANER AND PRESERVATIVE FOR WEAPONS AND WEAPONS SYSTEMS (METRIC) |
| MIL C 46081 : A | COATING COMPOUND, THERMAL INSULATING (INTUMESCENT) |
| MIL-C-83231 Revision A:1981 | COATING, POLYURETHANE, RAIN EROSION RESISTANT FOR EXTERIOR AIRCRAFT AND MISSILE PLASTIC PARTS |
| MIL-C-27725 Revision B:1969 | COATING, CORROSION PREVENTIVE, FOR AIRCRAFT INTEGRAL FUEL TANKS |
| MIL-S-8802 Revision F:1990 | SEALING COMPOUND, TEMPERATURE-RESISTANT, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES, HIGH ADHESION |
| MIL-C-6529 Revision C:1958 | CORROSION PREVENTIVE, AIRCRAFT ENGINE |
| MIL C 85285 : C | |
| MIL F 18264 : D | FINISHES: ORGANIC, WEAPONS SYSTEM, APPLICATION AND CONTROL OF |
| MIL S 5002 : D | SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS SYSTEMS |
| MIL P 23377 : G | PRIMER COATING, EPOXY, HIGH SOLIDS |
| MIL P 53030 : A | PRIMER COATING, EPOXY, WATER REDUCIBLE, LEAD & CHROMATE FREE |
| MIL-STD-889 Revision C:2016 | DISSIMILAR METALS |
| MIL-L-23398 Revision D:1985 | LUBRICANT, SOLID FILM, AIR DRYING, CORROSION INHIBITING, NATO CODE NUMBER S 749 |
| MIL-C-46168 Revision D:1987 | COATING, ALIPHATIC POLYURETHANE, CHEMICAL AGENT RESISTANT |
| MIL-C-5056 Base Document:1950 | Coating, Permanent Resin; Process for Application of, to Aircraft Parts |
| MIL R 3043 : B | RESIN COATING, UNPIGMENTED FOR ENGINE COMPONENTS AND METAL PARTS |
| MIL-C-8514 Revision C:1967 | COATING, COMPOUND, METAL PRETREATMENT, RESIGN ACID [ASG] |
| MIL C 22750 : F | COATING, EPOXY, VOC-COMPLIANT |
| MIL-C-8779 Revision E:1988 | COLOR, INTERIOR, AIRCRAFT, REQUIREMENTS FOR |
| MIL-C-8507 Revision D:1963 | Coating, Wash Primer (Pretreatment) for Metals, Application of (for Aeronautical Use) |
| MIL C 5541 : E | CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MIL T 83483 : B | THREAD COMPOUND, ANTISEIZE, MOLYBDENUM DISULFIDE-PETROLATUM |
| TT-P-28 Revision H:2007 | PAINT, ALUMINUM, HEAT RESISTING |
| MIL C 85054 : B | CORROSION PREVENTIVE COMPOUND, WATER DISPLACING, CLEAR (AMLGUARD) |
| MIL S 81733 : C | SEALING AND COATING COMPOUND CORROSION INHIBITIVE |
| MIL-S-29574 Base Document:1989 | SEALING COMPOUND, POLYTHIOETHER, FOR AIRCRAFT STRUCTURES, FUEL AND HIGH TEMPERATURE RESISTANT, FAST CURING AT AMBIENT AND LOW TEMPERATURE |
| MIL-S-38249 Base Document:1964 | SEALING COMPOUND, FIREWALL |
| MIL-C-11796 Revision C:1986 | CORROSION PREVENTIVE COMPOUND, PETROLATUM, HOT APPLICATION |
| MIL-STD-2161 Revision C:2014 | Paint Schemes and Exterior Markings for U.S. Navy and Marine Corps Aircraft |
| MIL C 53039 : A | COATING, ALIPHATIC POLYURETHANE, SINGLE COMPONENT, CHEMICAL AGENT RESISTANT |
| MIL-B-5087 Revision B:1964 | BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS |
| MIL L 46010 : D | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING |
| MIL-C-83286 Revision B:1973 | COATING URETHANE, ALIPHATIC ISOCYANATE, FOR AEROSPACE APPLICATIONS |
| VV-L-800 Revision C:1983 | LUBRICATING OIL, GENERAL PURPOSE, PRESERVATIVE, (WATER-DISPLACING, LOW TEMPERATURE) |
| TT-P-2760 Revision A:1994 | PRIMER COATING; POLYURETHANE, ELASTOMERIC |
| MIL-STD-171 Revision F:2011 | FINISHING OF METAL AND WOOD SURFACES |
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