MIL-F-7179 Revision G:1993
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM
11-15-1997
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Superseded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 AS 8700 : 1999 | 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 |
Please Login or Create an Account so you can add users to your Multi user PDF Later.
Important note : All end users must be registered with an Account prior to user licenses being assigned.
Users cannot be edited or removed once added to your Multi user PDF.
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.