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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 Systems (S/S by MIL-STD-7179)
Available format(s)
PDF
Published date
14-04-1993
Publisher
Superseded date
15-11-1997
Superseded by
£13.91
Excluding VAT
NO CONTENTS SECTION
Provides requirements for finishes, coatings and sealants for protection of aerospace weapons systems.
| DevelopmentNote |
Supersedes NAS 459. (04/2005)
|
| DocumentType |
Standard
|
| Pages |
26
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
This specification establishes the minimum requirements for finishes, protective coatings, and sealants used in the protection of aerospace weapons systems (see 6.1).
| 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 (No S/S Document) |
| MIL-T-5842 Revision B:1985 | Transparent Areas On Aircraft Surfaces (Windshields And Canopies), Rain Removing And Washing Systems For, De-Frosting, De-Icing, 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 (No S/S Document) |
| MIL STD 001303 : C | PAINTING OF NAVAL ORDNANCE EQUIPMENT |
| MIL-M-8555 Revision C:1984 | Missile, Guided, Design and Construction, General Specification for (No S/S Document) |
| 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 and Installation of Aircraft Electric Equipment |
| MIL-I-82787 Base Document:1990 | Igniter Assembly, Rocket Motor MK 104 (No S/S Document) |
| 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 (No S/S Document) |
| MIL-D-82687 Base Document:1980 | Device, Arming Firing, Rocket Motor Mark 298 Mod 0 |
| DOD-E-83578 Revision A:1987 | EXPLOSIVE ORDNANCE FOR SPACE VEHICLES, GENERAL SPECIFICATION FOR (METRIC) (NO S/S DOCUMENT) |
| 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 |
| 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 |
| 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 KSI FTU, 450 DEG. F (S/S BY NASM8984) |
| MIL-N-8985 Base Document:1972 | NUT, SELF LOCKING STEEL, 180 KSI FTU, 450 DEGREE F (S/S BY NASM8985) |
| 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 III 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, Design and Installation Requirements for (S/S by SAE-AS5440) |
| MIL-A-19736 Revision A:1960 | Air Refueling 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 (S/S BY MIL-HDBK-1250) |
| MIL-M-25047 Revision C:1968 | Markings and Exterior Finish Colors for Airplanes, Airplane Parts, and Missiles (Ballistic Missiles Excluded) (No S/S Document) |
| MIL-A-83469 Base Document:1976 | Adjuster, Lap Belt, 1-3/4 Inch Webbing (No S/S Document) |
| MIL S 25057 : B | SCREEN SYSTEM, AIR INLET, AIRCRAFT TURBINE ENGINE, GENERAL SPECIFICATION FOR |
| MIL-B-81365 Base Document:1966 | Bleed Air Systems, General Specification for |
| MIL-E-7080 Revision B:1962 | Electric Equipment, Aircraft, Selection and Installation of (S/S by MIL-STD-7080) |
| MIL-HDBK-1250 Revision A:1995 | Corrosion Prevention and Deterioration Control in Electronic Components and Assemblies (S/S by AS12500) |
| MIL-STD-1516 Revision B:1990 | Unified Code for Coating and Finishes for DOD Materiel (No S/S Document) |
| MIL-I-82826 Base Document:1985 | Igniter Assembly (No S/S Document) |
| 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 (No S/S Document) |
| 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 (No S/S Document) |
| MIL-S-83576 Base Document:1974 | SOLAR CELLS ARRAYS, SPACE VEHICLE, DESIGN AND TESTING, GENERAL SPECIFICATION FOR (NO S/S DOCUMENT) |
| MIL-C-18187 Revision A:1965 | Costings, Protective; Application to Fabric Surfaces of Aircraft (No S/S DOCUMENT) |
| MIL-STD-1303 Revision B:1975 | Painting of Naval Ordnance Equipment (No S/S Document) |
| MIL-I-8673 Base Document:1955 | Installation and Test of Aircraft Flexible Weapons Systems (No S/S Document) |
| MIL-C-81907 Base Document:1972 | Coating System, Polyurethane, Aliphatic, Weather Resistant: Process for Application of (No S/S Document) |
| 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 (S/S by SAE-AS8700) |
| JSSG-2006 Base Document:1998 | 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 (NO S/S DOCUMENT) |
| 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 | Targets, Aerial, Powered, Design and Construction of General Specification for (No S/S Document) |
| 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 | Colors, Exterior, Naval Aircraft: Requirements for (S/S by MIL-STD-2161) |
| MIL-T-81838 Base Document:1971 | Tank, Fuel, Aircraft, Auxiliary External 300 Gallon, Type Aero-1D (No S/S Document) |
| MIL-W-18326 Revision A:1956 | WELDING OF MAGNESIUM ALLOYS, GAS AND ARC, MANUAL AND MACHINE PROCESSES FOR (S/S BY MIL-STD-2219) |
| DOD-HDBK-343 Base Document:1986 | Design, Construction, and Testing Requirements for one of a Kind Space Equipment (No S/S Document) |
| MIL-HDBK-1568 Base Document:1996 | Material and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems (S/S by MIL-STD-1568) |
| 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 (No S/S Document) |
| MIL-C-8779 Revision E:1988 | Colors, Interior, Aircraft, Requirements for |
| MIL-T-5955 Revision C:1970 | TRANSMISSION SYSTEM, VTOL - STOL, GENERAL REQUIREMENTS FOR (NO S/S DOCUMENT) |
| 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 | Adhesives-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) (S/S BY A-A-371) |
| MIL-STD-970 Base Document:1987 | STANDARDS AND SPECIFICATIONS, ORDER OF PREFERENCE FOR THE SELECTION OF (NO S/S DOCUMENT) |
| TT-P-2756 Revision A:1996 | Polyurethane Coating: Self-Priming Topcoat, Low Volatile Organic Compounds (VOC) Content (No S/S Document) |
| 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 (S/S by SAE-AMS-C-83445) |
| MIL-A-9962 Revision A:1966 | Abrasive Mats, Non-Woven, Non-Metallic (S/S by A-A-58054) |
| MIL-A-83377 Revision B:1978 | Adhesive Bonding (Structural) for Aerospace and Other Systems, Requirements for (No S/S Document) |
| 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 | Coatings, Polyurethane, Rain Erosion Resistant for Exterior Aircraft and Missile Plastic Parts (S/S by SAE-AMS-C-83231) |
| MIL-C-27725 Revision B:1969 | Coating, Corrosion Preventive, for Aircraft Integral Fuel Tanks (S/S by SAE-AMS-C-27725) |
| MIL-S-8802 Revision F:1990 | SEALING COMPOUND, TEMPERATURE-RESISTANT, INTEGRAL FUEL TANKS AND FUEL CELL CAVITIES, HIGH-ADHESION (S/S BY SAE-AMS-S-8802) |
| 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 | Galvanic Compatibility of Electrically Conductive Materials |
| MIL-L-23398 Revision D:1985 | Lubricant, Solid Film, Air-Cured, Corrosion Inhibiting, NATO Code Number S-749 |
| MIL-C-46168 Revision D:1987 | Coating, Aliphatic Polyurethane, Chemical Agent Resistant (See Notice 1 for Replacement Information) |
| 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 Retreatment, Resin-Acid (ASG) |
| MIL C 22750 : F | COATING, EPOXY, VOC-COMPLIANT |
| MIL-C-8779 Revision E:1988 | Colors, 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 | Coating, 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 (S/S BY SAE-AMS3277, SEE NOTICE 1 FOR ADDITIONAL INFORMATION) |
| MIL-S-38249 Base Document:1964 | Sealing Compound, Firewall (S/S bySAE-AMS3374 andSAE-AMS3381) |
| 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 Lightning Protection, for Aerospace Systems (S/S by MIL-STD-464) |
| MIL L 46010 : D | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING |
| MIL-C-83286 Revision B:1973 | Coating, Urethane, Aliphatic Isocyanate, for Aerospace Applications (S/S by MIL-C-85285 S/S by MIL-PRF-85285) |
| VV-L-800 Revision C:1983 | Lubricating Oil, General Purpose, Preservative, (Water-Displacing, Low Temperature) (S/S by MIL-PRF-32033) |
| TT-P-2760 Revision A:1994 | Primer Coating: Polyurethane, Elastomeric, High-Solids |
| MIL-STD-171 Revision F:2011 | Finishing of Metal and Wood Surfaces |
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