MIL F 18264 : D
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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: ORGANIC, WEAPONS SYSTEM, APPLICATION AND CONTROL OF
Available format(s)
PDF
Publisher
Superseded date
29-06-2015
Superseded by
€15.75
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Describes application and control of organic finishing materials on weapons systems to achieve aerodynamically smooth, adherent, high quality exterior and interior finishes, with minimum of added weight to systems.
| Committee |
FSC 8010
|
| DevelopmentNote |
INACTIVE FOR NEW DESIGN 30/8/99
|
| DocumentType |
Standard
|
| Pages |
85
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| MIL-I-85889 Base Document:1988 | IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
| MIL STD 001303 : C | PAINTING OF NAVAL ORDNANCE EQUIPMENT |
| MIL-C-81907 Base Document:1972 | Coating System, Polyurethane, Aliphatic, Weather Resistant: Process for Application of (No S/S Document) |
| MIL-R-8236 Revision F:1995 | Reel, Shoulder Harness, Inertia Lock |
| MIL-C-8605 Revision B:1990 | Cap; Pressure Fuel Servicing |
| MIL S 81733 : C | SEALING AND COATING COMPOUND CORROSION INHIBITIVE |
| MIL-A-23121 Revision C:1970 | Aircrew Environmental, Escape and Survival Cockpit Capsule System General Specification for (No S/S Document) |
| 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) |
| MIL-R-85880 Base Document:1988 | ROCKET, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
| MIL-STD-2156 Base Document:1983 | Launcher, Rail, Guided Missile, Aircraft, General Design Criteria for |
| MIL-I-17563 Revision C:1992 | Impregnants for Cast of Powder Metal Components |
| 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-STD-1516 Revision B:1990 | Unified Code for Coating and Finishes for DOD Materiel (No S/S Document) |
| MIL-I-6869 Revision D:1971 | Impregnants for Aluminum Alloy and Magnesium Alloy Castings (S/S by MIL-I-17563) |
| MIL-STD-2131 Revision A:1991 | Launcher, Ejection, Guided Missile, Aircraft, General Design Criteria for |
| MIL-F-7179 Revision G:1993 | Finishes, Coatings, and Sealants for the Protection of Aerospace Weapons Systems (S/S by MIL-STD-7179) |
| MIL-DTL-85110 Revision B:1997 | Bar, Repeatable Release Holdback (RRHB), Aircraft Launching, General Requirement for |
| MIL-C-22751 Revision D:1971 | Coating System, Epoxy-Polyamide, Chemical and Solvent Resistant: Process for Application of (No S/S Document) |
| MIL-P-21960 Revision B:1967 | PAINTING AND MARKING, WAR HEADS, GUIDED MISSILE (NO S/S DOCUMENT) |
| MIL-STD-1303 Revision B:1975 | Painting of Naval Ordnance Equipment (No S/S Document) |
| MIL-R-7705 Revision B:1975 | RADOME, GENERAL SPECIFICATION FOR (NO S/S DOCUMENT) |
| MIL-C-8507 Revision D:1963 | Coating, Wash Primer (Pretreatment) for Metals, Application of (for Aeronautical Use) |
| MIL-DTL-19328 Revision F:1996 | Converter, Liquid Oxygen, 5 Liter, MB-5A |
| NASA MSFC SPEC 250 : 1963 | PROTECTIVE FINISHES FOR SPACE VEHICLE STRUCTURES AND ASSOCIATED FLIGHT EQUIPMENT GENERAL SPECIFICATION FOR |
| MIL-STD-7179 Revision A:2009 | Finishes, Coatings, and Sealants, for the Protection of Aerospace Weapons Systems and Support Equipment |
| MIL-STD-171 Revision F:2011 | Finishing of Metal and Wood Surfaces |
| MIL-P-83126 Revision A:1980 | PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
| MIL-W-5013 Revision L:1991 | Wheel and Brake Assemblies, Aircraft General Specification For |
| MIL-STD-2161 Revision C:2014 | Paint Schemes and Exterior Markings for U.S. Navy and Marine Corps Aircraft |
| JSSG-2010-12 Base Document:1998 | Crew Systems Deployable Aerodynamic Decelerator (DAD) Systems Handbook |
| MIL-PRF-81733 Revision D:1998 | Sealing and Coating Compound, Corrosion Inhibitive |
| NASA PRC 4002 : 2010 | PROCESS SPECIFICATION FOR THE APPLICATION OF THERMAL AND CORROSION CONTROL PAINTS AND COATINGS |
| MIL-C-18263 Revision F:1971 | Colors, Exterior, Naval Aircraft: Requirements for (S/S by MIL-STD-2161) |
| MIL-B-29511 Base Document:1988 | Buoy Interface Unit (BIU), J-3958/BRT-6 (No S/S Document) |
| MIL-DTL-13931 Revision J:1999 | Cannon: General Specification for |
| 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-C-8779 Revision E:1988 | Colors, Interior, Aircraft, Requirements for |
| MIL C 25666 : E (1) | CONVERTER, LIQUID OXYGEN, CAPACITANCE TYPE GAGING, GENERAL SPECIFICATION FOR |
| MIL-DTL-25666 Revision F:1995 | Converter, Liquid Oxygen, Capacitance Type Gauging, General Specification for |
| TT-T-266 Revision D:1976 | THINNER, DOPE AND LACQUER (CELLULOSE NITRATE) (S/S BY A-A-857) |
| TT-E-529 Revision G:1988 | ENAMEL, ALKYD, SEMIGLOSS, LOW VOC CONTENT (S/S BY A-A-2962) |
| MIL-P-6808 Revision C:1973 | PRIMER COATING, ZINC CHROMATE, PROCESS FOR APPLICATION OF (NO S/S DOCUMENT) |
| MIL-P-52192 Revision B:1971 | Primer Coating, Epoxy (S/S by MIL-P-53022, or MIL-P-53030) |
| MIL-D-5549 Revision B:1971 | Dope, Cellulose-Acetate-Butyrate Clear for Aircraft Use (No S/S Document) |
| MIL-C-18263 Revision F:1971 | Colors, Exterior, Naval Aircraft: Requirements for (S/S by MIL-STD-2161) |
| MIL-P-21563 Revision B:1962 | Paint System, Fluorescent, for Aircraft Application (No S/S Document) |
| MIL-W-5044 Revision C:1970 | WALKWAY COMPOUND, NONSLIP AND WALKWAY MATTING, NONSLIP (S/S BY A-A-59166 AND A-A-59124) |
| RR-S-366 Revision E:1973 | Sieve, Test (S/S ASTM-E11 and ASTM-E323) |
| MIL P 8585 : LATEST | PRIMER COATING, ZINC CHROMATE, LOW-MOISTURE SENSITIVITY |
| MIL-M-3171 Revision C:1966 | Magnesium Alloy, Processes for Pretreatment and Prevention of Corrosion on (S/S by SAE-AMS-M-3171) |
| MIL-C-22751 Revision D:1971 | Coating System, Epoxy-Polyamide, Chemical and Solvent Resistant: Process for Application of (No S/S Document) |
| MIL-R-7705 Revision B:1975 | RADOME, GENERAL SPECIFICATION FOR (NO S/S DOCUMENT) |
| 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 L 81352 : A | LACQUER, ACRYLIC (FOR NAVAL WEAPONS SYSTEMS) |
| MIL I 18464 : G NOTICE 1 | INSIGNIA AND MARKINGS FOR NAVAL WEAPONS SYSTEMS |
| MIL S 5002 : D | SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS SYSTEMS |
| MIL-L-19538 Revision C:1970 | Lacquer, Acrylic Nitrocellulose, Camouflage (for Aircraft Use) (S/S by MIL-L-81352) |
| MIL P 23377 : G | PRIMER COATING, EPOXY, HIGH SOLIDS |
| MIL-P-21600 Revision A:1962 | PAINT SYSTEM, FLUORESCENT, REMOVABLE, FOR AIRCRAFT APPLICATION (S/S BY SAE-AMS-P-21600) |
| TT-R-248 Revision B:1981 | REMOVER, PAINT AND LACQUER, SOLVENT TYPE |
| MIL P 21698 : A | PAINT, FLUORESCENT, FOR AIRCRAFT, PROCESS FOR APPLICATION OF |
| MIL-C-18187 Revision A:1965 | Costings, Protective; Application to Fabric Surfaces of Aircraft (No S/S DOCUMENT) |
| TT-N-97 Revision D:2007 | Naphtha; Aromatic |
| TT-T-548 Revision F:1991 | TOLUENE, TECHNICAL (S/S BY A-A-59107) |
| MIL-S-15847 Revision A:1953 | SPRAY GUN AND ACCESSORIES, PAINT AND DOPE, AIRCRAFT USE (NO S/S DOCUMENT) |
| 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-R-81294 Revision D:1990 | Remover, Paint, Epoxy, Polysulfide, and Polyurethane Systems |
| MIL C 22750 : F | COATING, EPOXY, VOC-COMPLIANT |
| MIL E 7729 : LATEST | |
| TT-E-776 Revision B:1960 | Ethylene Glycol Monobutyl Ether (for Use in Organic Coatings) (S/S by ASTM-D330) |
| TT-L-20 Revision A:1967 | LACQUER, CAMOUFLAGE (S/S BY A-A-3164) |
| MIL-T-19588 Revision A:1964 | TOLUENE-METHYL ISOBUTYL KETONE MIXTURE (NO S/S DOCUMENT) |
| MIL-C-8779 Revision E:1988 | Colors, Interior, Aircraft, Requirements for |
| MIL D 5550 : B | DOPE, CELLULOSE ACETATE BUTYRATE, PIGMENTED, CAMOUFLAGE |
| 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-C-38334 Revision A:1971 | Corrosion Removing Compound, Prepaint, for Aircraft Aluminum Surfaces (S/S by SAE-AMS1640) |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MIL E 5556 : LATEST | |
| TT-L-32 Revision A:1969 | Lacquer, Cellulose Nitrate, Gloss, for Aircraft use (S/S by A-A-3165) |
| MIL D 7850 : A | DOPE, CELLULOSE - ACETATE - BUTYRATE, FIRST COAT, FUNGICIDAL |
| P-C-444 Revision B:1983 | Cleaning Compound, Solvent Soluble, Grease Emulsifying |
| MIL-L-19537 Revision C:1965 | Lacquer: Acrylic-Nitrocellulose Gloss (for Aircraft use) (S/S by MIL-L-81352) |
| MIL-M-25047 Revision C:1968 | Markings and Exterior Finish Colors for Airplanes, Airplane Parts, and Missiles (Ballistic Missiles Excluded) (No S/S Document) |
| TT-I-735 Revision A:1963 | Isopropyl Alcohol |
| MIL-T-6095 Revision B:1969 | THINNER, CELLULOSE-NITRATE-DOPE, BLUSH RETARDING (NO S/S DOCUMENT) |
| MIL-W-5050 Revision A:1958 | Walkway, Coating and Matting, Nonslip, Aircraft, Application Of (ASG) |
| MIL D 5551 : B | DOPE, CELLULOSE ACETATE BUTYRATE, PIGMENTED, GLOSS |
| MIL-P-7962 Revision D:1980 | PRIMER COATING, CELLULOSE-NITRATE MODIFIED ALKYD TYPE, CORROSION-INHIBITING, FAST-DRYING (FOR SPRAY APPLICATION OVER PRETREATMENT COATING) (NO S/S DOCUMENT) |
| FED-STD-141 Revision D:2001 | Paint, Varnish, Lacquer and Related Materials: Methods of Inspection, Sampling and Testing |
| FED-STD-595 Revision C:2008 | Colors Used in Government Procurement (S/S By SAE-AMS-STD-595) |
| MIL S 7502 : C | SEALING COMPOUND, INTEGRAL FUEL TANKS & FUEL CELL CAVITIES, HIGH ADHESION, ACCELERATOR REQUIRED |
| MIL-F-7179 Revision G:1993 | Finishes, Coatings, and Sealants for the Protection of Aerospace Weapons Systems (S/S by MIL-STD-7179) |
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