MIL-W-5013 Revision L:1991
Current
Current
The latest, up-to-date edition.
Wheel and Brake Assemblies, Aircraft General Specification For
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Published date
31-10-1991
Publisher
€16.67
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Covers main and auxiliary wheel and brake assemblies for all types of military aircraft.
| DevelopmentNote |
INACTIVE FOR NEW DESIGN 30/8/99
|
| DocumentType |
Standard
|
| Pages |
72
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
This specification covers main and auxiliary wheel and brake assemblies for all types of military aircraft.
| MIL A 8862 : 0 | AIRPLANE STRENGTH AND RIGIDITY, LANDPLANE, LANDING AND GROUND HANDLING LOADS |
| SAE ARP5632 | Rotorcraft: Application of Existing Aircraft Designed Tires, Wheels and Brakes |
| 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)/7(2011) : 2011 | 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 |
| 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)/13(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 |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT7)SEC3/3(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 3: STRUCTURAL STRENGTH AND DESIGN FOR OPERATION ON SPECIFIED SURFACES |
| MIL B 8075 : D | BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
| MIL-HDBK-516 Revision C:2014 | Airworthiness Certification Criteria |
| MIL-STD-2073-1 Revision E:2008 | Standard Practice for Military Packaging |
| MIL-L-87139 Base Document:1979 | LANDING GEAR SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES. WRIGHT-PATTERSON AFB OH 45433-6503 |
| SAE AIR1934A | Use of Structural Carbon Heat Sink Brakes on Aircraft |
| RE.AERO 63001 : 1999 | QUALIFICATION CONDITIONS FOR WHEELS AND BRAKES FOR MILITARY AIRCRAFT |
| SAE AIR4012C | USAF Aircraft Wheels |
| MIL M 7700 : E | MANUALS AND ABBREVIATED CHECKLISTS, FLIGHT |
| DEFSTAN 00-970(PT7)SEC3/2(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 3: STRUCTURAL STRENGTH AND DESIGN FOR OPERATION ON SPECIFIED SURFACES |
| MIL PRF 7700 : F | MANUALS AND ABBREVIATED CHECKLISTS, FLIGHT |
| MIL-B-7874 Revision B:1982 | Bolt, Machine, 1200 Degrees F (S/S by NASM7874) |
| PPP-T-76 Revision C:1976 | Tape, Packaging, Paper (for Carton Sealing) (S/S by ASTM-D5486) |
| MIL B 8075 : D | BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
| MS27611 Revision G:2015 | Valve, Hydraulic Bleeder, Aircraft Wheel Brake |
| MIL-I-8500 Revision D:1980 | Interchangeability and Replaceability of Component Parts for Aerospace Vehicles |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MIL-STD-970 Base Document:1987 | STANDARDS AND SPECIFICATIONS, ORDER OF PREFERENCE FOR THE SELECTION OF (NO S/S DOCUMENT) |
| MS15795 Revision G:1986 | Washer, Flat-Metal, Round, General Purpose (S/S by NASM15795) |
| MIL-STD-130 Revision N:2007 | Identification Marking of U.S. Military Property |
| MIL-A-8863 Revision C:1993 | Airplane Strength and Rigidity Ground Loads for Navy Acquired Airplanes |
| MIL-R-8791-1 Base Document:1989 | RETAINER, PACKING, HYDRAULIC AND PNEUMATIC, POLYTETRAFLUOROETHYLENE RESIN, (SINGLE TURN) (S/S BY SAE-AS8791/1) |
| PPP-B-636 Revision J:1981 | Boxes, Shipping, Fiberboard (S/S by ASTM-D1974 and ASTM-D5118) |
| AN 960 : 0021 | WASHER, FLAT |
| MIL-C-81907 Base Document:1972 | Coating System, Polyurethane, Aliphatic, Weather Resistant: Process for Application of (No S/S Document) |
| MS20002 Revision E:1972 | WASHER, COUNTERSUNK AND PLAIN, HIGH STRENGTH (S/S BY NASM20002) |
| MIL C 25427 : A | COUPLING ASSEMBLY, HYDRAULIC, SELF-SEALING, QUICK DISCONNECT |
| ASTM D 1141 : 1998 : EDT 1 | Standard Practice for the Preparation of Substitute Ocean Water |
| MIL V 19068 : A | VALVE, SHUTTLE, HYDRAULIC, AIRCRAFT, TYPE 11 SYSTEMS |
| MIL-STD-2073-1 Revision E:2008 | Standard Practice for Military Packaging |
| MIL-H-6875 Revision H:1989 | Heat Treatment of Steel, Process for (S/S by SAE-AMS-H-6875) |
| MIL-A-22771 Revision D:1984 | Aluminum Alloy Forgings, Heat Treated (S/S by SAE-AMS-A-22771) |
| MS14157 Revision B:1978 | BOLT, WHEEL, TENSION, FLANGED STEEL, 180KSI FTU, 450 DEG. F EXTERNAL SPLINE DRIVE (S/S BY NASM14157) |
| MIL-B-8584 Revision C:1970 | Brake Systems, Wheel, Aircraft, Design of |
| 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 F 18264 : D | FINISHES: ORGANIC, WEAPONS SYSTEM, APPLICATION AND CONTROL OF |
| MIL L 81352 : A | LACQUER, ACRYLIC (FOR NAVAL WEAPONS SYSTEMS) |
| MIL S 5002 : D | SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS SYSTEMS |
| ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
| MIL P 23377 : G | PRIMER COATING, EPOXY, HIGH SOLIDS |
| MIL-T-9046 Revision J:1983 | TITANIUM AND TITANIUM ALLOY, SHEET, STRIP AND PLATE (S/S BY SAE-AMS-T-9046) |
| MIL-STD-2175 Revision A:1993 | CASTINGS, CLASSIFICATION AND INSPECTION OF (S/S BY SAE-AMS-STD-2175) |
| MIL-HDBK-275 Revision A:1976 | Guide for Selection of Lubricants, Fluids, and Compounds for Use in Flight Vehicles and Components |
| MIL STD 470 : B | MAINTAINABILITY PROGRAM REQUIREMENTS (FOR SYSTEMS AND EQUIPMENTS) |
| MIL-STD-889 Revision C:2016 | Galvanic Compatibility of Electrically Conductive Materials |
| MIL B 121 : F | BARRIER MATERIAL, GREASEPROOFED, WATERPROOFED, FLEXIBLE |
| PPP-T-60 Revision E:1986 | Tape: Packaging, Waterproof (S/S by ASTM D5486/ASTM-D5486M) |
| MIL-STD-6866 Base Document:1985 | Inspection, Liquid Penetrant (S/S by ASTM-E1417) |
| QQ-C-320 Revision B:1974 | CHROMIUM PLATING (ELECTRODEPOSITED) (S/S BY SAE-AMS-QQ-C-320) |
| MIL-F-7190 Revision B:1985 | Forging, Steel, for Aircraft/Aerospace Equipment and Special Ordinance Applications (S/S by SAE-AMS-F-7190) |
| MIL-STD-838 Revision C:1983 | LUBRICATION OF MILITARY EQUIPMENT |
| MIL-T-10727 Revision C:1989 | TIN PLATING: ELECTRODEPOSITED OR HOT-DIPPED, FOR FERROUS AND NONFERROUS METALS (S/S BY ASTM-B545, ASTM-B339) |
| MIL-STD-2154 Base Document:1982 | Inspection, Ultrasonic, Wrought Metals, Process for (S/S by ASTM-E2375 and SAE-AMS-STD-2154) |
| MIL I 6870 : E | INSPECTION PROGRAM REQUIREMENTS NONDESTRUCTIVE FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS |
| MIL-B-6812 Revision E:1994 | Bolts, Aircraft (S/S by NASM6812) |
| QQ-A-596 Revision E:1981 | Aluminum Alloy Permanent and Semipermanent Mold Castings (S/S by ASTM-B108) |
| MIL-G-5514 Revision G:1993 | Gland Design; Packings, Hydraulic, General Requirements for |
| SAE AS666D | Cavity Design and O-Ring Selection for Static Seal Use in Aircraft Tubeless Tire Wheels |
| MS14177 Revision B:1991 | WASHER, RECESSED, COUNTERSUNK TWO SURFACES, FOR USE WITH WHEEL BOLTS AND NUTS UP TO AND INCLUDING 220 KSI FTU (S/S BY NASM14177) |
| MIL-STD-882 Revision E:2012 | System Safety |
| MIL-B-7838 Revision C:1989 | Bolt, Internal Wrenching, 160 KSI FTU (S/S by NASM7838) |
| MS27436 Revision B:1985 | Valve Special, Aircraft Wheel |
| MIL C 5541 : E | CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS |
| MIL-S-8879 Revision C:1991 | Screw Threads, Controlled Radius Root withIncreased Minor Diameter, General Specification for (S/S by SAE-AS8879) |
| MIL T 5041 : J | TIRE, PNEUMATIC, AIRCRAFT |
| MIL-A-8868 Revision B:1987 | Airplane Strength and Rigidity Data and Reports (No S/S Document) |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MIL-H-8775 Revision D:1976 | Hydraulic System Components, Aircraft and Missiles General Specification for (S/S by SAE-AS8775) |
| MIL-A-21180 Revision D:1984 | Aluminum-Alloy Castings, High Strength (S/S by SAE-AMS-A-21180) |
| MS14155 Base Document:1974 | WASHER, RECESSED COUNTERSUNK TWO SURFACES, FOR USE WITH WHEEL BOLTS AND NUTS UP TO AND INCLUDING 180 KSI FTU (S/S BY NASM14155) |
| TT-P-28 Revision H:2007 | Coating, Heat Resisting |
| MIL-P-116 Revision J:1988 | PRESERVATION, METHODS OF (S/S BY MIL-STD-2073-1) |
| MIL-STD-1472 Revision G:2012 | Human Engineering |
| QQ-A-601 Revision F:1981 | Aluminum Alloy Sand Castings (S/S by ASTM-B26/B26M) |
| MIL-T-18303 Revision B:1966 | Test Procedures; Preproduction, Acceptance, and Life for Aircraft Electronic Equipment, Format for |
| MIL-H-5440 Revision H:1993 | Hydraulic Systems, Aircraft, Design and Installation Requirements for (S/S by SAE-AS5440) |
| MIL-P-81985 Base Document:1974 | Peening of Metals |
| QQ-P-416 Revision F:1991 | Plating, Cadmium (Electrodeposited) (S/Sby SAE-AMS-QQ-P-416) |
| MIL G 83016 : NOTICE 1 | GAGE, AIRCRAFT WHEEL, INTEGRAL, TIRE PRESSURE INDICATING |
| MIL-P-83461 Revision B:1980 | PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT, IMPROVED PERFORMANCE AT 275 DEG. F (135 DEG. C) (S/S BY SAE-AMS-P-83461) |
| MIL-C-8837 Revision B:1983 | Coating, Cadmium (Vacuum Deposited) (S/S by SAE-AMS-C-8837) |
| MS14156 Base Document:1974 | NUT, WHEEL, SELF-LOCKING, FLANGED, STEEL, 180 KSI FTU, 450 DEG. F, SPLINE DRIVE (S/S BY NASM14156) |
| MIL-T-5544 Revision C:1991 | THREAD COMPOUND, ANTISEIZE, GRAPHITE-PETROLATUM (S/S BY SAE-AMS2518) |
| MIL-B-8831 Revision B:1982 | Bolt, 180 KSI FTU and 180 KSI FSU, 450 Degrees F Protruding and Flush Head, General Specification for (S/S by NASM8831) |
| MIL-G-4343 Revision C:1978 | Grease, Pneumatic System (S/S by SAE-AMS-G-4343) |
| MIL G 81322 : E | GREASE, AIRCRAFT, GENERAL PURPOSE, SIDE TEMPERATURE RANGE, NATO CODE NUMBER G-395 |
| MIL-STD-105 Revision E:1989 | Sampling Procedures and Tables for Inspection by Attributes (See Notice 3 for Replacement Information) |
| 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) |
| MIL-F-3541 Revision C:1989 | Fittings, Lubrication, General Specification for (S/S by SAE-AS35411) |
| FED-STD-595 Revision C:2008 | Colors Used in Government Procurement (S/S By SAE-AMS-STD-595) |
| MIL-STD-785 Revision B:1980 | RELIABILITY PROGRAM FOR SYSTEMS AND EQUIPMENT DEVELOPMENT AND PRODUCTION |
| PPP-C-843 Revision D:1977 | CUSHIONING MATERIAL, CELLULOSIC (S/S BY A-A-1898) |
| MIL-F-83142 Revision A:1969 | Forging, Titanium Alloys, Premium Quality (See Notice 5 for Replacement Information) |
| MIL-F-7179 Revision G:1993 | Finishes, Coatings, and Sealants for the Protection of Aerospace Weapons Systems (S/S by MIL-STD-7179) |
| MIL-A-8860 Revision B:1987 | Airplane Strength and Rigidity, General Specification for |
| MIL-P-81958 Base Document:1974 | Pressure Relief Devices, Overpressurization Prevention, Wheel/Tire, Aircraft |
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