MIL-B-5087 Revision B:1964
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS
Available format(s)
PDF
Superseded date
09-04-1997
Superseded by
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.NO CONTENTS SECTION
Gives the characteristics, application, and testing of electrical bonding for aerospace systems, and for the installation and interconnection of electrical and electronic equipment. Coverage includes classification, applicable documents, selection of materials, standard parts, hardware usage, bonding surface preparation, impedance, return path, coaxial antenna, current capacity, and voltage drop.
| DocumentType |
Standard
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| Pages |
35
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Superseded
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| SupersededBy |
| MIL-R-85895 Base Document:1988 | RACK, BOMB EJECTOR, AIRCRAFT BRU-32/A |
| MIL A 85670 : 0 | ANTENNA, BROADBAND AS-3191/A, AS-3792/A, AND AS -3793/A |
| AFGS-87213 Revision B:1993 | DISPLAYS, AIRBORNE, ELECTRONICALLY/OPTICALLY GENERATED |
| MIL-A-6271 Revision C:1976 | ANTENNA, SUBSYSTEM FOR VHF AIRBORNE COMMUNICATION EQUIPMENT GENERAL SPECIFICATION FOR |
| MIL-HDBK-253 Base Document:1978 | GUIDANCE FOR THE DESIGN AND TEST OF SYSTEMS PROTECTED AGAINST THE EFFECTS OF ELECTROMAGNETIC ENERGY |
| MIL-R-29583 Base Document:1992 | RADIO SET |
| MIL-M-8555 Revision C:1984 | MISSILE, GUIDED, DESIGN AND CONSTRUCTION, GENERAL SPECIFICATION |
| MIL A 87136 : NOTICE 1 | ANTENNAS, AIRBORNE GENERAL SPECIFICATION FOR |
| MIL-I-83152 Revision B:1974 | INDICATOR, INDICATED-AIRSPEED AVU-22/A (INDICATOR-TRANSDUCER) |
| MIL-L-6503 Revision H:1975 | LIGHTING EQUIPMENT, AIRCRAFT, GENERAL SPECIFICATION FOR INSTALLATION OF |
| MIL-A-85055 Base Document:1979 | Avionics System Performance Specification for A-4M/AV-8 Bombing Set, Angle Rate AN/ASB-19(V) |
| MIL-STD-7080 Base Document:1994 | SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
| MIL-G-25597 Revision D:1973 | Gyroscope, Displacement, Roll and Pitch, Type MD-1 |
| MIL A 85097/13 : NOTICE 1 | AIRCREW ESCAPE PROPULSION SYSTEMS (AEPS), ROCKET MOTOR, CANOPY JETTISON, MARK 109 MOD O LOADED ASSEMBLY |
| MIL-D-70789 Revision A:1992 | DYNAMIC REFERENCE UNIT (DRU) |
| SAE AIR 5128 : 2012 | ELECTRICAL BONDING OF AIRCRAFT FUEL SYSTEMS |
| MIL DTL 0085097/13 : B | AIRCREW ESCAPE PROPULSION SYSTEMS (AEPS) ROCKET MOTOR, CANOPY JETTISON, MARK 109 MOD 0 (LOADED ASSEMBLY) |
| MIL D 87213 : 0 | DISPLAYS/OPTICALLY GENERATED REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | 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 |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | 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)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| 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 |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-R-81876 Revision B:1988 | RECEIVER, TRANSMITTER RADIO SET AN/APX-100(V) |
| MIL-H-25475 Revision B:1971 | HYDRAULIC SYSTEM, MISSILE, DESIGN, INSTALLATION TESTS AND DATE REQUIREMENTS, GENERAL REQUIREMENTS FOR |
| DEFSTAN 00-69(PT2)/1(1998) : 1998 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM - PART 2: DESIGN PRINCIPLES AND PRACTICES FOR, AND GUIDE TO, THE IMPLEMENTATION OF THE AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
| MIL-H-8891 Revision A:1978 | HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR |
| MIL-HDBK-244 Revision A:1990 | GUIDE TO AIRCRAFT - STORES COMPATIBILITY |
| MIL R 23016 : A | RADIO SET AN/ARC-94 |
| MIL A 28875 : 0 | AMPLIFIER, RADIO FREQUENCY AND MICROWAVE, SOLID STATE, GENERAL SPECIFICATION FOR |
| MIL-STD-2156 Base Document:1983 | LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
| 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-W-8160 Revision D:1961 | WIRING, GUIDED MISSILE, INSTALLATION OF, GENERAL SPECIFICATION FOR |
| MIL-STD-877 Base Document:1968 | ANTENNA SUBSYSTEMS, AIRBORNE, CRITERIA FOR DESIGN AND LOCATION OF |
| MIL-I-85671 Base Document:1987 | INDICATOR, FREQUENCY CHANNEL ID-2121A/ARC, ID-2229A/ARC AND ID-2303/ARC |
| MIL-P-5994 Revision D:1972 | PUMP, HYDRAULIC, ELECTRIC MOTOR DRIVEN, VARIABLE DELIVERY, GENERAL SPECIFICATION FOR |
| MIL-T-63534 Base Document:1981 | TURRET SUBSYSTEM, UNIVERSAL, (UTS) FOR ARMAMENT SUBSYSTEM, HELICOPTER, 20MM, M97E1 AND M97E2, TURRET CONTROL UNIT FOR |
| MIL-STD-1541 Revision A:1987 | ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS FOR SPACE SYSTEMS |
| MIL P 52955 : A | POSITION & AZIMUTH DETERMINING SYSTEM (PADS), AN/USQ-70(U) |
| MIL-E-7080 Revision B:1962 | ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF |
| MIL-P-83927 Revision B:1981 | Power Supplies, Guided Missile Launchers, Single Types PP-2401B/A PP-2401C/A PP-2401D/A, PP-4285/A, PP-4286/A, and Composite Type PP-4506/A and PS-1037 |
| 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 SYSTEM |
| MIL C 15370 : F | COUPLERS, DIRECTIONAL GENERAL SPECIFICATION FOR |
| SAE AS8700 | Installation and Test of Electronic Equipment in Aircraft, General Specification for |
| SAE AS8181A | Detector, Ice, Air Intake Duct, Aircraft Engines and Airframe Systems, General Specification For |
| MIL-I-18802 Revision A:1962 | INSTALLATION OF FUEL AND OIL LINES, AIRCRAFT |
| SAE ARP4729A | Document for 270 Voltage Direct Current (270 V DC) System |
| MIL-HDBK-1760 Revision A:2004 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
| MIL-C-85518 Base Document:1984 | COMPUTER SET, STANDARD AIRBORNE AN/AYK-14(V) GENERAL SPECIFICATION FOR |
| SAE AS18802 | Fuel and Oil Lines, Aircraft, Installation of |
| MIL C 85629 : A (1) | CONTROL MONITOR SET GUIDED WEAPON, AN/AWW-13 |
| MIL-I-8673 Base Document:1955 | INSTALLATION AND TEST OF AIRCRAFT FLEXIBLE WEAPONS SYSTEMS |
| SAE AS4764A | Validation Methods for MIL-STD-1760 Aircraft Station Interfaces |
| MIL-R-7705 Revision B:1975 | RADOME, GENERAL SPECIFICATION FOR |
| MIL I 18373 : B | INSTRUMENT AND NAVIGATION EQUIPMENT, AIRCRAFT, INSTALLATION OF |
| NASA HDBK 4001 : 0 | ELECTRICAL GROUNDING ARCHITECTURE FOR UNMANNED SPACECRAFT |
| MIL-A-6224 Revision E:1976 | ANTENNA SUBSYSTEM FOR UHF AIRBORNE COMMUNICATIONS EQUIPMENT, GENERAL SPECIFICATION FOR |
| MIL-I-8700 Revision A:1970 | INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-P-87210 Base Document:1984 | PNEUMATIC POWER SYSTEMS, HIGH PRESSURE |
| SAE ARP1616B | Self-Sealing Breakaway Valves for Crash-Resistant Aircraft Fuel and Oil Systems |
| MIL-F-8615 Revision D:1976 | FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG] |
| MIL-HDBK-272 Revision A:1993 | NUCLEAR WEAPONS SYSTEMS, SAFETY DESIGN AND EVALUATION CRITERIA FOR |
| JSSG-2006 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
| NASA MSFC SPEC 250 : 1963 | PROTECTIVE FINISHES FOR SPACE VEHICLE STRUCTURES AND ASSOCIATED FLIGHT EQUIPMENT GENERAL SPECIFICATION FOR |
| MIL P 17842 : NOTICE 1 | POWER PLANT VIBRATION ISOLATOR, DESIGN AND INSTALLATION REQUIREMENTS |
| NASA MSFC HDBK 670 : 1991 | GENERAL ENVIRONMENTAL TEST GUIDELINES (GETG) FOR PROTOFLIGHT INSTRUMENTS AND EXPERIMENTS |
| MIL-T-63520 Base Document:1981 | TURRET SUBSYSTEM, UNIVERSAL (UTS) FOR ARMAMENT SUBSYSTEM, HELICOPTER, 20MM, M97E1 AND M97E2, GUN CONTROL ASSEMBLY FOR |
| MIL-N-49098 Revision A:1990 | NAVIGATIONAL SET, DOPPLER AN/ASN-128()(XE-2) |
| MIL-D-8181 Revision B:1965 | DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS GENERAL SPECIFICATION FOR |
| MIL-A-25730 Revision C:1976 | ANTENNA SUBSYSTEMS FOR AIRBORNE IDENTIFICATION AND NAVIGATION EQUIPMENT, GENERAL SPECIFICATION FOR |
| MIL-I-8671 Revision D:1994 | INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS |
| 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 |
| MIL-T-63536 Base Document:1981 | TURRET SUBSYSTEM, UNIVERSAL (UTS) FOR ARMAMENT SUBSYSTEM, HELICOPTER, 20MM, M97E1 AND M97E2, LOGIC CONTROL UNIT ASSEMBLY FOR |
| SAE AS4270A | Validation Methods for MIL-STD-1760 Mission Stores |
| SAE MA2241 | Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Metric |
| SAE AIR4728 | References, Spacecraft and Spacecraft Servicing, Fluid System Components (Abbreviations, Acronyms, Definitions, Applicable Documents and Environmental Conditions) |
| MIL-D-19326 Revision H:1990 | Design and Installation of Liquid Oxygen Systems in Aircraft, General Specification for |
| MIL-STD-1512 Base Document:1972 | ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHODS |
| DOD STD 1788 : LATEST | AVIONICS INTERFACE DESIGN STANDARD (METRIC) |
| MIL-I-85112 Base Document:1978 | INDICATOR SET, VERTICAL SCALE |
| MIL-H-23799 Base Document:1963 | HOSE ASSEMBLY, METAL, TRANSFER, LIQUID OXYGEN |
| MIL A 83366 : 0 | ANTENNA ASSEMBLIES, AIRBORNE, GENERAL SPECIFICATION FOR |
| MIL-I-83456 Base Document:1974 | INSTALLATION OF SEGMENTED LIGHTNING DIVERTER STRIPS ON AIRCRAFT RADOMES, GENERAL SPECIFICATION FOR |
| MIL-A-85505 Base Document:1983 | ALTIMETER, STANDBY, TYPES 1 AND 2 |
| MIL-L-85762 Revision A:1988 | LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION |
| MIL-A-83212 Revision A:1976 | ALTIMETER, PRESSURE AAU-27/A |
| MIL-A-85672 Base Document:1987 | AMPLIFIER, RADIO FREQUENCY AM-7177A/ARC |
| MIL-W-18326 Revision A:1956 | WELDING OF MAGNESIUM ALLOYS, GAS AND ARC, MANUAL AND MACHINE PROCESSES FOR |
| MIL-D-8708 Revision C:1991 | DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
| SAE AS47641A | Validation Methods for MIL-STD-1760B Aircraft Station Interfaces |
| MIL-C-87970 Base Document:1982 | CONTROL SET, GYROSCOPE, ATTITUDE HEADING AN/ASN-129 |
| MIL-E-6051 Revision D:1967 | ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM |
| MIL-STD-463 Revision A:1977 | DEFINITION AND SYSTEM OF UNITS, ELECTROMAGNETIC INTERFERENCE TECHNOLOGY |
| MIL-I-8672 Revision B:1969 | INSTALLATION AND TEST OF AIRCRAFT PYROTECHNIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR [ASG] |
| MIL-A-55368 Base Document:1972 | AIRBORNE DATA ANNOTATION SYSTEM AN/AYA-10() |
| MIL-C-81883 Base Document:1976 | CONTROL GROUP, ELECTRIC POWER OK-XXX (V) A GENERAL SPECIFICATION FOR |
| MIL-L-5667 Revision B:1964 | LIGHTING EQUIPMENT, AIRCRAFT INSTRUMENT PANEL, GENERAL SPECIFICATION FOR INSTALLATION OF [ASG] |
| MIL I 83361 : (4) | INDICATOR, PRESSURE OIL, DUAL EGU-18/A, 0-100 PSI |
| MIL-P-85576 Revision B:1987 | POWER SUPPLY PP-2581C/A |
| SAE AIR 5774 : 2012 | COMPOSITE FUEL TANKS, FUEL SYSTEM DESIGN CONSIDERATIONS |
| SAE AS5994A | Pump Units, Hydraulic, Electric Motor Driven, Variable Delivery |
| MS 35339 : LATEST | WASHER, LOCK, SPLIT, HELICAL, HEAVY SERIES |
| AN 960 : 0021 | WASHER, FLAT |
| AN742 Revision 13:2011 | CLAMP, LOOP, PLAIN, SUPPORT, AIRCRAFT |
| NAS680:1987 | NUT - SELF-LOCKING - PLATE - TWO LUG - LOW HEIGHT - C'BORE |
| AN 935 : LATEST | WASHER - LOCK, SPRING |
| MIL-STD-143 Revision B:1969 | STANDARDS, AND SPECIFICATIONS ORDER OF PRECEDENCE FOR THE SELECTION OF |
| MS25083 Revision K:1980 | JUMPER ASSEMBLY, ELECTRIC, BONDING AND CURRENT RETURN |
| NAS679:2010 | NUT, SELF-LOCKING, HEXAGON, LOW HEIGHT |
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