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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Bonding, Electrical, and Lightning Protection, for Aerospace Systems (S/S by MIL-STD-464)
Available format(s)
PDF
Published date
15-10-1964
Publisher
Superseded date
09-04-1997
Superseded by
€16.67
Excluding VAT
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
|
| Pages |
37
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
This specification covers the characteristics, application, and testing of electrical bonding (see 6.2.2) for aerospace systems, as well as bonding for the installation and interconnection of electrical and electrod equipment therein, and lightning protection.
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| MIL-H-8891 Revision A:1978 | Hydraulic Systems, Manned Flight Vehicles, Type III 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, Design and Installation Requirements for (S/S by SAE-AS5440) |
| MIL-A-19736 Revision A:1960 | Air Refueling Systems, General Specification for |
| MIL-W-8160 Revision D:1961 | WIRING, GUIDED MISSILE, INSTALLATION OF, GENERAL SPECIFICATION FOR (S/S BY MIL-W-5088) |
| MIL-STD-877 Base Document:1968 | ANTENNA SUBSYSTEM, AIRBORNE, CRITERIA FOR DESIGN AND LOCATION OF (NO S/S DOCUMENT) |
| 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 Units, Hydraulic, Electric Motor Driven, Variable Delivery, General Specification for (No S/S Document) |
| 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 (Future Acquisitions may Refer to: SMC-S-008, AIAA-S-121, and MIL-STD-464) |
| 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 (S/S by MIL-STD-7080) |
| 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 Systems (S/S by MIL-STD-7179) |
| 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 (S/S by SAE-AS18802) |
| SAE ARP4729A | Document for 270 Voltage Direct Current (270 V DC) System |
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| 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 (No S/S Document) |
| SAE AS4764A | Validation Methods for MIL-STD-1760 Aircraft Station Interfaces |
| MIL-R-7705 Revision B:1975 | RADOME, GENERAL SPECIFICATION FOR (NO S/S DOCUMENT) |
| 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 Systems for UHF Airborne Communications Equipment, General Specification for Design of (No S/S Document) |
| MIL-I-8700 Revision A:1970 | Installation and Test of Electronic Equipment in Aircraft, General Specification for (S/S by SAE-AS8700) |
| MIL-P-87210 Base Document:1984 | Pneumatic Power Systems, High Pressure (No S/S Document) |
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| MIL-F-8615 Revision D:1976 | Fuel System Components, General Specification for (S/S by SAE-ARP8615) |
| MIL-HDBK-272 Revision A:1993 | Nuclear Weapons Systems, Safety Design and Evaluation Criteria for |
| JSSG-2006 Base Document:1998 | Aircraft Structures |
| NASA MSFC SPEC 250 : 1963 | PROTECTIVE FINISHES FOR SPACE VEHICLE STRUCTURES AND ASSOCIATED FLIGHT EQUIPMENT GENERAL SPECIFICATION FOR |
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| NASA MSFC HDBK 670 : 1991 | GENERAL ENVIRONMENTAL TEST GUIDELINES (GETG) FOR PROTOFLIGHT INSTRUMENTS AND EXPERIMENTS |
| MIL-T-63520 Base Document:1981 | Turret Subsystems, Universal (UTS) for Armament Subsystems, Helicopter, 20MM, M97E1 and M97E2, Gun Control Assembly for |
| MIL-N-49098 Revision A:1990 | NAVIGATIONAL SET, DOPPLER AN/ASN-128( ) (XE-2) (NO S/S DOCUMENT) |
| MIL-D-8181 Revision B:1965 | Detector, Ice, Air Intake Duct, Aircraft Engines and Airframe Systems, General Specification for (S/S by SAE-AS8181) |
| MIL-A-25730 Revision C:1976 | Antenna Subsystems for Airborne Identification and Navigation Equipments, General Specification for (No S/S Document) |
| 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 | Targets, Aerial, Powered, Design and Construction of General Specification for (No S/S Document) |
| 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 |
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| MIL-I-85112 Base Document:1978 | Indicator Set, Vertical Scale |
| MIL-H-23799 Base Document:1963 | Hose Assembly, Metal, Transfer, Liquid Oxygen (No S/S Document) |
| 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 (No S/S Document) |
| 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 (No S/S Document) |
| 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 (S/S BY MIL-STD-2219) |
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| 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 (No S/S Document) |
| MIL-E-6051 Revision D:1967 | Electromagnetic Compatibility Requirements, Systems (S/S by MIL-STD-464) |
| MIL-STD-463 Revision A:1977 | DEFINITIONS AND SYSTEM OF UNITS, ELECTROMAGNETIC INTERFERENCE AND ELECTROMAGNETIC COMPATIBILITY TECHNOLOGY (S/S BY IEEE-C63.14) |
| MIL-I-8672 Revision B:1969 | Installation and Test of Aircraft Pyrotechnic Equipment in Aircraft, General Specification for (No S/S Document) |
| MIL-A-55368 Base Document:1972 | Airborne Data Annotation System AN/AYA-10( ) (No S/S Document) |
| MIL-C-81883 Base Document:1976 | Control Group, Electric Power OK-XXX (V)/A, General Specification for (No S/S Document) |
| MIL-L-5667 Revision B:1964 | Lighting Equipment, Aircraft Instrument Panel, General Specification for Installation of (No S/S Document) |
| 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 AS5994A | Pump Units, Hydraulic, Electric Motor Driven, Variable Delivery |
| AIAA S 122 : 2007 | ELECTRICAL POWER SYSTEMS FOR UNMANNED SPACECRAFT |
| MS 35339 : LATEST | WASHER, LOCK, SPLIT, HELICAL, HEAVY SERIES |
| AN 960 : 0021 | WASHER, FLAT |
| AN742 Revision 13:2011 | Clamp, Loop, Plain, Support, Aircraft |
| AN 935 : LATEST | WASHER - LOCK, SPRING |
| MIL-STD-143 Revision B:1969 | STANDARDS & SPECIFICATIONS, ORDER OF PRECEDENCE FOR THE SELECTION OF (S/S BY MIL-STD-970) |
| MS25083 Revision K:1980 | JUMPER ASSEMBLY, ELECTRIC, BONDING AND CURRENT RETURN (S/S BY MIL-C-83413/8) |
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