MIL R 6106 : J
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
RELAYS, ELECTROMAGNETIC [INCLUDING ESTABLISHED RELIABILITY [ER] TYPES
Available format(s)
PDF
Superseded date
01-12-1997
Superseded by
Language(s)
English
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.| Committee |
FSC 5945
|
| DocumentType |
Standard
|
| Pages |
98
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| MIL-STD-7080 Base Document:1994 | SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
| MIL B 83424 : 0 | BATTERY SYSTEMS, SEALED CELL, NICKEL CADMIUM, INTEGRAL CHARGE CONTROL, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-HDBK-217 Revision F:1991 | RELIABILITY PREDICTION OF ELECTRONIC EQUIPMENT |
| MIL-A-19736 Revision A:1960 | AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR |
| MIL R 6106/26 : D | RELAY, ELECTROMAGNETIC, 50 AMPERES, SPST NC WITH 5 AMPERE SPDT AUXILIARY HERMETICALLY SEALED |
| MIL-E-7080 Revision B:1962 | ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF |
| DOD-STD-35-8 Revision B:1979 | AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM RELAYS |
| MIL-H-11511 Revision G:1980 | HEATER, SPACE, MULTIFUEL, WITH BLOWER 60,000 BTU/HR |
| MIL B 8075 : D | BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
| MIL-S-8812 Revision D:1975 | STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR |
| 06/30157712 DC : 0 | PREN 2593-001 - AEROSPACE SERIES - BASES FOR 10 A ELECTROMAGNETIC PLUG-IN RELAYS, TWO AND FOUR POLES DOUBLE THROW - PART 001: TECHNICAL SPECIFICATION |
| MIL E 917 : E | ELECTRIC POWER EQUIPMENT, BASIC REQUIREMENTS (NAVAL SHIPBOARD USE) |
| SAE ARP4729A | Document for 270 Voltage Direct Current (270 V DC) System |
| MIL-STD-1547 Revision B:1992 | ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE VEHICLES |
| MS27401 Revision X:1994 | RELAY, ELECTROMAGNETIC, TYPE I (INCLUDING ESTABLISHED RELIABILITY (ER) TYPES) PERMANENT MAGNET DRIVE, 10 AMPERE, 2 PDT, HERMETICALLY SEALED |
| MIL PRF 12883/51 : A | SOCKETS AND ACCESSORIES FOR PLUG-IN ELECTRONIC COMPONENTS, BRACKET AND SOCKET ASSEMBLY FOR RELAYS, 4-POLE, 10 AMPERES |
| MIL-R-24358 Base Document:1968 | RESTORATION SHIPBOARD ELECTRONIC EQUIPMENT F, 1N AND 2N COGNIZANCE |
| MIL R 6106/48 : A | RELAYS, ELECTROMAGNETIC, TYPE I, HERMETICALLY SEALED, 100 AMPERES, SPST (N.O.) WITH SPDT (FORM Z) 5 AMPERES AUXILIARY CONTACTS |
| MIL-R-28894 Base Document:1986 | RELAY, HYBRID OR SOLID STATE, SENSORS, ESTABLISHED RELIABILITY GENERAL SPECIFICATION FOR |
| MIL-M-28787-133 Revision B:1979 | MODULE, STANDARD ELECTRONIC RELAY, 4PDT, ANALOG KEY CODE NRN |
| MIL R 83055 : 0 | RAIN REPELLENT DISPENSING SYSTEMS, AIRCRAFT WINDSHIELD, GENERAL SPECIFICATION FOR |
| DIN 65167:1988-12 | AEROSPACE; PLUG-IN RELAYS; DC 28 V, TWO- AND FOUR-POLE, 5 AMP, POLARIZED, MONOSTABLE |
| MIL-G-83380 Base Document:1979 | GENERATOR SET, GAS TURBINE ENGINE DRIVEN, 30 AND 60 KW, 400 HZ |
| MIL P 81305 : A | POWER, DISTRIBUTION PANEL, ALTERNATING CURRENT, F-4 AIRCRAFT, SPECIFICATION FOR |
| MIL-F-23447 Base Document:1962 | FIRE WARNING SYSTEMS, AIRCRAFT, RADIATION SENSING TYPE, TEST AND INSTALLATION OF |
| MIL-STD-1346 Revision C:1994 | RELAY, SELECTION AND APPLICATION |
| DIN 65168:1988-12 | AEROSPACE; PLUG-IN RELAYS; DC 28 V, ONE- AND THREE-POLE, 10 AMP, POLARIZED, MONOSTABLE |
| MIL-S-21277 Revision A:1958 | SWITCH, LIQUID LEVEL, GENERAL SPECIFICATION FOR |
| MIL-P-11268 Revision L:1983 | PART, MATERIALS, AND PROCESSES USED IN ELECTRONIC EQUIPMENT |
| MIL-I-8672 Revision B:1969 | INSTALLATION AND TEST OF AIRCRAFT PYROTECHNIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR [ASG] |
| DOD-C-85050 Base Document:1982 | CHARGERS, BATTERY, NICKEL-CADMIUM, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-P-85576 Revision B:1987 | POWER SUPPLY PP-2581C/A |
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