MIL-G-23081 Revision C:1972
Current
Current
The latest, up-to-date edition.
Gyroscope Indicator System, Vertical
Available format(s)
PDF
Published date
02-10-1972
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.Requirements for two,types of Vertical Gyroscope Indicator System.
| DocumentType |
Standard
|
| Pages |
68
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
The equipment covered by this specification is a Vertical Gyroscope Indicator System operated by 115/200 volt, 400 Hertz, 3-phase, 4-wire wye power supply.
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| MS17400 Revision B:1964 | INDICATOR ATTITUDE REMOTE - 3 INCH CASE |
| MIL-G-23083 Revision C:1972 | Gyroscope, Rate Switching MS 17399 |
| MS 17322 : LATEST | |
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| MS14114 Base Document:1975 | GYROSCOPE DISPLACEMENT ROLL AND PITCH (HARD MOUNTED) |
| MS24367 Revision C:1971 | LAMP, INCANDESCENT MINIATURE INTEGRAL LIGHTING |
| BB-N-411 Revision C:1973 | NITROGEN, TECHNICAL |
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| MIL-C-14806 Revision A:1969 | COATING, REFLECTION REDUCING, FOR INSTRUMENT COVER GLASSES AND LIGHTING WEDGES |
| MS17399 Revision C:1971 | Gyroscope, Rate Switching |
| MS33558 Revision C:1968 | NUMERAL AND LETTER, AIRCRAFT INSTRUMENT DIAL, STANDARD FORM OF |
| MS3106 Revision D:1992 | CONNECTOR, PLUG, ELECTRIC, STRAIGHT, SOLDER CONTACTS, AN TYPE |
| DD-G-451 Revision D:1977 | GLASS, FLOAT OR PLATE, SHEET, FIGURED (FLAT, FOR GLAZING, MIRRORS AND OTHER USES) |
| MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
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| MIL-STD-1334 Revision B:1977 | PROCESS FOR BARRIER COATING OF ANTI-FRICTION BEARINGS |
| MIL-T-5422 Revision F:1971 | TESTING, ENVIRONMENTAL, AIRCRAFT ELECTRONIC EQUIPMENT |
| MIL-STD-471 Revision A:1973 | MAINTAINABILITY DEMONSTRATION |
| MIL-T-18303 Revision B:1966 | TEST PROCEDURES, REPRODUCTION, ACCEPTANCE, AND LIFE FOR AIRCRAFT ELECTRONIC EQUIPMENT, FORMAT FOR |
| MIL C 5015 : G | CONNECTOR, ELECTRICAL, CIRCULAR THREADED AN TYPE, GENERAL SPECIFICATION FOR |
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| MIL-L-25467 Revision D:1977 | LIGHTING, INTEGRAL, RED, AIRCRAFT INSTRUMENT, GENERAL SPECIFICATION FOR |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| MIL G 81322 : E | GREASE, AIRCRAFT, GENERAL PURPOSE, SIDE TEMPERATURE RANGE, NATO CODE NUMBER G-395 |
| MIL-STD-785 Revision B:1980 | RELIABILITY PROGRAM FOR SYSTEMS AND EQUIPMENT DEVELOPMENT AND PRODUCTION |
| MIL-STD-781 Revision D:1986 | RELIABILITY TESTING FOR ENGINEERING DEVELOPMENT, QUALIFICATION AND PRODUCTION |
| MIL L 6085 : C | LUBRICATING OIL, INSTRUMENT, AIRCRAFT, LOW VOLATILITY |
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