MIL-I-5482 Revision C:1960
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
Indicator, Pressure, Synchro, Aircraft, 165 Degree Scale (No S/S Document)
01-02-1960
24-09-1999
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. NOTES
Outlines fifteen 2-inch, hermetically sealed, clamp mounted, single and dual 165-degree scale indicators.
| DevelopmentNote |
C NOTICE 1 - Notice of Cancellation without replacement. (04/2004)
|
| DocumentType |
Standard
|
| Pages |
21
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
This specification covers fifteen 2-inch, hermetically sealed, clamp mounted, single and dual 165-degree scale, synchro type, aircraft pressure indicators.
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| FED-STD-1 Revision A:1972 | Standard for Laboratory Atmospheric Conditions for Testing (S/S by ASTM-E171) |
| MS33585 Revision B:1961 | POINTER, DIAL, STANDARD DESIGN OF AIRCRAFT INSTRUMENT (NO S/S DOCUMENT) |
| MIL-T-5483 Revision D:1964 | Transmitter, Pressure, Synchro, Aircraft, 165 Degree Movement (No S/S Document) |
| MIL-D-70327 Base Document:1959 | DRAWINGS, ENGINEERING AND ASSOCIATED LISTS |
| MS33678 Revision A:2004 | Connector, Receptacle, Electric, Integral Mounting |
| MIL E 5400 : T | ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR |
| MS33558 Revision C:1968 | Numeral and Letters, Aircraft Instrument Dial, Standard Form of |
| QQ-C-320 Revision B:1974 | CHROMIUM PLATING (ELECTRODEPOSITED) (S/S BY SAE-AMS-QQ-C-320) |
| DD-G-451 Revision D:1977 | Glass, Float or Plate, Sheet, Figured (Flat, for Glazing, Mirrors and Other Uses) |
| MS25470 Revision A:1962 | Indicator, Pressure, Synchro, Aircraft, 165-Degree Scale |
| MIL P 7936 : LATEST | PARTS AND EQUIPMENT, AERONAUTICAL, PREPARATION FOR DELIVERY |
| MIL C 5541 : E | CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MS33639 Revision D:1988 | Cases, Instrument, Clamp - Mounted, Aircraft |
| MIL-P-116 Revision J:1988 | PRESERVATION, METHODS OF (S/S BY MIL-STD-2073-1) |
| MIL T 5350 : E | TRANSMITTER, SYNCHRO OPERATED, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL C 26482 : G | CONNECTOR, ELECTRICAL (CIRCULAR, MINIATURE, QUICK DISCONNECT, ENVIRONMENT RESISTING) RECEPTACLES AND PLUGS, GENERAL SPECIFICATION FOR |
| QQ-P-416 Revision F:1991 | Plating, Cadmium (Electrodeposited) (S/Sby SAE-AMS-QQ-P-416) |
| MIL-L-25467 Revision D:1977 | Lighting, Integral, Red, Aircraft Instrument, General Specification for |
| FED-STD-595 Revision C:2008 | Colors Used in Government Procurement (S/S By SAE-AMS-STD-595) |
| QQ-N-290 Revision A:1971 | NICKEL PLATING (ELECTRODEPOSITED) (S/S BY SAE-AMS-QQ-N-290) |
| MIL-S-7742 Revision D:1991 | Screw Threads, Standard, Optimum Selected Series: General Specification for |
| MS3112 Revision H:2007 | Connectors, Receptacle, Electrical, Box Mounting, Flange, Bayonet Coupling, Solder Contact, Series 1 |
| MS28055 Revision B:2007 | Flanges, Mounting, Attachable, Aircraft Instrument |
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