MIL A 25949 : E (2)
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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ACCELEROMETER, AIRCRAFT RANGE -5 TO PLUS 1OG UNITS, INTEGRALLY LIGHTED
Published date
12-01-2013
Publisher
Superseded date
01-05-1995
Superseded by
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Details the above.
| DocumentType |
Standard
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| MIL I 5949 : G | INSTRUMENTS, FLIGHT AND ENGINE, AIRCRAFT, FUNCTIONAL TESTS AND TOLERANCES OF |
| MIL-STD-130 Revision N:2007 | Identification Marking of U.S. Military Property |
| PPP-B-636 Revision J:1981 | Boxes, Shipping, Fiberboard (S/S by ASTM-D1974 and ASTM-D5118) |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MS33585 Revision B:1961 | POINTER, DIAL, STANDARD DESIGN OF AIRCRAFT INSTRUMENT (NO S/S DOCUMENT) |
| MIL-G-81704 Base Document:1969 | Glass, Aircraft Instrument, Lighting Wedge and Cover |
| MIL-STD-889 Revision C:2016 | Galvanic Compatibility of Electrically Conductive Materials |
| MIL-C-14806 Revision A:1969 | Coating, Reflection Reducing, for Instrument Cover Glasses and Lighting Wedges |
| MS33558 Revision C:1968 | Numeral and Letters, Aircraft Instrument Dial, Standard Form of |
| MS28105 Revision D:2006 | Cover Glass, Aircraft Instrument Dial |
| MIL-STD-831 Base Document:1963 | TEST REPORTS, PREPARATION OF |
| MIL-L-27160 Revision C:1972 | Lighting, Instrument, Integral, White, General Specification for |
| MIL-STD-143 Revision B:1969 | STANDARDS & SPECIFICATIONS, ORDER OF PRECEDENCE FOR THE SELECTION OF (S/S BY MIL-STD-970) |
| MIL P 26514 : F | POLYURETHANE FOAM, RIGID OR FLEXIBLE, FOR PACKAGING |
| MIL C 5541 : E | CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MIL-STD-100 Revision G:1997 | ENGINEERING DRAWINGS (S/S BY ASME-Y14.100, ASME-Y14.24, ASME-Y14.35M, AND ASME-14.34M) |
| MIL-P-116 Revision J:1988 | PRESERVATION, METHODS OF (S/S BY MIL-STD-2073-1) |
| 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) |
| 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 |
| MS23009 Revision E:1987 | Accelerometer-Aircraft, Integrally Lighted ABU-4A/A and ABU-4B/A |
| MIL L 6085 : C | LUBRICATING OIL, INSTRUMENT, AIRCRAFT, LOW VOLATILITY |
| MIL-S-7742 Revision D:1991 | Screw Threads, Standard, Optimum Selected Series: General Specification for |
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