MIL P 26517 : A
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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POWER SUPPLY, TRANSFORMER-RECTIFIER, AIRCRAFT, GENERAL SPECIFICATION FOR
16-06-2000
Details general requirements for power supplies converting a nominal 115/200V, 400 cps, a.c. aircraft electrical system to direct-current power.
| DevelopmentNote |
INACTIVE FOR NEW DESIGN
|
| DocumentType |
Standard
|
| Pages |
22
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MIL-STD-704 Revision F:2004 | Aircraft Electric Power Characteristics |
| MIL-STD-130 Revision N:2007 | Identification Marking of U.S. Military Property |
| MIL-M-3171 Revision C:1966 | Magnesium Alloy, Processes for Pretreatment and Prevention of Corrosion on (S/S by SAE-AMS-M-3171) |
| MIL-D-70327 Base Document:1959 | DRAWINGS, ENGINEERING AND ASSOCIATED LISTS |
| MIL-STD-143 Revision B:1969 | STANDARDS & SPECIFICATIONS, ORDER OF PRECEDENCE FOR THE SELECTION OF (S/S BY MIL-STD-970) |
| MS33543 Revision A:1953 | CRITERIA TEMPERATURE AND ALTITUDE RANGE SELF COOLED ELECTRIC EQUIPMENT (NO S/S DOCUMENT) |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MIL T 9107 : LATEST | TEST REPORTS, PREPARATION OF |
| MIL I 26600 : LATEST | INTERFERENCE CONTROL REQUIREMENTS, AERONAUTICAL EQUIPMENT |
| MIL-M-7969 Revision C:1965 | Motors, Alternating Current, 400-Cycle, 115/200-Volt System, Aircraft, General Specification for |
| QQ-P-416 Revision F:1991 | Plating, Cadmium (Electrodeposited) (S/Sby SAE-AMS-QQ-P-416) |
| MIL-S-7742 Revision D:1991 | Screw Threads, Standard, Optimum Selected Series: General Specification for |
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