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MIL-DTL-26517 Revision B:2000

Current
Current

The latest, up-to-date edition.

POWER SUPPLY, TRANSFORMER-RECTIFIER, AIRCRAFT GENERAL SPECIFICATION FOR
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PACKAGING
6. NOTES

Gives general requirements for power supplies that convert power from a nominal 115/200 V, 400 Hz, alternating current (AC) aircraft electrical system to direct-current power.

Committee
FSC 6130
DevelopmentNote
Supersedes MIL P 26517 (A) Inactive for New Design (06/2004) B NOTICE 1 - Notice of Validation but remains Inactive for New Design. (09/2014)
DocumentType
Standard
Pages
18
PublisherName
US Military Specs/Standards/Handbooks
Status
Current
Supersedes

MIL-STD-704 Revision F:2004 AIRCRAFT ELECTRIC POWER CHARACTERISTICS
MIL-STD-130 Revision N:2007 IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
MIL-STD-889 Revision C:2016 DISSIMILAR METALS
MIL-STD-461 Revision G:2015 REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
MIL A 8625 : F ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS
DOD-D-1000 Revision B:1977 DRAWINGS, ENGINEERING AND ASSOCIATED LISTS
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)
SAE AMS M 3171 : 1998 MAGNESIUM ALLOY, PROCESSES FOR PRETREATMENT AND PREVENTION OF CORROSION ON
MIL-S-7742 Revision D:1991 SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR

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