MIL-I-85071 Revision A:1992
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
INVERTERS, AIRCRAFT, DC TO AC, GENERAL SPECIFICATION FOR
Available format(s)
PDF
Superseded date
14-10-2010
Superseded by
Publisher
Covers requirements for self-cooled inverters for converting electrical power form nominal 28 VDC to three-phase or single phase ac power at 400 Hertz.
| Committee |
FSC 6130
|
| DevelopmentNote |
A NOTICE 1 - Notice of Inactivation for New Design. A NOTICE 2 - Notice of Cancellation/Superseded by MIL PRF 7032. (10/2010)
|
| DocumentType |
Standard
|
| Pages |
47
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| MIL-STD-7080 Base Document:1994 | SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-D-8708 Revision C:1991 | DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
| MIL-STD-481 Revision B:1988 | CONFIGURATION CONTROL, ENGINEERING CHANGES, DEVIATIONS AND WAIVERS (SHORT FORM) |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MIL-STD-970 Base Document:1987 | STANDARDS AND SPECIFICATIONS, ORDER OF PREFERENCE FOR THE SELECTION OF |
| MIL-STD-130 Revision N:2007 | IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
| MIL C 39006/22 : E | CAPACITOR, FIXED, ELECTROLYTIC (NONSOLID ELECTROLYTE) TANTALUM (POLARIZED SINTERED SLUG), 85 DEG C (VOLTAGE DERATED TO 125 DEG C) ESTABLISHED RELIABILITY STYLE CLR79 |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-STD-2073-1 Revision E:2008 | STANDARD PRACTICE FOR MILITARY PACKAGING |
| MIL-I-46058 Revision C:1972 | Insulating Compound, Electrical (for Coating Printed Circuit Assemblies) |
| MIL C 39006/25 : A | CAPACITOR, FIXED, ELECTROLYTIC (NONSOLID ELECTROLYTE) TANTALUM (POLARIZED SINTERED SLUG) (EXTENDED RANGE) 85 DEG C (VOLTAGE DERATED TO 125 DEG C). ESTABLISHED RELIABILITY STYLE CLR81 |
| MIL-STD-2175 Revision A:1993 | CASTING, CLASSIFICATION AND INSPECTION OF |
| MIL P 15024 : E | PLATES, TAGS AND BANDS FOR IDENTIFICATION OF EQUIPMENT |
| MIL-STD-831 Base Document:1963 | TEST REPORTS, PREPARATION OF |
| MS3376 Revision B:1971 | NUT, SELF LOCKING, REDUCED HEIGHT, STEEL, 450 DEGREES F, 12 POINT, CAPTIVE WASHER |
| MIL-STD-1562 Revision W:1991 | LISTS OF STANDARD MICROCIRCUITS |
| MIL R 39015 : C (3) | RESISTOR, VARIABLE, WIRE WOUND (LEAD SCREW ACTUATED), ESTABLISHED RELIABILITY GENERAL SPECIFICATION FOR |
| MS90415 Revision C:1988 | NUT, SELF-LOCKING, STEEL, 160KSI, 450 DEG F, 12 POINT, CAPTIVE WASHER |
| MIL-STD-2000 Revision A:1991 | STANDARD REQUIREMENTS FOR SOLDERED ELECTRICAL AND ELECTRONIC ASSEMBLIES |
| MIL-HDBK-217 Revision F:1991 | RELIABILITY PREDICTION OF ELECTRONIC EQUIPMENT |
| MS33543 Revision A:1953 | CRITERIA TEMPERATURE AND ALTITUDE RANGE SELF COOLED ELECTRIC EQUIPMENT |
| MIL C 5541 : E | CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MIL-A-21180 Revision D:1984 | ALUMINUM-ALLOY CASTINGS, HIGH STRENGTH |
| MIL-STD-198 Revision E:1984 | CAPACITOR, SELECTION AND USE OF |
| MIL S 19500 : J | SEMICONDUCTOR DEVICES, GENERAL SPECIFICATION FOR |
| MIL-T-7928 Revision G:1976 | TERMINAL, LUG SPLICES, CONDUCTOR, CRIMP STYLE, COPPER, GENERAL SPECIFICATION FOR |
| MIL-P-116 Revision J:1988 | PRESERVATION, METHODS OF |
| MIL-STD-1629 Revision A:1980 | PROCEDURES FOR PERFORMING A FAILURE MODE, EFFECTS AND CRITICALITY ANALYSIS |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| FED-STD-595 Revision C:2008 | COLORS USED IN GOVERNMENT PROCUREMENT |
| MIL-STD-785 Revision B:1980 | RELIABILITY PROGRAM FOR SYSTEMS AND EQUIPMENT DEVELOPMENT AND PRODUCTION |
| MIL-E-81910 Revision A:1977 | ELECTRICAL POWER GENERATING AND CONTROL EQUIPMENT, AIRCRAFT, GENERAL SPECIFICATIONS FOR |
| MIL-S-7742 Revision D:1991 | SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR |
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