MIL C 7115 : F
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
CONVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR
Available format(s)
PDF
Publisher
Superseded date
11-07-2012
Superseded by
€16.67
Excluding VAT
Specifies devices which convert power from 115/200 volt, 400 Hertz, 3-phase, (ac) aircraft electric system to 28 volt (dc) power.
| Committee |
FSC 6130
|
| DevelopmentNote |
Supersedes SAE AS 4361. (07/2011) Supersedes SAE AS 8023. (08/2011)
|
| DocumentType |
Standard
|
| Pages |
91
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| MIL-STD-7080 Base Document:1994 | Selection and 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)/7(2011) : 2011 | 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)/12(2014) : 2014 | 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 |
| AFGS-87219 Revision B:2012 | Electrical Power Systems, Aircraft |
| MS3370 Revision B:1991 | Converter, 100 Ampere Class C, Nonregulated Aircraft, Blast Cooled |
| MIL-E-7080 Revision B:1962 | Electric Equipment, Aircraft, Selection and Installation of (S/S by MIL-STD-7080) |
| MIL-C-7115-3 Revision B:1991 | Converter, Aircraft, 150 Ampere Type II, Blast Cooled, Class C |
| SAE ARP4729A | Document for 270 Voltage Direct Current (270 V DC) System |
| MS28126 Revision F:1991 | Converter, 200 Ampere Class A, Nonregulated Aircraft, Fan Cooled |
| DOD-STD-35-82 Revision A:1979 | AUTOMATED ENGINEERING DOCUMENT PREPARATION SYSTEM CONVERTERS AND INVERTERS (NO S/S DOCUMENT) |
| 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 (NO S/S DOCUMENT) |
| 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 | CASTINGS, CLASSIFICATION AND INSPECTION OF (S/S BY SAE-AMS-STD-2175) |
| MIL P 15024 : E | PLATES, TAGS AND BANDS FOR IDENTIFICATION OF EQUIPMENT |
| MS14151 Base Document:1973 | WASHER, FLAT, ROUND, CORROSION RESISTING STEEL (FOR ELECTRICAL APPLICATIONS) (S/S BY NASM14151) |
| MIL-STD-831 Base Document:1963 | TEST REPORTS, PREPARATION OF |
| MIL-STD-1562 Revision W:1991 | LISTS OF STANDARD MICROCIRCUITS (NO S/S DOCUMENT) |
| MIL R 39015 : C (3) | RESISTOR, VARIABLE, WIRE WOUND (LEAD SCREW ACTUATED), ESTABLISHED RELIABILITY GENERAL SPECIFICATION FOR |
| MIL-STD-2000 Revision A:1991 | STANDARD REQUIREMENTS FOR SOLDERED ELECTRICAL AND ELECTRONIC ASSEMBLIES (NO S/S DOCUMENT) |
| MIL-HDBK-217 Revision F:1991 | Reliability Prediction of Electronic Equipment |
| MS33543 Revision A:1953 | CRITERIA TEMPERATURE AND ALTITUDE RANGE SELF COOLED ELECTRIC EQUIPMENT (NO S/S DOCUMENT) |
| MS35650 Revision G:1985 | NUT, PLAIN, HEXAGON, MACHINE SCREW, UNF-2B (S/S BY NASM35650) |
| 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 (S/S by SAE-AMS-A-21180) |
| MIL-STD-198 Revision E:1984 | CAPACITORS, SELECTION AND USE OF (S/S BY MIL-HDBK-198) |
| MIL S 19500 : J | SEMICONDUCTOR DEVICES, GENERAL SPECIFICATION FOR |
| MIL-T-7928 Revision G:1976 | Terminals, Lug: Splices, Conductor: Crimp Style, Copper, General Specification for (S/S BY SAE-AS7928) |
| MIL-P-116 Revision J:1988 | PRESERVATION, METHODS OF (S/S BY MIL-STD-2073-1) |
| MIL-STD-1629 Revision A:1980 | PROCEDURES FOR PERFORMING A FAILURE MODE, EFFECTS AND CRITICALITY ANALYSIS (NO S/S DOCUMENT) |
| 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 (S/S By SAE-AMS-STD-595) |
| MIL-STD-785 Revision B:1980 | RELIABILITY PROGRAM FOR SYSTEMS AND EQUIPMENT DEVELOPMENT AND PRODUCTION |
| MS35338 Revision L:1994 | WASHER, LOCK-SPRING, HELICAL, REGULAR (MEDIUM) SERIES (S/S BY NASM35338) |
| 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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