MS33543 Revision A:1953
Withdrawn
Withdrawn
CRITERIA TEMPERATURE AND ALTITUDE RANGE SELF COOLED ELECTRIC EQUIPMENT (NO S/S DOCUMENT)
Available format(s)
PDF
Published date
11-27-1953
Publisher
Withdrawn date
08-06-1997
US$20.00
Excluding Tax where applicable
| DocumentType |
Standard
|
| Pages |
2
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
| MIL-M-8609 Revision B:1965 | Motor, DC, 28 Volt System, Aircraft, General Specification for |
| MIL-P-9388 Revision B:1986 | Pump, Pressure, Oil Free Air Type MA-2 (No S/S Document) |
| MIL-I-85071 Revision A:1992 | Inverters, Aircraft, DC to AC, General Specification for (S/S by MIL-PRF-7032) |
| MIL P 26517 : A | POWER SUPPLY, TRANSFORMER-RECTIFIER, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-I-27273 Revision A:1965 | Inverter, Power, Static, General Specification for |
| MIL R 26895 : 0 | RELAY, FIELD CONTROL, GENERATOR 28 VOLT DC, TYPE MD AND 1 |
| MIL-E-81910 Revision A:1977 | Electrical Power Generating and Control Equipment, Aircraft, General Specifications for |
| MIL-R-23761 Revision B:1975 | Regulators, Voltage, and Control Panels Aircraft, Direct Current Generator, General Specification for |
| MIL-P-9389 Revision A:1987 | PUMP, PRESSURE, OIL FREE AIR TYPE MA-3 (NO S/S DOCUMENT) |
| MIL-B-23072 Base Document:1961 | Blower, Anti-Exposure Suit Ventilation, General Specification for(No S/S Document) |
| MIL-M-7969 Revision C:1965 | Motors, Alternating Current, 400-Cycle, 115/200-Volt System, Aircraft, General Specification for |
| MIL G 21480 : A | GENERATOR SYSTEM, 400 HERTZ ALTERNATING CURRENT, AIRCRAFT GENERAL SPECIFICATION FOR |
| MIL C 7115 : F | CONVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR |
Summarise
US$20.00
Excluding Tax where applicable
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