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MS33543 Revision A:1953

Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

CRITERIA TEMPERATURE AND ALTITUDE RANGE SELF COOLED ELECTRIC EQUIPMENT

Available format(s)

PDF

Withdrawn date

06-08-1997

€17.95
Excluding VAT

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Withdrawn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
MIL-I-85071 Revision A:1992 INVERTERS, AIRCRAFT, DC TO AC, GENERAL SPECIFICATION FOR
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 AND FREE AIR, TYPE MA AND 3
MIL-B-23072 Base Document:1961 BLOWER, ANTI-EXPOSURE SUIT VENTILATION, GENERAL SPECIFICATION FOR
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

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