NPFC - MIL-T-58097
TRANSMITTERS, PRESSURE, HELICOPTER, VOLTAGE RATIO TYPE, GENERAL SPECIFICATIONS FOR
active, Most Current
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| Organization: | NPFC |
| Publication Date: | 10 January 1975 |
| Status: | active |
| Page Count: | 20 |
scope:
This specification covers the general requirements for voltage ratio type helicopter pressure transmitters.
intended Use:
The transmitters covered by this specification are intended for use with variable-reluctance-
Document History
December 3, 2014
Transmitters, Pressure, Helicopter, Voltage Ratio Type, General Specification for
A description is not available for this item.
March 3, 2010
Transmitters, Pressure, Helicopter, Voltage Ratio Type, General Specification for
A description is not available for this item.
March 24, 2005
TRANSMITTERS, PRESSURE, HELICOPTER, VOLTAGE RATIO TYPE, GENERAL SPECIFICATIONS FOR
A description is not available for this item.
July 14, 1995
TRANSMITTERS, PRESSURE, HELICOPTER, VOLTAGE RATIO TYPE, GENERAL SPECIFICATIONS FOR
A description is not available for this item.
December 5, 1991
TRANSMITTERS, PRESSURE, HELICOPTER, VOLTAGE RATIO TYPE, GENERAL SPECIFICATIONS FOR
A description is not available for this item.
January 19, 1990
TRANSMITTERS, PRESSURE, HELICOPTER, VOLTAGE RATIO TYPE, GENERAL SPECIFICATIONS FOR
A description is not available for this item.
October 20, 1988
TRANSMITTERS, PRESSURE, HELICOPTER, VOLTAGE RATIO TYPE, GENERAL SPECIFICATIONS FOR
A description is not available for this item.
October 20, 1988
TRANSMITTERS, PRESSURE, HELICOPTER, VOLTAGE RATIO TYPE, GENERAL SPECIFICATIONS FOR
A description is not available for this item.
September 9, 1981
TRANSMITTERS, PRESSURE, HELICOPTER, VOLTAGE RATIO TYPE, GENERAL SPECIFICATIONS FOR
A description is not available for this item.
MIL-T-58097
January 10, 1975
TRANSMITTERS, PRESSURE, HELICOPTER, VOLTAGE RATIO TYPE, GENERAL SPECIFICATIONS FOR
The transmitters covered by this specification are intended for use with variable-reluctance-type indicators conforming to MIL-I-58098 in providing remote indication of aircraft pressure functions.