TXT
묘사:
Flight Information Processor
MRC:
The alternating current voltage for which the item is rated,expressed in volts.ACUQ
Alternating Current Voltage Rating In Volts:
115.0
MRC:
The direct current voltage for which the item is rated,expressed in volts.ACUR
Direct Current Voltage Rating In Volts:
26.0
MRC:
The national stock number or the identification information of the end equipment for which the item is a part.AGAV
End Application:
F-15s
MRC:
A measurement of the longest dimension of an item unencumbered by packaging or packing,in distinction from width.AJAF
Unpackaged Unit Length:
9.50 inches
MRC:
A measurement taken at right angles to the length of an item unencumbered by packaging or packing,in distinction from thickness.AJAG
Unpackaged Unit Width:
6.20 inches
MRC:
A measurement from the bottom to the top of an item unencumbered by packaging or packing,in distinction from depth.AJAH
Unpackaged Unit Height:
6.50 inches
MRC:
The source of power which provides the energy required for the operation of the item.AWZJ
Power Source:
External
MRC:
Indicates the type of intelligence the item is capable of receiving.AXQH
Input Intelligence Type:
Air pressure and angle of attack and air temperature and altitude, general data
MRC:
The means used to input the intelligence.AXQJ
Intelligence Input Method:
Air or electrical
MRC:
Indicates the type of intelligence the item is capable of transmitting.AXQK
Output Intelligence Type:
Air data
MRC:
The number of alternating current phases.FAAZ
Phase:
Single
MRC:
Those unusual or unique characteristics or qualities of an item not covered in the other requirements and which are determined to be essential for identification.FEAT
Special Features:
There are 2 different mechanical mounts, 1 used in the eaic location and 1 used in the adc location
MRC:
The cycles per second /hertz/ of the alternating current.FREQ
Frequency In Hertz:
400.0
MRC:
Describes the capabilities,intended use,and/or purpose for which the item is provided.FTLD
Functional Description:
The processor acceptsinputs from the aircraft free stream pitot-static pressure system, angle of attack sensors, aircraft total temperature sensors, ngine air inlet duct pitot-static pressure system, and altimeter barometric setting. Ds necessary to control the variable enginge inlet geometry 3) provide the afcs with pitot pressure, static pressure and impact pressure.Suppgtech characteristics: milstd-1750a processor, contains 1553 bus, built-in-test/3 external fail indicators, requires no cooling air, provides pressure signal outputs, controls engine intake air flow, provides air data to other aircraft systems.
MRC:
The alpha-numeric-alpha designation used to identify the type and/or model of the basic item.TMDN
Type/model Designation:
Cpu-194/a
