*
Quick access recorder function (QARF)
*
Digital flight data acquisition function (DFDAF).
These are the software functions in the CPM/ACMF:
*
Data conversion gateway function (DCGF)
*
Flight management computing function (FMCF)
*
Thrust management computing function (TMCF)
*
Airplane condition monitoring function (ACMF).
These are the software functions in the CPM/Basic:
*
Data conversion gateway function (DCGF)
*
Flight management computing function (FMCF)
*
Thrust management computing function (TMCF).
These are the software functions in the CPM/GG:
*
Data conversion gateway function (DCGF)
*
Primary display function (PDF).
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Avionics Systems Supported by AIMS
The AIMS cabinets do the calculations for several avionic systems. Because the cabinets do the calculations for these systems the systems are considered to be integrated. The systems are:
*
Primary display system (PDS)
*
Central maintenance computing system (CMCS)
*
Airplane condition monitoring system (ACMS)
*
Digital flight data recorder system (DFDRS)
*
Data communication management system (DCMS)
*
Flight management computing system (FMCS)
*
Thrust management computing system (TMCS).
The system includes the software function in the AIMS cabinets plus their components that have an interface.
Primary Display System
The components of the primary display system are:
*
Primary display function (PDF)
*
Display unit (DU) (6)
*
Display select panel (DSP)
*
Cursor control device (CCD) (2)
*
Captain display switching panel
*
First officer display switching panel
*
Center display control panel
*
Instrument source select panel (2)
*
EFIS control panel (EFIS CP) (2)
*
Remote light sensor (RLS) (2).
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Central Maintenance Computing System
These are the components of the central maintenance computing system:
*
Central maintenance computing function (CMCF)
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Maintenance access terminal (MAT)
*
Portable maintenance access terminal (PMAT).
Airplane Condition Monitoring System
These are the components of the airplane condition monitoring system:
*
Airplane condition monitoring function (ACMF)
*
Quick access recorder (QAR)
*
Quick access recorder function (QARF).
Flight Data Recorder System
These are the components of the flight data recorder system:
*
Digital flight data acquisition function (DFDAF)
*
Flight data recorder (FDR).
Data Communication Management System
These are the components of the data communication management system:
*
Data communication management function (DCMF)
*
Flight deck communication function (FDCF)
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* Accept/Cancel/Reject switch (2).
Flight Management Computing System
These are the components of the flight management computing system:
*
Flight management computing function (FMCF)
*
Control display unit (CDU) (3).
Thrust Management Computing System
These are the components of the thrust management computing system:
*
Thrust management computing function (TMCF)
*
Autothrottle servo motor (ASM) (2)
*
TO/GA switch (2)
*
Autothrottle disconnect switch (2).
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General Interfaces
The AIMS has interface with all types of data communication formats. The two AIMS cabinets send data to and receive data from many of these:
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