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In the NORMAL position, the captain displays show data from
MMR 1, VOR 1, and DME 1 systems and the F/O displays show
data from MMR 2, VOR 2, and DME 2 systems.
When BOTH ON 1 or BOTH ON 2 is selected, the captain and the
F/O displays show navigation data from the selected source.
CDS - NAVIGATION INTERFACES - 4
EFFECTIVITY
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
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CDS - NAVIGATION INTERFACES - 4
CDS - NAVIGATION INTERFACES - 4
EFFECTIVITY
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
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Data Loader Control Panel
SHZ 009-999
The data loader control panel sends information to the display
electronic units (DEU) from the airborne data loader (ADL).
Software can be uploaded to the DEUs in this manner.
SHZ 001-003
The data loader control panel sends information to the display
electronic units (DEU) from the portable data loader (PDL).
Software can be uploaded to the DEUs in this manner.
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The control panel also receives data from the DEUs on the
DFDAU bus. This function is used to download fault history from
the DEUs
A function discrete from the data loader is switched through the
data loader control panel to the DEUs. This ground discrete is
the load enable signal to the DEUs.
Airplane Condition Monitoring System
The DEUs send EEC data on the ENGINE EEC buses. The DEUs
send all the labels received from the four EEC input buses to the
FDAU. EEC channel A data for both engines goes from DEU 1
and EEC channel B data for both engines goes from DEU 2. This
data is used by the airplane condition monitoring system.
CDS - INDICATING AND RECORDING INTERFACES
EFFECTIVITY
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CDS - INDICATING AND RECORDING INTERFACES
CDS - INDICATING AND RECORDING INTERFACES
EFFECTIVITY
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CDS - INDICATING AND RECORDING INTERFACES
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
Mode Control Panel
The mode control panel (MCP) sends data to the display
electronic units (DEUs) on ARINC 429 buses. The MCP 1 bus
has this data:
* Selected course 1
* Selected heading
* MCP selected altitude.
The MCP 2 bus has this data:
* Selected course 2
* Selected heading
* MCP selected altitude.
The DEUs use this data to show on the flight and navigation
displays.
Flight Control Computers
The flight control computers (FCCs) send data to and receive
data from the DEUs on ARINC 429 buses.
The FCCs send this data to the DEUs:
* Target mach number
* Local selected course
* Selected heading
* Selected altitude
* Selected vertical speed
* Selected mach number
* Flap position
* Flight director commands (pitch)
* Flight director commands (roll)
* Airspeed bug drive
* Spoiler position (left and right)
* AFDS discrete word 2
* AFDS discrete word 3
* AFDS discrete word 4.
The AFDS discrete word 2 has this data:
* FLARE ARM
* CWS ROLL
* CWS PITCH
* SINGLE CH
* TO/GA
* V/S ENGAGE
* ALT HOLD
* ALT ACQ
* HDG SEL
* VOR/LOC ENGAGE
* G/S ENGAGE
* FLARE ENGAGE.
The AFDS discrete word 3 has this data:
* IAS/MACH select
* Altitude hold (MCP or VNAV)
* Altitude acquire (MCP or VNAV).
The AFDS discrete word 4 has this data:
CDS - AUTOFLIGHT INTERFACES
EFFECTIVITY
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
　
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