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* 1300 Hz marker
* 400 Hz marker.
The GPWS sends these parameters to the FDAU:
FDRS - FDAU DIGITAL INTERFACE
EFFECTIVITY
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
31-31-00-009
* Wind shear caution
* Wind shear
* Terrain pull up
* Minimums
* Glideslope
* Too low terrain
* Too low flap
* Too low gear
* Don’t sink
* Terrain
* Pull up
* Sink rate
* GPWC failure.
The radio altimeter 1 and 2 transceivers send these parameters
to the FDAU:
* Radio altitude
* LRRA receiver antenna
* LRRA transmit antenna
* LRRA failure.
The TCAS computer sends these parameters to the FDAU:
* Altitude Select
* Sensitivity level control
* SPI
* Altitude reporting
* Down advisory
* Up advisory
* vertical control
* Combined control
* Advisory rate to maintain
* RI field
* TCAS sensitivity level
* TCAS system status
* TCAS computer unit.
The left and right ADIRU sends these parameters to the FDAU:
* AD/IR fault
* Excess motion error
* No IR initialization
* Align fault
* On DC
* IR fault
* ADC fault
* DC fail
* altitude invalid
* Set heading
* Nav mode
* Rev attitude mode
* Align mode not ready
* Auto nav realign
* IR A/C ident code invalid
* variable align select
* ADIRU select.
The clock sends these parameters to the FDAU:
* GMT
* GMT (hrs/min)
* GMT (second)
* Date (day)
FDRS - FDAU DIGITAL INTERFACE
EFFECTIVITY
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D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
31-31-00-009
* Date (month)
* Date (year).
DEU 1 and 2 send these parameters to the FDAU:
* Engine system parameters
* Brake system parameters
* Hydraulic system oil parameters
* Hydraulic system pressure parameters
* Fuel system parameters
* Radio altitude
* Localizer and glideslope deviation
* ADIRU parameters
* Displayed indications
* autopilot system parameters
* Electrical system parameters
* CDS display unit formats
* TCAS parameters
* VOR parameters
* ADF parameters
* FMCS parameters
* CDS EFIS control panel selections
* GPWS parameters
* CDS fault annunciations.
The APU electronic control unit sends these parameters to the
FDAU:
* N1
* Oil temperature
* EGT
* Fuel flow
* Low oil quantity
* Bleed valve open
* Any fault detected
* Bleed air switch
* Ready to land.
The stall management yaw dampers 1 and 2 send these
parameters to the FDAU:
* Rudder position
* Rudder command
* Angle of attack
* Stick shaker speed
* Minimum airspeed for flap retraction
* Minimum operating speed
* High speed buffet
* Auto slat enable
* Yaw damper engage
* Auto slat command
* Auto slat valid.
The FCC 1 and 2 send these parameters to the FDAU:
* Selected course
* Selected heading
* Selected altitude
* Selected airspeed
* Selected vertical speed
* Selected mach
* Spoiler position number 2
* Spoiler position number 7
* MCP speed
* L Nav mode oper
* CWS roll
FDRS - FDAU DIGITAL INTERFACE
EFFECTIVITY
SHZ ALL 31-31-00
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D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
31-31-00-009
* CWS pitch
* A/P off
* Single channel
* TO/GA
* V/S engaged
* Altitude hold
* Altitude acquire
* Heading select
* VOR/LOC engage
* G/S engage
* Flare engage
* Local limited master
* G/S deviation warning
* Localizer deviation warning
* A/T speed warning
* ILS deviation warning
* Visual altitude alert
* CWS B
* CWS A
* CMD B
* CMD A
* F/D B on
* F/D A on
* CWS warning
* Indicated airspeed display
* Vertical speed PB lite
* V Nav PB lite
* Level change PB lite
* Altitude hold PB lite
* N1 PB lite
* Speed PB lite
* Approach PB lite
* Heading select PB lite
* VOR/LOC PB lite
* L Nav PB lite
* B master light
* A master light.
The auto throttle sends these parameters to the FDAU:
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