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UF94200
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TMUFGCN01-P02 LEVEL 1
FMGS WARNINGS - ALTITUDE ALERT / DECISION HEIGHT (DH)
EFFECTIVITY 22-00-00 Page 5
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MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
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FMGS WARNINGS
AUTOLAND
The AUTOLAND red warning informs the pilot that,
depending on the procedures, he has to perform a
go-around or a manual landing.
This warning can only be activated in LAND mode with
at least one autopilot engaged.
The AUTOLAND red warning is triggered below 200ft in
LAND mode in the following cases:
- Both AP OFF below 200ft RA.
- LOC excessive deviation (1/4 dot above 15ft
RA) or GLIDE excessive deviation (1 dot above
100ft RA).
LOC and GLIDE scales flash on the PFD.
- Loss of LOC signal above 15ft or loss of GLIDE
signal above 100ft.
The FD bars flash on the PFD. The LAND mode
remains engaged.
A triple click aural warning is generated in the event
of landing capacity downgrading.
The warning is cancelled by LOC mode or AP
disengagement or by performing a go-around.
NOTE: A warning test can be performed by pressing the
Captain or the First Officer AUTOLAND
pushbutton.
TMUFGCN01-T03 LEVEL 1
EFFECTIVITY 22-00-00 Page 6
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FMGS WARNINGS - AUTOLAND
TMUFGCN01-P03 LEVEL 1
EFFECTIVITY 22-00-00 Page 7
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THIS PAGE INTENTIONALLY LEFT BLANK
TMUFGCN01 LEVEL 1
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22 - AUTO FLIGHT SYSTEM
22-66-00 FAC INTERFACES
CONTENTS:
Analog Inputs/Outputs
Discrete Inputs/Outputs
ARINC Inputs/Outputs
TMUFACJ01 LEVEL 3
EFFECTIVITY 22-66-00 Page 1
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MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
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FAC INTERFACES
ANALOG INPUTS/OUTPUTS
The schematic shows the Flight Augmentation Computer
(FAC) analog inputs and outputs.
TMUFACJ01-T01 LEVEL 3
EFFECTIVITY 22-66-00 Page 2
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TMUFACJ01-P01 LEVEL 3
FAC INTERFACES - ANALOG INPUTS/OUTPUTS
EFFECTIVITY 22-66-00 Page 3
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FAC INTERFACES
DISCRETE INPUTS/OUTPUTS
The schematic shows the FAC discrete inputs and
outputs.
TMUFACJ01-T02 LEVEL 3
EFFECTIVITY 22-66-00 Page 4
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FAC INTERFACES - DISCRETE INPUTS/OUTPUTS
TMUFACJ01-P02 LEVEL 3
EFFECTIVITY 22-66-00 Page 5
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MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
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FAC INTERFACES
ARINC INPUTS/OUTPUTS
The FAC dialogues with the other components mainly
through ARINC 429 digital buses.
The schematic shows the FAC input and output ARINC 429
buses.
NOTE : - The FAC data are transmitted to the other
systems through the FAC main bus.
- The Fault Isolation and Detection System
(FIDS) is only activated in FAC 1 by the
SIDE 1 discrete signal.
TMUFACJ01-T03 LEVEL 3
EFFECTIVITY 22-66-00 Page 6
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MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
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FAC INTERFACES - ARINC INPUTS/OUTPUTS
TMUFACJ01-P03 LEVEL 3
EFFECTIVITY 22-66-00 Page 7
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MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
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