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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 410
ALL
CFDS SPECIFIC PAGE PRESENTATION
TMUFCPG05-P03 LEVEL 3
EFFECTIVITY 27-00-00 Page 7
Aug 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 411
ALL
CFDS SPECIFIC PAGE PRESENTATION
SFCC-1
SLAT TEST RESET
SFCC TEST FAILURE REPORT (MEMORY READ OUT)
Failure data from the automatic integrity test (PWR
UP TEST) or from the maintenance test (SFCC-TEST) is
stored in the SFCC TEST FAILURE REPORT.
If there is no failure, therefore no report, the "NO
FAULTS" message is displayed.
To read the failure message, the corresponding failure
report has to be selected.
On selection of one PWR UP TEST report, the failure
message is displayed.
NOTE: "L1: OUTPUT DISCRETES" denotes failure messages
about LANE 1.
"L2: OUTPUT DISCRETES" denotes failure messages
about LANE 2.
WTB-RESET
When the START WTB RESET key is pressed, the associated
WTB solenoid valves are reset and the result is
displayed.
TMUFCPG05-T04 LEVEL 3
EFFECTIVITY 27-00-00 Page 8
Aug 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 412
ALL
CFDS SPECIFIC PAGE PRESENTATION
TMUFCPG05-P04 LEVEL 3
EFFECTIVITY 27-00-00 Page 9
Aug 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 413
ALL
CFDS SPECIFIC PAGE PRESENTATION
SFCC-1
SLT SYSTEM DATA
PPU
The slat PPU data is refreshed every 5 seconds with
updated data.
NOTE: "272.3" represents the decimal value of the
synchro angles.
"C1A" represents the hexadecimal value of the
same data.
ARINC 429 INPUT STATUS
Whatever the selection SLAT ARINC INPUT STATUS or FLAP
ARINC INPUT STATUS the display has the same
presentation. Except for FLAP an additional STATUS
message is displayed concerning ARINC 429 inputs from
LGCIU: ("LGCIU OK").
DISCRETE INPUTS
The status of the slat discrete inputs is displayed
on the MCDU.
NOTE: "$" represents function set (1) or function reset
(0).
"%" represents logic 1 or logic 0 as determined
by input circuit.
"AOG" means Aircraft On Ground.
"SGOI" means System Ground Operation Inhibit.
NOTE: The following data are available only in the
flap channel.
"XX...XX" replaces FLAP RELIEF ENABLED or FLAP
RELIEF DISABLED or FLAP RELIEF CODING FAIL
"YY...YY" replaces MAX FLAP 25 DEG or MAX FLAP
CODING FAIL
X-LINK INPUT
Each channel receives and validates the following
information:
- LABEL 23 Attachment data
- LABEL 60 Diagnosis data
- LABEL 61 Unused
- LABEL 62 System Status Word data
- LABEL 63 FPPU Synchro Angle data
- LABEL 64 LH APPU Synchro Angle data
- LABEL 65 RH APPU Synchro Angle data
- LABEL 67 WTB/POB data word
TMUFCPG05-T05 LEVEL 3
EFFECTIVITY 27-00-00 Page 10
Aug 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 414
ALL
CFDS SPECIFIC PAGE PRESENTATION
TMUFCPG05-P05 LEVEL 3
EFFECTIVITY 27-00-00 Page 11
Aug 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 415
ALL
CFDS SPECIFIC PAGE PRESENTATION
SFCC-1
TROUBLE SHOOTING DATA
The "TROUBLE SHOOTING DATA" item provides additional
data about the failures (all classes) recorded during
the last and previous legs.
The failure selected on the previous page is displayed
with its snapshot data at the occurence of this
failure.
SFCC-1
ON GROUND FAULTS
The MCDU displays the faults stored in the "on ground
failure memory"(generally limited to the 3 last faults
recorded).
But if no failures are stored, the MCDU displays the
"NO FAULTS" message.
TMUFCPG05-T06 LEVEL 3
EFFECTIVITY 27-00-00 Page 12
Aug 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 27 FLIGHT CONTROLS
UF94200
EFFECTIVITY Page 416
ALL
CFDS SPECIFIC PAGE PRESENTATION
　
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