21 AIR CONDITION COMPUTER
PANE
DESIGNATION
FIN
C.B
NOTE
10HQ
D06
21-26-34
L AEVC
49VU
AIR COND/AVNCS VENT/CTL
(811/E2-4)
49VU
AIR COND/AVNCS VENT/CTL
D05
122VU
AIR COND/AVNCS/VENT/MONG
Y17
CPC 1 (811/E1-3)
49VU
AIR COND/CAB/PRESS/CTL 1
1HL
D09
CPC 2 (811/E2-3)
122VU
AIR COND/CAN PRESS/CTL/2
2HL
Y22
CPC 1 & 2
122VU
AIR COND/CAB PRESS/CTL/MAN
PACK SYS 1
122VU
AIR COND/PACK TEMP/CTL
21-26-34
Y23 7HH
X22
21-61-34
SYS1/1/115VAC (811/E1-3)
122VU
AIR COND/PACK TEMP/CTL
X21
SYS1/1/28VDC 122VU
AIR COND/PACK TEMP/CTL
Y19
SYS2/1/28VDC 122VU
AIR COND/PACK TEMP/CTL
Y18
SYS2/1/115VAC PACK SYS 2
122VU
AIR COND/PACK TEMP/CTL
27HH
W22
21-61-34
SYS1/2/115VAC (811/E2-3)
122VU
AIR COND/PACK TEMP/CTL
W21
SYS1/2/28VDC 122VU
AIR COND/PACK TEMP/CTL
Y21
SYS2/2/28VDC 122VU
AIR COND/PACK TEMP/CTL
Y20
SYS2/2/115VAC ZONE CTL
122VU
AIR COND/ZONE TEMP CTL/28VDC/SYS 1
(811/E1-2)
122VU
AIR COND/ZONE TEMP CTL/115VDC/SYS
8HK
V19 V17
1 122VU
AIR COND/ZONE TEMP CTL/28VDC/SYS 2
V20
122VU
AIR COND/ZONE TEMP CTL/115VDC/SYS
V18
2 AFT CARGO FAN 49VU
AIR COND/AFT CARGO/VENT/CT;&MONG
(822)
122VU
AIR COND/AFT CARGO/VENT/FAN
GALLEY FAN
122VU
A/C /LAV/GALLEY VENT CTL/EXT FAN/CTL
(826/AFT CARGO) 122VU
A/C /LAV/GALLEY VENT CTL/EXT
C07 35HN
S22 U21
1HU
U19
FAN/SPLY RECIRC FAN
122VU
AIR COND/RECIRC FAN/R/CTL
(825/FWD
122VU
AIR COND/RECIRC FAN/R/SPLY
CARGO)
W20 14HG
W18
21-63-34
122VU
AIR COND/RECIRC FAN/L/CTL
X20
122VU
AIR COND/RECIRC FAN/L/SPLY
X18
GROUND COOL 123VU
VENT/GND COOL/UNIT
12HD
AC11 21-27-34
UNIT(824)
123VU
VENT/GROUND COOL/UNIT
AC03
122VU
AIR COND/VENT/GND/COOL/CTL
W23
AVNCS FAN
123VU
AVNCS VENT/BLOWER/FAN
20HQ
AD10
(824)
123VU
AVNCS VENT/EXTC/FAN
18HQ
AC04
IND
49VU
AIR COND/FLOW/CTL&/IND 1
D07
122VU
AIR COND/FLOW/CTL&/IND 2
V21
49VU
AIR COND/RAM/AIR/INLET
L/8HH D10
122VU
AIR COND/FLOW/MIXER/FLAP
20HB
R/28HH
V22
早上 PACK KNOT 擺在 COOL 位置,,如果擺在中間,容易有”AVNCS SYS FAULT”會有:”HORN”可將 C/B”P09”OFF RESET C/B’S DURING 10 SEC AT LEAST,, UNLESS OTHERWISE SPECIFIED
ECAM WARNING PACK 1 (2) FAULT OR OVHT
SYSTEM RESET OVHT TEMP’S
OR OFF PACK OUTLET TEMP>,=,95℃ PACK 1 + 2 FAULT
PACK COMPRESS. OUTLET TEMP>,=,260℃ FAULT LIGHT GOSE OUT WHEN OVHT DISAPPEARS
PACK 1 (2) REGUL FAULT FOR ALL OF THESE ECAM WARNING’S(FAULT’S) PACK 1 AND 2 OFF AFTER 30 SEC. RESET C/B’S DURING 2 MIN PACK1→ X21, X22, Y18, Y19 PACK2→ W21, W22, Y20, Y21 AUTO TEST 30 SEC。PACK 1 & 2 ON FWD (AFT) CRG VENT FAULT C/B’S：C7, T22 AUTO TEST 30 SEC。 CKPT (FWD, AFT CAB)
OVHT TEMP：DUCT TEMP,>,=,80℃
(GOW, AFT CRG) DUCT OVHT FAULT L/T GOSE OUT WHEN DUCT TEMP.<70℃ HOT AIR P/B RESETED HOT AIR FAULT
WSIT 3 MIN. AFTER PACK’S ON BEFORE HOT AIR P/B BE RESETED. IF UNSUCCESSFUL, RESET： C/B’S：V17, V18, V19, V20 ATUO TEST 36 SEC
TRIM AIR SYS FAULT
If the warning and the message TRIM AIR PR are triggered when all
Trim Air vlves are closed (during the first 30sec.after the packs are Selected ON or in flight if all zones heating demands are fulfilled)， Disregard them。If not：reset HOT AIR P/B If unsuccessful, reset： C/B’S：V17, V18, V19, V20 AUTO TEST 36 SEC。 ZONE REGUL FAULT
PACK 1 AMD 2 OFF C/B’S V17, V18, V19, V20 AUTO TEST 36 SEC。 PACK 1 AND 2 ON
Note ：reset with engine running may triggered the message ENG 1(2) FADEC，in STATUS page。 ＊ L+ R CAB FAN FAULT
C/B’S LH--X18，X20
LAV + GALLEY FAN FAULT
C/B’S U19，U21
RH--W18，W20
(＊＝ NO DISPATCH) FWD CRG ISOL VLV
C/B’S T22
AFT CRG ISOL VLV
C7，S22
FWD CRG HEAT VLV
T22
AFT CRG HEAT VLV
C7，S22 AUTO TEST 28 SEC
SYS 1(2) FAULT
ADIRU 1，2，3，NAV RESET C/B’S DURING 2 MIN C/B’S： CPC1—D09
SYS 1 + 2 FAULT
CPC2—Y22 MAN CTRL—Y23
RESET C/B’S DURING 2MIN C/B’S：D09，Y22，Y23
＊ OUTFLOW VLV NOT OPEN TRY CAB PRESS MAN CTRL MODE SEL－MAN MAN VS CTL－FULL UP It may take 10 sec，in MAN mode before the crew notices a change of the outflow valve position。 IF UNSUCESSFUL，PACK 1 AND 2 －OFF LDG ELEV FAULT
CHECK FMGS DESTINATION DATA (ALT ) TRY CAB PRESS MAN CONTRAL
BLOWER FAULT
For all of these ECAM WARNING pull C/B’S：Y17，D05，D06 And AE2 (AC4 for A321) check “AVNCS SYS FAULT”
EXTRACT FAULT
Appears on ECAM after 10 sec 。 Push C/B’S and check message disappears。 AUTO TEST 85 SEC
SKIN VLV FAULT
If any message about VENT SYS still remains after reset C/B’S，
Try DITCHING “ON ” than OFF to reset inputs to AVIONICS SYS AVNCS SYS FAULT
If a message persist on ECAM verify that the “deactivation sw”， In both valves (EXTRACT AND BLOWER ) are OFF ，it must Be “ON”
22 AUTO FLT SYSTEM COMPUTER
PANEL DESIGNATION
FIN
C.B
NOTE
FAC 1 (824/E1-2)
49VU
AUTO FLT/FAC1/28VDC
1CC1
B04
22-66-34
49VU
AUTO FLT/FAC1/26VAC
B03
CAT ll
121VU
AUTO FLT/FAC2/28VDC
M19
Reset 10”sec
121VU
AUTO FLT/FAC2/26VAC
M18
Auto test 90 sec
49VU
AUTO FLT/FCU/1
B05
22-81-12
122VU
LIGHTING/INSTL LT/GLARE/SHLD
Y05
CAT ll
121VU
AUTO FLT/FCU/2
M21
RVSM
FAC 2 (824/E2-2) FCU
1CC2 2CA
FMGC 1 (824/E1-2)49VU
AUTO FLT/FMGC/1
1CA1
B02
22-83-34
FMGC 2 (824/E1-2)121VU
AUTO FLT/FMGC/2
1CA2
M17
CAT ll RNP-10
MCDU 1
49VU
AUTO FLT/MCDU/1
3CA1
B01
22-82-12
MCDU 2
121VU
AUTO FLT/MCDU/2
3CA2
N20
RNP-10
122VU
LIGHTING/INSTL LT/GLARE/SHLD
Y05
（FAC＝Flight Augmentation Computer） （FCU＝Flight Control Unin） （FMGC＝Flight Management and Guidance Computer） （MCDU＝Multipurpose Control & Display Unit）
（22）AUTO FLIGHT NOTE：reset C/B during 10 sec at least, unless otherwise specified
ECAM WARNING
SYSTEM RESET
YAW DAMPER 1 (2)
RESET FAC 1 (2) P/B
YAW DAMPER SYS
On the ground, if unsuccessful，the C/B of the affected FAC should
RUD TRIM 1 (2)
Be pulled with the yellow and green hyd sys pressurized and ENG
RUD TRIM SYS
Stopped, and reseted after 10sec。
RUD TRV LIM 1 (2)
C/B：FAC1--B3，B4
RUD TRV LIM SYS
FAC2—M18，M19
（TRV=Travel）
AUTO TEST 90 sec
FAC 1 (2) (1+2) FAULT
ENG 1 and 2 stopped C/B：FAC 1 –B3，B4 FAC 2 –M18，M19 AUTO TEST 90 SEC
FCU 1 (2) (1+2) FAULT
RESET DURING 7 min ，at least C/B：FCU 1 – B5 FCU 2 – M21
WIND SHEAR
RESET BOTH FAC’s，one after another C/B：FAC 1 –B3，B4 FAC 2 –M18，M19 AUTO TEST 90 SEC
23 COMMUNICATION SYSTEM COMPUTER
PANEL DESIGNATION
FIN C.B NOTE
CIDS 1(824)
121VU
COM
101R M06 23-73-34
NAV/CIDS/DIR/NORM 1
H
CIDS 2(824)
49VU
COM/CIDS/DIR ESS / 1
121VU
COM/NAV/CIDS/DIR/NOR 102R M07 B-22312 M2
HF (824) VHF (824) DEU A (Decoder/Encoder
G01 H
49VU
COM/CIDS/DIR ESS / 2
49VU
COM NAV/FH 1
3RE1 HA14 23-11-33
121VU
COM NAV/FH 2
3RE2 L13
49VU
COM NAV/VHF 1
1RC1 G09 23-12-33
121VU
COM NAV/VHF 2
1RC2 L04
49VU
COM NAV/CIDS/DEU A
200R G04
ESS/LINE 1
H
49VU
G02 M05,G02
COM NAV/CIDS/DEU A
G05 LOUD SPKR
ESS/LINE 2 Unit)
121VU
COM NAV/CIDS/DEU A
M10
GENRL ILLIUM
NORM/L FWD ASM23-73/06,07,08
121VU
COM NAV/CIDS/DEU A
M11 PAX LT SIGN
NORM/R FWD 121VU
COM NAV/CIDS/DEU A
M12 PAX CALL
NORM/L MID 121VU
COM NAV/CIDS/DEU A
M13
NORM/R MID DEU B
49VU 121VU
COM NAV/CIDS/DEU B
300R G03 AIP ACP FAP
/ESS
H
COM NAV/CIDS/DEU B
M09 HAND SET
/NORM EMER EVAC CTL&IND
AMU
49VU
COM/AUDIO/ACP/CAPT
1RN G06 23-51-34
Audio
49VU
COM/AUDIO/ACP/F/O
G07
Management
49VU
COM/AUDIO/FLT/INTPH
G08
Unit
121VU
COM NAV/SELCAL
M04
RMP
49VU
COM NAV/RMP/1
1RG1G10 23-13-13
121VU
COM NAV/RMP/2
1RG2L02
121VU
COM NAV/RMP/3
1RG3L03
49VU
COM/CVR/CTL
E13 23-71-35
49VU
COM/CVR/SPLY
E14
121VU
COM NAV/CIDS/FWD
120R M14 23-73-12
ATTNO/PNL
H
COM NAV/CIDS/PROG &
110R M08
TST PNL
H
CVR FAP
121VU ANNCH
2000VU CABIN COMMUNICATION 10RX F07 SYSTEM-PRA 121VU
COM
M03
NAV/ACP/AVNCS/COMPT 121VU
EIS/HORN/SPLY
P09
121VU
COM NAV/ACARS/MU
L06 ON A/C 002-002
2000VU COMMUNICATION
F06 ON A/C 001-002
SYSTEM-PES
23 COMMUNICATIONS NOTE：reset C/B during 10 sec at least, uniess otherwise specified ECAM WARNING ＊ CIDS 1+2 FAULT
SYSTEM RESET SEE ANEX 1
Cabin Intercommunication Data System
＊ VHF EMITTING
Check transmission key on ACP，side stick radio selector or hand Mike selector or PTT switch is not in “transmit” position。In the Other case ，deselect the affected transmission for 1 sec，to reset The caution。 If no selector / key is found in “transmit” position，reset the affected C/B。 C/B： VHF 1-G9 VHF 2-L4 VHF 3-L5 （if install）AUTO TEST 2 sec
HF EMITING (if install)
Check transmission key on ACP，side stick radio selector or hand
Mike selector or PTT switch is not in “transmit” position。In the Other case，deselect the affected transmission for 1 sec，to reset the Caution。 If no selector / key is found in “transmit” position，reset the affected C/B。 C/B： HF 1 – HA14
ACARS FAULT （If install）
C/B：L6 ANNEX1 CIDS SYSTEM FUNCTION RESTORATION
In the event of a misbehavior of one or more functions associated to the CIDS the actions described in the following page are intended To Assist in restoring the correct operation The majority for the troubles encountered can be classified as follows： －ALOSS OF CONTROL OF A FUNCTION －SPURIOUS ACTIVATION OF A FUNCTION －FAILURE OF A FUNCION （1）The functions directly controlled by CIDS are： IN FLIGHT －THE PASSENGER ADRESS －THE CABIN AND FLIGHT CREW INTERPHONE －THE CALL SYSTEM －THE PASSENGER LIGHTED SIGNS －THE CABIN ILLIMINATION ON GROUND －THE SERVICE INTERPHONE －THE EXTENDED EMERGENCY LIGHT TEST For any troubles on the above functions，please go directly to PART I which gives recommendations for resetting the CIDS. （2）The systems indicated or interfaced through the forward attendant panel ( FAP ) are： －THE PRE RECORDED ANNOUCEMENT AND BOARDING MUSIC MODULE ( PRAM ) －THE LAVATORY SMOKE INDICATION －CIDS CAUTION LIGHT －EVAC WARNING LIGHT For any troubles on the above systems，please go directly to PART II for a system diagnostic and recovery
procedure。 PART I RESET OF CIDS Two procedures are given below： Procedure A－any be used on ground （engines running or not）or in flight is a simplligied reset procedure which allows the reset of directories and does not allow the reset of all other CIDS components 。( FAP…….) however，it covers the majority of reported failures Procedure B－may only be used on ground with both engines stopped allows the full reset of all the system。 Note（1）for PROCEDURE A or B The pulling of C/B results in a reset of the CIDS and power up test during which time the system will not respond to any inputs or changes Of commands until the power up test has finished。Time are indicated for each procedure。 Note（2） A reset function is provided on the menu of the PTP ( programming and test panel ) .in the event of a malfunction of the CIDS the data bus Link between the director and the PTP may also be affected, therefore it is suggested to limit resets to the pulling of detalled C/B as a reset Push baton at the PTP, and initiates a power up test only if the ARINC communication link between the programming and test panel and Director gxists PROCEDURE A NOTE：During power-up test the CIDS remains out of service Condition： In flight or on ground（engine(s) running or not）。 Procedure： Pull the following C/B： A320
A321
G2
G2
49VU
G1
49VU
M7
121VU
M6
121VU
M5
Wait approximatrly 10 sec 。If doors are close，or 30 sec。If doors are open. Re-engage the above C/B： Power-up test 50 sec If doors are close，120 sec If doors are open。 PROCEDURE B CONDITION：on ground with both engines stopped。 PROCEDURE：pull the following C/B in the order given below：
A320
A321
49VU
G2
G2
49VU
G1
121VU
M7
121VU
M6
49VU
G5
G5
49VU
G4
G4
49VU
G3
G3
121VU
M5
M14
121VU
M13
M13
121VU
M12
M12
121VU
M11
M11
121VU
M10
M10
121VU
M9
M9
121VU
M8
M8
121VU
M7
121VU
M6
121VU M14
121VU
C8 , C7 , C6 , C5
2001VU
WAIT FOR 30 SEC.AND REENGAGE THE FOLLOWING C/B , IN ORDER GIVEN BELOW： A320
A321 C5
2001VU
C6
2001VU
C7
2001VU
C8
2001VU
M14
121VU
M13
M13
121VU
M12
M12
121VU
M11
M11
121VU
M10
M10
121VU
M9
M9
121VU
M8
M8
121VU
M7
121VU
M6
121VU M14
121VU
G5
G5
49VU
G4
G4
49VU
G3
G3
49VU
PART II
RESET OF SYSTEMS INDICATED OR INTERFACED THROUGH FORWARD FLIGHT ATTENDANT PANEL （FAP） This section covers the following functions A－The pre recorder announcement and boarding music module （PRAM） B－The lavatory smoke indication C－CIDS caution light D－EVAC (evacuation) Warning light Note：cabin illumination is directly controlled by CIDS but the interface is through the FAP The following procedures can be applied either in flight or on ground, engines running or not, regardless of whether the door are open Or not unless PROCEDURE A is applied。 A－Procedure for restoring control of PRAM ON FAP： （1）PRESS STOP P/B （2）PRESS CLEAR P/B （3）ENSURE ALL WINDOWS INDICATE PROGRAM 000 LOADED , IF NOT ENTER 000 IN EACH MEMO （4）LOAD THE NUMBERS CORRESPONDING TO THE REQUIRED ANNOUNCEMENT SLOWLY AND PRECISELY TO ENSUER CORRECT RECOGNITION OF COMMAND （5）OPERATED IN USUAL MANNER If the PRAM still fails to operate correctly it will be necessary to perform a reset of the PRAM by （a）pulling PRAM C/B 2RX on panel 2000VU （b）wait approximately 10 sec （c）pushing in C/B 2RX （d）allow approximately 3 min for PRAM to initialixe （e）enter data as in （4）above The reset procedure described in PART I for resetting the CIDS to gain control a functions may also be used in the event of a Loss of control of the FAP which is subsequently causing a loss of control of the PRAM in which case PROCEDURE A （reset of the CIDS by C/B）should be inserted between point （b）and （c）of the previous procedure。 B－Procedure for extinguishing incorrect or spurious illumination of LAV SMOKE light on FAP Subject to there being no genuine reason for the LAV SMOKE light to be illuminated （no smoke）after a check of the relevant Toilets the light on the FAP and area call panels can be extinguished by the following procedure provided that the reporting
Smoke detection unit or controller is not faulty （1）Press reset P/B on FAP （2）Light the attendant handset in the area nearest to the reporting toilet smoke detector （3）Replace handset Note：if the signal was spurious the LAV SMOKE lamp will extinguish , if it illuminates again the above procedure may be tried only After a check of the relevant toilet area。Repetitive indication indicate further maintenance trouble shooting on ground will be necessary。 C－CIDS CAUTION LIGHT The caution light should only illuminate in flight when there is some positive action to be taken by the cabin attendants or When there is some degradation of a system that they need to know of。 Procedure in the event the CAUTION LIGHT illuminated （1）push ” DISPLAY ON ” P/B on the programming and test panel （2）Read message displayed on display of programming and test panel （3）take and necessary action as advised by message （4）reset caution light by pushing caution light front face Note：The message on the PTT will disappear automatically after 5 min。 The caution light will illuminate automatically after landing if the failure still exists Wait a further 30 sec。then re-engage the following C/B , in the order given below： A320
A321
M5
M7
121VU
M6
121VU
G2
49VU
G1
49VU
G2
POWER-UP TEST－50 sec 。if doors are closed 120 sec 。if doors are open D－EVAC LIGHT If the EVAC warning goes off spuriously then the aural warning in the cabin can be cancelled by pressing the reset button On forward attendant panel and /or aft attendant panel。If the EVAC lamp is lit with no aural warning it will by necessary to Activate the EVAC signal via the “ comd ” P/B on FAP （Provided the EVAC swich in the cockpit is in the CAPT+PURS position）
Or the EVAC switch in cockpit directly （which will generate a warning ）and then cancel the warning by pressing the “ comd ” P/B or switching the EVAC switch 。 Alternatively a reset of the CIDS would correct the situaton，see PART I。 ANNEX II VACUUM CONTROL If the light SYSTEM INOP is ON and be utilized in normal condition but we need pull the C/B VACUUM SYS On AFT GALLEY ， the WASTED QTY indication will be lost。 Below 16000” push the C/B in order to recover the VACUUM STSYEM。 For reset the VACUUM SYSTEM pull the C/B VACUUM SYS LAVATORY POWER FWD LAVATORY POWER AFT LH/RH
On the AFT GALLEY，during at least 30 sec。
24 ELECTRICAL POWER SYSTEM COMPUTER
PANEL DESIGNATION
EGIU 1 (811E1-3) 122VU ELEC/EXT PWR/LT CLT/AVAIL
FIN
C.B
22XU17
X31 24-22-33
ELECTRICAL
122VU ELEC/EXT PWR/CTL
X29
GENERATION
122VU ELEC/EXT
X28
NOTE
PWR/COCKPIT/AVAIL/LT INTERFACE
122VU ELEC/EXT PWR/EGIU1/28VDC
Z31
UNIT
122VU ELEC/GEN1/EGIU1/28VDC
Z30
122VU EXT PWR/EGIU1/115VAC
AA07
122VU GEN1/EGIU1/115VAC
AF12
122VU ELEC/IDG1/DISC
T24
122VU ELEC/GCU/1
T26
EGIU 2(811/E2-3) 122VU ELEC/GEN1/OFF/BTC2 SPLY
22XU2
T30
122VU ELEC/IDG2/DISC
T25
122VU APU GEN/EGIU2/28VDC
Y31
122VU GEN2/EGIU2/28VDC
Y30
24-22-33
123VU APU GEN/EGIU2/115VAC
AA08
123VU GEN2/EGIU2/115VAC
AF01
122VU ELEC/GCU/2
T27
GPCU(811/E2-1) 122VU ELEC/GPCU
1XG
Y24 24-41-34
GROUND
122VU ELEC/EXT PWR/CTL
X29
POWER
123VU GND/PWR/PROT
AB07
CONTROL UNIT GCU-APU(811E1- 122VU ELEC/GEN1/OFF/BTC1 SPLY
1XS
T28
24-23-34
1 122VU ELEC/APU/GCU GCU 1
Y25
122VU ELEC/GCU/1
1XU1
T26
GCU 2(811E1-1) 122VU ELEC/GCU2
1XU2
T27
BLC 1(822) BLC 2 CSM/G
ESS TR
105VU ELEC/BAT BUS/REF/BCL 1
G01 24-38-34
105VU ELEC/BAT REF/BCL 1
F01
105VU ELEC/BAT BUS/REF/BCL 2
J02
105VU ELEC/BAT REF/BCL 2
F02
122VU ELEC/EMER GEN AUTO/1
Z25
122VU ELEC/EMER GEN AUTO/2
Z26
105VU ELEC/CSM/G/EV AUTO/SPLY
C01
105VU ELEC/CSM/G /EV/MAN/SPLY
B04
106VU ESS TR/CNTOR/CTL
C02
106VU ESS TR/SPLY
C01
123VU AC ESS/BUS ON/BUS 1
AC12
123VU AC ESS/BUS ON/BUS 2
AC01
122VU ELEC/CNTOR/ESS/DC BUS/TIE
W26
105VU ELEC/CSM/G/EV AUTO/SPLY
C01
106VU ELEC/CSM/G/EV/MAN/SPLY
B04
106VU AC ESS BUS/EMER CNTOR/CTL
B07
106VU AC ESS
C06
BUS/EMER/STBY/CNTOR/SPLY
TR 1
106VU AC ESS BUS/MONG/SPLY
C05
106VU AC ESS BUS/STBY/CNTOR/CTL
B08
106VU AC ESS/BUS NORM/CNTOR/CTL
B03
106VU AC ESS/BUS/EMER/CNTOR/SPLY
C08
122VU ELEC/TR1/FAULT/DC BUS
W29
TIE/CONFIG Transformer
122VU ELEC/TR1/MONG
X25
Rectifier
125VU TR1/CNTOR/SPLY
CF01
123VU TR1/SPLY
AB10
122VU ELEC/TR2/FAULT/DC BUS
W30
TR 2
24-22-34
TIE/CONFIG
GALLEY
STAT INV
122VU ELEC/TR2/MONG
X26
123VU TR2/214XP/SPLY
AB04
124VU TR2/CNTOR/SPLY
BC01
123VU TR2/SVCE/BUS 2/SPLY
AB08
122VU ELEC/GALLEY/CNTOR
S28
122VU ELEC/GALLEY/GND/FLT/LOGIC
S24
122VU ELEC/GALLEY/FAULT/LT CTL
S25
123VU FWD GALLEY/FEEDER D
AD04
123VU MAIN AFT GALLEY/FEEDER E
AF09
123VU MAIN FWD GALLEY FEEDER F
AC10
123VU MAIN-GALLEY A/PWR/SPLY
AF04
105VU ELEC/STAT INV/BUS 901XP/SPLY
H02
105VU ELEC/STAT INV/CNTOR/CTL
G02
24- ELECTRICAL NOTE：reset C/B during 10 sec at feast, unless otherwise specified ECAM WARNING
SYSTEM RESET
＊ EMER CONFIG ＊ ESS BUSSES ON BAT IDG1（2）OIL PR/OVHT GEN1（2）FAULT
C/B： GCU1 － T26 GCU2 － T27
GEN1（2）OFF APU GEN FAULT
C/B： GCU APU － Y25
GEN1（2）or APU GEN PVER LOAD EMER GEN 1 LINE OFF ＊ BAT1（2）FAULT BAT1（2）OFF BCL1（2）FAULT
RESET P/B BAT OFF THEN ON
TR1（2）or ESS TR FAULT
Reset can be performed through CFDS（MCDU） MENU＞＞CFDS＞＞SYS REPORT AND TEST＞＞ELEC＞＞ TR’S RESET
25 EQUIPMENT/FURNISHINGS SYSTEM COMPUTER FAK25-64-00
PANEL
DESIGNATION
122VU
C.B
NOTE
FOOT WARMER
X15
ON A/C 001-002
122VU
COCKPIT SEATS/SEAT CTL/F/O
U14
ON A/C ALL
122VU
COCKPIT SEATS/SEATS/SEAT
U11
CTL/CAPT
IDNT
2001VU
VACUUM CLEANER SOCKET
F01
CARGO Z0261
26 FIRE PROTECTION SYSTEM COMPUTER
PANEL
DESIGNATION
IDNT
C.B
APU FDU
121VU
APU/FIRE & OVHT/DET/LOOP B 13WG L44
121VU
APU/FIRE & OVHT/DET/LOOP A
NOTE 26-13-34
L43
不能在 APU 運作中測試，會 AUTO SHUTDOWN ENG1 FDU
49VU
ENG/1/FIRE DET/LOOP A
121VU
ENG/ENG1/FIRE DET/LOOP B
49VU
ENG/2/FIRE DET/LOOP B
121VU
ENG/ENG2/FIRE DET/LOOP A
SDCU
49VU
AIR COND/SDCU/CHAN 1
10WQ C06
Smoke
122VU
AIR COND/SDCU/CHAN 2
T18
Detection
121VU
APU/AUTO/EXTIG/GND/TEST
L40
Control
121VU
APU/FIRE/EXTIG/SQUIB/A
L38
Unit
121VU
APU/FIRE/EXTIG/SQUIB/B
L39
121VU
APU/FIRE/LP VALVE/NORM
M42
121VU
APU/FIRE/LP VALVE/STBY
M41
121VU
ENG/ENG1 & 2 FIRE
Q43
ENG2 FDU
2WD1 A06
26-12-34
Q38 2WD2 A07
26-12-34
Q39
26-17-34
EXTIG/BTL1/SQUIB/A 121VU
ENG/ENG1 & 2 FIRE
Q44
EXTIG/BTL1/SQUIB/B 121VU
ENG/ENG1 & 2 FIRE
Q41
EXTIG/BTL2/SQUIB/A 121VU
ENG/ENG1 & 2 FIRE
Q42
EXTIG/BTL2/SQUIB/2 121VU
AIR COND/CARGO/FIRE/EXTIG
T19
一、FIRE WARNING 產生原因：（1）兩個 LOOP 都偵測到（2）一個 LOOP 偵測到，另一個失效（3）兩個 都偵測到 FAULT 5 秒（兩個都失效） 二、LOOP FAULT WARNING 的原因：（1）FLECTRICAL FAILURE（2）INTEGRATY FAILURE（3） 一組偵測 FIRE 超過 16 秒，但另一組正常 三、DETECTION FAULT WARNING 原因：兩個 LOOP FAILURE 26-FIRE PROTECTION NOTE：NOTE：reset C/B during 10 sec at feast, unless otherwise specified ECAM WARNING ＊ AVIONICS SMOKE
SYSTEM RESET RESET SDCU C/B：SDCU 1－C6
SDCU2－T18 AUTO TEST 10 SEC ＊LAVATORY SMOKE
SDD ANEX 1 ＞＞PART II－B
LAV+CRG DET FAULT LAVATORY DET FAULT ＊CARGO SMOKE （IF INSTALLED） FWD CRG DET FAULT AFT CRG DET FAULT FWD（AFT）BTL SQUIB FAULT（IF INSTALLED） FIRE LOOP A（B）FAULT
C/B：ENG1-LOOP A＞＞A6
＊FIRE DET FAULT
ENG1-LOOP B＞＞Q38 ENG2-LOOP A＞＞Q39 ENG2-LOOP B＞＞A7
（AUTO TEST 57 SEC）
APU FIRE LOOP A（B）FAULT
C/B：LOOP A＞＞L43
FIRE DET FAULT
LOOP B＞＞L44 AUTO TEST 10 SEC
27 FLIGHT CONTROL SYSTEM COMPUTER
PANEL
DESIGNATION
IDNT C.B
NOTE
ELAC1（E1-
49VU
FLT CNTL/ELAC1/NORM/SPLY
2CE1 B11
27-93-34
105VU
FLT CTL/ELAC1/STBY SPLY
105VU
FLT CNTL/ELAC2/STBY SPLY
121VU
FLT CNTL/ELAC2/NORM SPLY
2） ELAC2（E2-
A01 CAT II 2CE2 A02 27-95-34
2） ELAC= Elevator aileron
R20
computer
SEC1
49VU
FLT CNTL/SEC1/NORM/SPLY
1CE1 B08
SEC1
105 VU
FLT CTL/SEC1STBY SPLY
SEC2
121 VU
FLT CNTL/SEC2/SPLY
1CE2 Q18
SEC3
121 VU
FLT CNTL/SEC3/SPLY
1CE3 Q19
27-94-34
B01
SEC= SPOILER ELEVATOR COMPUTER FCDC1(E1-2)
49VU
FLT CNTL/FCDC1/SPLY
3CE1 B10
FCDC2
121VU
FLT CNTL/FCDC2/SPLY
3CE2 Q20
27-95-34
FCDC= Flight SFCC1（E1-3） 49VU
Ctrl Data Concentrator
FLT CNTL/SLT FLP/POS/IND 1
21CV B12
27-51-34
49VU
FLT CNTL/FLP/CTL&MONG/SYS 1
B07
C/B 49VU&121VU
49VU
FLT CNTL/SLT/CTL&MONG/SYS 1
B06
OPEN C/B 3 SEC
105VU
ELEC/HOT BUS/701PP SPLY
D01 Then CLS WAIT 1 MIN.
SFCC2（E2-3） 121VU
WTB/FLP WTB/SLT
FLT CNTL/FLP/CTL&MONG/SYS2
22CV Q21 27-51-34
105VU
ELEC/HOT BUS/702PP SPLY
E02
105VU
ELEC/HOT BUS/702PP SPLY
D02 OPEN C/B 3 SEC
121VU
FLT CNTL/SLT FLP/POS/IND2
P16
121VU
FLT CNTL/SLT/SYS2
R21 1 MIN.
122VU
FLT CNTL/WTB/FLP/SYS1
S07
121VU
FLT CNTL/WTB/FLP/SYS2
P20
122VU
FLT CNTL/WTB/SLT/SYS1
S06
121VU
FLT CNTL/WTB/SLT/SYS2
P19
WTB= Wing
Tip Brake
THS
121VU
FLT CNTL/THS/ACTR/MOT1
Q16
+（ELAC1）
49VU
FLT CNTL/THS/ACTR/MOT2
B09
121VU
FLT CNTL/THS/ACTR/MOT3
Q17
THS= Trimmable
Horizontal Stablizer
27 – FLIGHT CONTROLS NOTE：reset C/B during 10 sec at feast, unless otherwise specified ECAM WARNING
SYSTEM RESET
＊ FLAPS/SLATS FAULT C/B： FLAPS＞＞B07，Q21 SLATS＞＞B06，R21 AUTO TEST 2 SEC SEE OEB 82/3 ＊ FLAPS/SLATS LOCKED
SEE OEB 82/3
＊ SLATS AND FLAPS FAULT in conf 0 ＊ FLAP SYS 1（2）FAULT
C/B： SYS 1＞＞B7 SYS2＞＞Q21 AUTO TEST 2 SEC SEE OEB 82/3
C/B 49VU&121VU Then CLS WAIT
＊ SLAT SYS 1（2）FAULT
C/B： SYS 1＞＞B6 SYS2＞＞R21 AUTO TEST 2 SEC
FLAT TIP BRK FAULT
C/B： B7，Q21
SLAT TIP BRK FAULT
C/B： B6，R21
＊ FLAP ATTACH SENSOR
C/B： B7，Q21 AUTO TEST 2 SEC ，FOR ALL THIS RESET
＊ ELAC FAULT
HYD PRESSURE＞＞ZERO P/B ELAC 1，2 ＞＞OFF THAN ON AUTO TEST 8 SEC If not recovered，reset C/B： ELEC 1＞＞B11 ELEC 2＞＞R20 AUTO TEST 8 SEC SWITCH ON THE HYD 。PUMPS ONLY AFTER THE AUTO TEST If it was triggered after a flight，pitch trim will be regulate
SEC FAULT
PRES HYD＞＞ZERO P/B SEC 1，2 ＞＞OFF，wait 5 sec. than ON AUTO TEST 18 SEC。 If unsuccessful，reset C/B during 5 sec： SEC 1＞＞B8 SEC 2＞＞Q18 SEC 3＞＞Q19 AUTO TEST 18 SEC Wait 45 sec ， Before switch on the HYD PUMP
FCDC FAULT
HYD PRES＞＞ZERO RESET C/B： FCDC 1＞＞B10 FCDC 2＞＞Q20 AUTO TEST 3 SEC
FCDC= Flight
Control Data Concentrator
SWITCH ON THE HYD PUMPS ONLY AFTER THE AUTO TEST AUTO TEST The FCDC reset with HYD pres may triggered an warning of LAF DEGRADED
＊ ELEC 1（2）PITCH FAULT L（H）SIDESTICK FAULT
SEE RESET OF ELAC SEE RESET OF ELAC & SEC
＊ SIDESTICK PRIORITY
SEE RESET OF ELAC
ALTN LAW
May be triggered during eng start，due to electrical transient Swith OFF the G，Y and B HYD PUMPS （PARKING BRK AT ON），wait 1 min。Than reset ELAC 1 And ELAC 2 P/B，after 8 sec 。 （end of power up test indicated by disappearance of ALTN LAW Warning）switch G，Y，B， HYD PUMPS AT ON/AUTO POSITION
AIL SERVO FAULT
For all of these ECAM WARNING
＊ ELEV SERVO FAULT
Try reset of the FLT CTL COMPUTER，according to the
＊ AIL FAULT
FLT CTL ARCHITECTURE publish in QRH page 5.03
＊ L（R）ELEV FAULT
（OPS DATA）
＊ L+R ELEV FAULT ＊ STABILIZER JAM SPLR FAULT GND SPLR FAULT SPD BRK FAULT
SEE RESET OF SEC
SPD BRK DISAGREE
SEE RESET OF SEC
LAF ACCU FAULT【1】
SEE RESET OF ELAC AND SEC
SPD BRK 2（3+4）FAULT 【1】【3】
SEE RESET OF SEC
＊ L（R）SIDESTICK FAULT
SEE RESET OF ELAC AND SEC
＊ PITCH TRIM NOT IN T.O. RANGE ＊ SPEED BRK NOT RETRACTED
SEE RESET OF SEC
＊ RUD TRIM NOT IN T.O. RANGE【2】 【3】 【1】320【2】319【3】321
28 FUEL SYSTEM COMPUTER
PANEL DESIGNATION
IDNT C.B
NOTE
FLSCU 1&2（E2-1）121VU FUEL/HI/LVL/SPLY
7QJ
28-46-34
Fuel Level Sensing Cnotrol
9QJ
L25
Unit FQIC（E2-1）
APU
49VU
FUEL/FQI/CHAN/1
3QT
A13 28-42-34
121VU FUEL/FQI/CHANNEL/1 & 2
L26
121VU FUEL/FQI/CHAN/2
M27 28-42-00
121VU APU/FUEL/BLOW OFF/CTL
K39
49VU
B14
APU/FUEL/BLOW OFF/PUMP
121VU APU/FUEL/ PUMP/CTL
M38
121VU APU/APU/CTL
L42
121VU APU/ECB/SPLY
L41
121VU APU/FUEL/LP VALVE/CTL
M40
TEST PAGE：
LOW LVL
LP VALVE
PUMPS
121VU APU/FUEL/LP VALVE/SPLY
M39
49VU
FUEL/AFT LOW LVL/&OVFL WING/L
A10
49VU
FUEL/AFT LOW LVL/&OVFL WING/R
A11
121VU FUEL/FWDLOW LVL/WING/L
M22
121VU FUEL/FWDLOW LVL/WING/R
M23
49VU
FUEL/LP VALVE/MOT1/ENG1
A08
49VU
FUEL/LP VALVE/MOT1/ENG2
A09
121VU FUEL/LP VALVE/MOT2/ENG1
M25
121VU FUEL/LP VALVE/MOT2/ENG2
M26
121VU FUEL/CTR TK/AUTO/CTL
R27 OPERATION
121VU FUEL/CTR TK /PUMPS1 & 2 /CTL &
R25 TEST：
IND 121VU FUEL/CTR TK /PUMPS1 & 2 /CTL &
R26 28-21-00
IND
X FEED RFL/DFL
121VU FUEL/PUMPS/1/L CTL & R IND
AD12
121VU FUEL/PUMPS/1/R CTL & L IND
AE12
121VU FUEL/PUMPS/2/L CTL & R IND
R23
121VU FUEL/PUMPS/2/R CTL & L IND
R28
123VU FUEL/L WING TK/PUMP 1/STBY SPLY
R24
123VU FUEL/R WING TK/PUMP 1/STBY SPLY
R29
121VU FUEL/L WING TK/PUMP1 SPLY
N23
121VU FUEL/L WING TK/PUMP2 SPLY
N26
121VU FUEL/R WING TK/PUMP1 SPLY
Q23
121VU FUEL/R WING TK/PUMP2 SPLY
Q26
49VU
FUEL/X FEED/VALVE/MOT1
A12
121VU FUEL/X FEED/VALVE/MOT2
M24
121VU FUEL/RFL/DFL/SPLY
L24
121VU FUEL/RFL/DFL/XFR/DEFUEL/VALVE
L23
49VU
A14
FUEL/SMOKE/CONFIG/PUMP CTL 28 - FUEL
NOTE：reset C/B during 10 sec at feast, unless otherwise specified ECAM WARNING L（R）XFR VALVE CLOSED OR
SYSTEM RESET To close XFR valve：
OPEN 【1】 Refueling sw – ON than OFF To open XFR valves： Pull C/B：A10，A11，M11，M22，M23 then Push C/B：A10，A11，M11，M22，M23 L（R）XFR VALVE FAULT【2】
C/B：R25 & R26
XFR VALVES FAULT【2】
C/B：R25 & R26
AUTO TRANSFER FAULT 【2】
C/B：R27
FQI CH 1（2）FAULT
At exterior refuel panel： MODE SELECT - OFF At refuel coupling（if insealled）： 2 P/B REFUEL - OFF RESET C/B： FQI/CHAN 1＞＞A13 FQI/CHAN 2＞＞M27 FQI/CHAN 1 & 2＞＞26 AUTO TEST 80 SEC
【1】319 &320 【2】 321
29 HYDRAULIC POWER SYSTEM COMPUTER
PANEL
DESIGNATION
FIRE VALVE
49VU
HYD/FIRE VALVE/G/ENG 1
C13
49VU
HYD/FIRE VALVE/G/ENG 2
C14
121VU
HYDRAULIC/G HYD/PUMP ENG1/CTL
R35
121VU
HYDRAULIC/G HYD/PUMP
R34
PUMP
IDNT C.B
ENG1/MONG 121VU
HYDRAULIC/G HYD/PUMP ENG2/CTL
Q36
121VU
HYDRAULIC/G HYD/PUMP
Q37
ENG2/MONG RAT SOL VALVES
49VU
HYDRAULIC/RAT/CTL
D14
121VU
HYDRAULIC/RAT/SPLY/EXTN/SOL1
P33
121VU
HYDRAULIC/SOL
N35
VALVES/G/Y/B/LEAK/TST ELEC PUMP
IND
121VU
HYDRAULIC/SOL VALVES/G/Y/PTU
N34
123VU
B HYD/ELEC PUMP
AB09
123VU
Y HYD/ELEC PUMP/NORM
AB03
123VU
Y HYD/ELEC PUMP
AB06
121VU
HYDRAULIC/HYD POWER/Y
N30
121VU
HYDRAULIC/HYD/QTY/IND
P35
121VU
HYDRAULIC/LOW/LVL/IND
N32
49VU
HYD/HYD PWR/B WARN/&CTL
C12
49VU
HYD/HYD/PRESS/XMTR
C11
29 - HYDRAULIC NOTE：reset C/B during 10 sec at feast, unless otherwise specified ECAM WARNING
SYSTEM RESET
NOTE
＊ G（Y）（B）RSVR LO AIR PR ＊ G（Y）（B）RSVR OVHT
For Y RSVR OVHT see procedure Y ELEC PUMP OVHT described below
＊ G（Y）（B）RSVR LO LVL
C/B： HYD＞G＞＞R34，R35
＊ G（Y）（B）（B+Y）（B+G）
HYD＞Y＞＞N30，Q36，Q37
（Y+G）SYS LO PR
HYD＞B＞＞C12 HYD＞XMTR＞＞C11
Y ELEC PUMP OVHT
If the pump is continuously running and does not stop When selected OFF，it can be stopped by pulling C/B： DOOR CARGO＞＞T12（if cargo doors are open） OR Y HYD ELE PUMP＞＞AB6 Y HYD ELE PUMP NNORM＞＞AB3 （SEE MEL 29-24）
Y ELEC PUMP LO PR ＊ B ELEC PUMP OVHT ＊ B ELEC PUMP LO PR ＊ G（Y）ENG 1（2）PUMP LO PR ＊ PTU FAULT
C/B：N34
＊ RAT FAULT
C/B： P33（A319） P32 and P33（A320） P33 and D14（A321）
30 ICE & RAIN PROTECTION SYSTEM COMPUTER
PANEL DESIGNATION
IDNT C.B
PHC 1
49VU
ANTI ICE/PROBES/AOA/1
6DA1 D04 30-31-34
（DR 811/LH WALL） 49VU
ANTI ICE/PROBES/PHC/1
D03
Probe Heat
49VU
ANTI ICE/PROBES/PITOT/1
D02
Computer
122VU ANTI ICE/PROBES/1/STATIC
Z13
122VU ANTI ICE/PROBES/1/TAT
Z12
PHC 2
122VU ANTI ICE/PROBES/2/TAT
（DR 811/RH WALL） 122VU ANTI ICE/PROBES/2/PITOT
PH 3
Y14 Y13
122VU ANTI ICE/PROBES/2/PHC
Y12
122VU ANTI ICE/PROBES/2/STATIC
Y11
（DR 811/LH WALL） 122VU ANTI ICE/PROBES/3/PITOT
WHC 1
6DA2 Y15 30-31-34
122VU ANTI ICE/PROBES/2/AOA
122VU ANTI ICE/PROBES/PHC/3
6DA3 Y16 30-31-34 Y16
122VU ANTI ICE/PROBES/3/AOA
Z15
122VU ANTI ICE/PROBES/3/STATIC
Z14
122VU ANTI ICE/WINDOWS/L
NOTE
2DG1 X14 30-42-34
（DR 811/LH WALL） 122VU ANTI ICE/WHC/1
X13 CAT II
Window Heat
122VU ANTI ICE/L/WSHLD
AF10
WHC 2
122VU ANTI ICE/WINDOWS/R
2DG2 W14
（DR 811/RH WALL） 122VU ANTI ICE/WHC/2 CHECK VALVE
W13
122VU ANTI ICE/R/WSHLD
AF03
49VU
D01
ANTI ICE/RAIN/RPLNT/CAPT
122VU ANTI ICE/RAIN/RPLNT/F/O
W11
2000VU WATER SYSTEM ICE PROT CTL
D08
2000VU WATER SYSTEM ICE PROT HTR
D07
A ICE/WING/CTL
49VU
ANTI ICE/WING/CTL
C02
A ICE/WING/MONG
49VU
ANTI ICE/WING/MONG
C01
A ICE/ENG/1
122VU ANTI ICE/ENG/1
X10
A ICE/ENG/2
122VU ANTI ICE/ENG/2
W10
A ICE/PROBES/
122VU ANI ICE/PROBES/P2/T2/ENG1
Z10
122VU ANI ICE/PROBES/P2/T2/ENG1
Y10
WIPER/CAPT
122VU ANTI ICE/WIPER/CAPT
X12
F/O/WIPER
122VU ANTI ICE/F/O/WIPER
W12
SANSOR
P2/T2/ENG1 A ICE/PROBES/ P2/T2/ENG2
30 – ICE AND RAIN PROTECTION NOTE：reset C/B during 10 sec at feast, unless otherwise specified ECAM WARNING L（R）WINDOW
SYSTEM RESET RESET WHC C/B DURING 5 SEC
L（R）WINDSHIELD
WHC 1＞＞X13
L+R WINDSHIELD
WHC 2＞＞W13 AUTO TEST 5 SEC
ENG 1（2）VALVE CLSD or OPEN ICE DECTECTED SECERE ICE DECECTED DETECT FAULT WING ANTI ICE： L（R）VALVE OPEN OPEN ON GND SYS FAULT ＊ L（R）HI PR
OEB 45/4 （MSN 1852-191）
＊ CAPT（F/O）（STBY）PITOT
For all these ECAM WARNING
CAPT（F/O）（STBY）L（R）STAT
Reset the C/B of PHC，during 5 sec min
CAPT（F/O）（STBY） AOA
PHC 1＞D3
CAPT（F/O）TAT
PHC 2＞Y12
CAPT（F/O）（STBY）PROBES
PHC3＞Y16 AUTO TEST 14 sec，verity no ECAM WARING If one warning persist，proceed according the message Pull the C/B from the system with fault（see list below）and Verify that will trigger the ECAM WARNING push the C/B ECAM WARNING CAPT AOA F/O AOA STBY AOA
SYSY
AOA 1 AOA 2
STBY PITOT
F/O TAT
Z15 D2
PITOT 2
Y14
PITOT 3
Z16
STATIC 1 STATIC 2
STBY STATIC CAPT TAT
Y13
PITOT 1
CAPT STATIC F/O STATIC
D4
AOA 3
CAPT PITOT F/O PITOT
C/B
Z13 Y11
STATIC 3 TAT 1 TAT 2
Z14
Z12 Y15
AUTO TEST 14 sec
31 INDICATING RECORDING SYSTEM COMPUTER
PANEL DESIGNATION
IDNT C.B
NOTE
CFDIU（E1-4）
121VU CFDS/CFDOI/SPLY
1TW J18
31-32-34
Centralized Fault
121VU CFDS/CFDIU/BACK/UP
Display Interface DMC 1（E1-3） DMC 2（E2-3）
J17
Reset aft clock initial wait few mins 49VU
EIS/DMC1/SPLY
49VU
EIS/DMC1/SWTG
121VU EIS/DMC2/SPLY 121VU EIS/DMC2/SWTG EIS/DMC3/SWTG
1WT1 E11 E09
RVSM
1WT2 Q08 R08
DMC 3（E1-3）
49VU
Data Management
121VU EIS/DMC3/SPLY
Q09
Computer
49VU
EIS/DMC3/SPLY/SPLY
E10
SDAC 1（E1-3）
49VU
SDAC/1/SPLY
F04
49VU
SDAC/1/26VAC SYNC/AC ESS BUS
121VU EIS/SDAC/1/BUS1/26VAC SYNC AC
31-63-34
1WT3 E07
1WV1F02 Q04
31-55-34
121VU EIS/SDAC/1/BUS2/26VAC SYNC AC
Q03
SDAC 1 & 2
49VU
SDAC/1 & 2/28VDC/ESS BUS
F05
SDAC 2（E2-3）
49VU
SDAC/2/26VAC SYNC/AC ESS BUS
System Data
121VU EIS/SDAC/2/SPLY
Q06
Acquisition
121VU EIS/SDAC/2/BUS1/26VAC SYNC AC
Q05
Concentrator
121VU EIS/SDAC/2/BUS2/26VAC SYNC AC
Q02
DMU（E1-4）
121VU AIDS/DMU
1TV
K16 31-36-34
121VU RCDR/FDIU
2TV
K17 31-33-34
FWC 1（E1-3）
49VU
1WW1 F01F 31-53-34
FWC 2（E2-3）
121VU EIS/FWC2/SPLY
ECAM DU
121VU EIS/ECAM DU/LOWER/SPLY
R11
4WT1（UPR）
121VU EIS/ECAM DU/LOWER/SWTG
R10 31-63-22
4WT2（LWR）
49VU
EIS/ECAM DU/LOWER/SPLY
E05
AMM31-63-22-4000-00
49VU
EIS/ECAM DU/LOWER/SWTG
E06
ND
49VU
EIS/ND CAPT/SPLY
E01
CAT II
3WT1（CAPT）
49VU
EIS/ND CAPT/SWTG
E02
NAP-10
3WT2（F/O）
121VU EIS/PFD/F/O
R04 31-63-22
121VU EIS/ND/F/O/SWTG
R06
PFD
49VU
EIS/PFD CAPT/SPLY
E03
CAT II
2WT1（CAPT）
49VU
EIS/PFD CAPT/SWTG
E04
31-63-22
2WT2（F/O）
121VU EIS/PFD/F/O
R03
121VU CFDS/TEST PLUG/1
J19
121VU CFDS/TEST PLUG/2
J20
121VU EIS/PFD/F/O/SWTG
R05
1WV2F03
31-55-34
Data Management Unit
FDIU（E1-4） Fight Data Interface Unit
FWS/FWC1/SPLY
DRA
121VU RCDR/ACCLRM
Digital AIDS Recorder
121VU AIDS/DMU
DFDR
121VU RCDR/DFDR
LOUD/SPKR
49VU 49VU
2TV
（test with BRK ON）
49VU
CAT II
K18
CAPT/LOUD/SPKR
K16 31-33-55 7WW F10 8WW P08
EIS/RLY/BOX/CAPT
E08
121VU EIS/RLY/BOX/F/O CLOCK
CAT II RVSM
K15
121VU EIS/FO/LOUD/SPKR RLY/BOX
1WW2 F02
CLOCK/NORM/SPLY
R07 2FS
F11
OPEN J17，J18
121VU CLOCK/STBY/SPLY
N03 AFT ADJ
121VU EIS/SDAC1 & 2/BUS1/28VDC
P04
121VU EIS/SDAC1 & 2/BUS2/28VDC
P03
121VU EIS/SDAC1 & 2/DOOR/DET/AVNCS
P02
121VU EIS/SDAC1 & 2/DOOR/DET/PAX 49VU
PRINTER
P05
EIS/ECAM/CTL/PNL
6WT E12
121VU DATA/LOADER/SPLY
J16
106VU DC BUS/1 & 2/MONG
C03
106VU EMER/GEN/REF
B05
121VU PTR/SPLY
4TW J21
31 – INDICATING/RECORDING SYSTENS NOTE：reset C/B during 10 sec at feast, unless otherwise specified ECAM WARNING DMC FAULT
SYSTEM RESET Indication of respective DU’s with a cross white lin C/B：DME 1 ＞＞E9，E11 DME 2 ＞＞Q8，R8 DME 3 ＞＞E7，E10，Q9 AUTO TEST 4 SEC
＊ SDAC 1 FAULT
C/B：SDAC 1 ＞＞F2，F4，Q3，Q4
SDAC 2 FAULT
SDAC 2 ＞＞F3，Q2，Q5，Q6
＊SDAC1+2 FAULT
SDAC 1 & 2 ＞＞F5 AUTO TEST 5 SEC
＊ FWC 1 FAULT
C/B：FWC 1 ＞＞F1
FWC 1 FAULT
FWC 2 ＞＞Q7
＊ FWC 1+2 FAULT
AUTO TEST 50 SEC
DFDR FAULT
ENG 1，2 STOPPED C/B：K16 AUTO TEST 25 SEC
FDIU FAULT
ENG 1，2 STOPPED C/B：J17，J18 AUTO TEST 60 SEC
32 LANDING GEAR SYSTEM COMPUTER
PANEL
DESIGNATION
IDNT
BSCU（E2-
121VU
HYD/BRKING &
10GG M36
2）
C.B
STEERING/SYS2/SPLY 121VU
HYD/BRKING &
M35
STEERING/SYS2/CTL 121VU
HYD/BRKING &
M34
STEERING/SYS1/CTL 121VU
HYD/BRKING & STEERING/SYS1/IND &/SPLY
M33
NOTE 32-42-34
BSCU= Braking and Steering
Control Unit LGCIU（E1-
49VU
L/G/LGCIU/SYS1/NORM
5GA1
C09
2,E2-2）
121VU
HYDRAULIC/LGCIU/SYS2
5GA2
Q35
121VU
HYDRAULIC/LGCIU/SYS1/GRN
32-31-71
Q34
D SPLY LGCIU= Landing Gear Cortrol
And Interface Unit BRK FAN
121VU
HYDRAULIC/BRK
L32
FAN/WHEELS/1 & 2 121VU
HYDRAULIC/BRK
L35
FAN/WHEELS/3 & 4 PARK BRK
121VU
HYDRAULIC/BRK FAN/CTL
M32
121VU
HYDRAULIC/PARK
N36
TEST：
N37
32-45-00
BRK/CTL/NORM 121VU
HYDRAULIC/PARK BRK/CTL/STBY
BRK/TEMP
121VU
HYDRAULIC/BRK/TEMP/DET/U
M37
NIT IND
49VU
L/G/Y BRK/PRESS/IND
C10
32 – LANDING GEAR NOTE：reset C/B during 10 sec at feast, unless otherwise specified ECAM WARNING
SYSTEM RESET
＊ SHOCK ABSORBER FAULT GEAR NOT UPLOCKED
Reset C/B from LGCIU（SEE BELOW）
GEAR NOT DOWNLOCKED GEAR UPLOCK FAULT ＊ DOORS NOT CLOSED ＊ LGCIU 1（2）FAULT
C/B：LGCIU 1＞＞C9，Q34（GOR A320） LGCIU 1＞＞C9（FOR A319） LGCIU 2＞＞Q35
＊ SYS DISAGREE GEAR NOT DOWN N/W STEER FAULT
RESET C/B FROM ‘‘BSCU’’（SEE BELOW） OEB 50/12（MSN185-395）
＊ HYD SEL FAULT ＊ TYRE LO PR（IF INSTALLED）
C/B：M31
AUTO TEST 5 SEC【45 SEC IF CFDS NOT AVAILABLE】 ＊ PARKING BRAKE ON
BRAKES ＊ HOT RESET C/B FROM ‘’BSCU（SEE BELOW） ANTI SKID FAULT ANTI SKID/NWS OFF ＊ AUTOBRK FAULT
Reset C/B from BSCU （SEE BELOW） OEB 50/12（MSN185-395）
BSCU CH 1（2）FAULT（319&320）
A/C Stooped – PRAK BRAKE - ON A/SKID & N/W STRG -ON
BSCU SYS 1（2）FAULT（321）
C/B：BSCU CH 1＞＞M33，M34 BSCU CH 2＞＞M35，M36 AUTO TEST 1 SEC
33 LIGHTS SYSTEM COMPUTER
PANEL
DESIGNATION
IDN
C.B
NOTE
H04
ON A/C101-103
H04
ON A/C104-106
T 49VU
LIGHTING/STBY/COMP/LIGHT
49VU EPSU
CEILING
WINDOW
CARGO
ANN LT
49VU
LIGHTING/EMER LT/CABIN
H06
33-51-38
49VU
LIGHTING/EMER LT/CABIN
H05
ASM33-51-00
122VU
LIGHTING/ACBIN/EMER/LT
V07
SHEET-002
2000VU
CABIN LIGHT POWER-CEILING FWD
H06
2000VU
CABIN LIGHT POWER-CEILING FWD
H05
2000VU
CABIN LIGHT POWER-CEILING AFT
H08
2000VU
CABIN LIGHT POWER-CEILING AFT
H07
2000VU
CABIN LIGHT POWER-WINDOW FWD
H02
2000VU
CABIN LIGHT POWER-WINDOW FWD
H01
2000VU
CABIN LIGHT POWER-WINDOW AFT
H04
2000VU
CABIN LIGHT POWER-WINDOW AFT
H03
2000VU
AIR CONDTN COMPT OUTLET
B08
2000VU
CARGO CONMPT LIGHT-AFT
B05
2000VU
CARGO CONMPT LIGHT-FWD
B04
2000VU
CARGO CONMPT LIGHT-LDG AERA
B06
121VU
LIGHTING/ANN LT SPLY/XFMR/BUS 1
X04
121VU
LIGHTING/ANN LT SPLY/XFMR/BUS 2
X05
121VU
LIGHTING/ANN LT SPLY/XFMR/STAT
X03
INV AVINCS
FLOOD
EMER LT
122VU
LIGHTING /AVNCS COMPT/DOME
Z07
122VU
LIGHTING /AVNCS COMPT/OUT/115VAC
Z09
122VU
LIGHTING /AVNCS COMPT/OUT/28VDC
Z08
122VU
LIGHTING/CKPT/DOME
Z06
122VU
LIGHTING/FLOOD/CAPT/SIDE
Z05
122VU
LIGHTING/FLOOD/CTR INST/PNL
Z04
122VU
LIGHTING/FLOOD/F/O/SIDE
Z06
49VU
LIGHTING/EXER LT/CABIN
H07
49VU
LIGHTING/EXER LT/CKPT/DOME
H08
2000VU
LIGHTING-ATTND WORK
J05
2000VU
LIGHT-CABIN ENTRY
J04
※ READING LT 有損壞可在 CIDS 1 第 3 頁（COM 裡面查詢） COMPUTER
PANEL
DESIGNATION
IDN
C.B
T BEACON NAV LOGO RWY TAXI
122VU
LIGHTING/EXT LT/BEACON/LOWER
U03
122VU
LIGHTING/EXT LT/BEACON/UPER
U06
122VU
LIGHTING/EXT LT/NAV1 &LOGO/LT
T03
122VU
LIGHTING/EXT LT/NAV2 &LOGO/LT
T02
122VU
LIGHTING/LOGO/L
V03
122VU
LIGHTING/LOGO/R
V02
122VU
LIGHTING/EXT LT/RWY TURN OFF/L
W06
122VU
LIGHTING/EXT LT/RWY TURN OFF/R
W05
122VU
LIGHTING/EXT LT/TAXI &TAKE
W09
OFF/CTL 122VU
LIGHTING/EXT LT/TAXI &TAKE
W08
OFF/TAXI LANDING
INSTL LT
122VU
LIGHTING/EXT LT/TAXI &TAKE OFF/TO
W07
122VU
LIGHTING/L&ING LT/L/CTL
T05
122VU
LIGHTING/L&ING LT/L/SPLY
T04
122VU
LIGHTING/L&ING LT/R/CTL
T07
122VU
LIGHTING/L&ING LT/R/SPLY
T06
122VU
LIGHTING/INSTL LT/GLARE/SHLD
Y05
122VU
LIGHTING/INSTL LT/MAIN
Y04
INST/PNL&/PED 122VU WHL WELL
122VU
LIGHTING/INSTL LT/OVHD/PNL LIGHTING/WHL WELL/LTG/DOME
Y03 X08
NOTE
122VU
LIGHTING/WHL WELL/LTG/OUT
X07
122VU
LIGHTING/EXT LT/WING/& ENG SCAN/L
W02
122VU
LIGHTING/EXT LT/WING/& ENG SCAN/R
W03
STROBE
122VU
LIGHTING/WING/STROBE
V05
READING
2000VU
PASSENGER READING LIGHT
G03
2000VU
PASSENGER READING LIGHT
G07
2000VU
PASSENGER READING LIGHT
G06
2000VU
PASSENGER READING LIGHT
G05
2000VU
PASSENGER READING LIGHT
G04
2000VU
PASSENGER READING LIGHT
G02
122VU
LIGHTING/TST/BOARD/SPLY
X06
49VU
LIGHTING/XFMR/115V.5V/ESS BUS
H03
WING
34 NAVIGATION SYSTEM COMPUTER
PANEL
DESIGNATION
IDNT C.B
NOTE
ADIRU 1
49VU
NAV PROBES/ADIRU 1/& AOA 1/26VAC
1FP1 F07
34-12-34
49VU
NAV PROBES/ADIRU 1/115VAC
F06
CAT II
105VU
ADIRS/ADIRU1/28VDC
C02
RNP-10
121VU
ADIRS/ADIRU/2PWR/SHED
121VU
ADIRS/ADIRU/2/26VAC & AOA
N09
121VU
ADIRS/ADIRU/2/115VAC
N07
121VU
ADIRS/ADIRU/2/28VDC
N05
49VU
NAV PROBES/ADIRU3/PWR/SWTG
121VU
ADIRS/ADIRU/3PWR/SWTG
N10
121VU
ADIRS/ADIRU/3/26VAC & AOA
N08
121VU
ADIRS/ADIRU/3/115VAC
N06
121VU
ADIRS/ADIRU/3/28VDC
N04
ADIRU 2
ADIRU 3
1FP2 N11
RVSM
1FP3 F09
ADIRU= Air Data Inertial Reference Unit GPWS（E1-
121VU
EIS/GPWS/115VAC
1EZ
P07
121VU
EIS/GPWS/28VDC
P06
49VU
COM NAV/DME/1
2SD1 G14
121VU
COM NAV/DME/2
2SD2 K06
34-48-34
1,E2-1） DME（E1-
34-51-33
1,E2-1） DME= Distance Measuring Equipment TCAS（E2-1） 121VU
NAV/TCAS TCAS= Traffic Collision Avoidance
System
1SG
K10
34-43-34
ADF(E1-1,E2-1)49VU 121VU
NAV/ADF/1
2RP1 H14
NAV/ADF/2
2RP2 K02
34-53-31
ADF= Automatic Direction Finder ATC（E1-1,E2- 49VU
NAV/ATC/1
1SH1 G11
34-52-33
NAV/ATC/2
1SH2 K07
RVSM
NAV/ILS/1
2RT1 G12
34-36-31
NAV/ILS/2
2RT2 K09
CAT II
RA(AFT CGO) 121VU
NAV/RAD ALTM/1
25A1 K11
34-42-33
121VU
NAV/RAD ALTM/2
25A2 K12
CAT II
1SQ1 K13
34-41-33
1） 121VU
ATC=Air Traffic Control ILS(E1-3,E2-3) 49VU 121VU
RA=Radio Altimeter WX(LH WALL)121VU
NAV/RADAR/1
1SQ2 WX=Weather
Mode（ND）
VOR(E1-1,E2- 49VU
NAV/VOR/1
3RS1 G13
1)
121VU
NAV/VOR/2
3RS2 K08
RMI
122VU
LIGHT/INSTL LT/MAIN INST/PNL &/PED
21FN Y04
49VU
NAV PROBES/ADIRU3/PWR/SWTG
F09
49VU
NAV/VOR/DME/RMI
F13
49VU
NAV/STBY/ALTM
F14
49VU
NAV/STBY/HORIZON
F12
34-55-31
RMI= Radio Magnetic Indicator 34 - NAVIGATION NOTE：reset C/B during 10 sec at feast, unless otherwise specified ECAM WARNING HDG/ATT/ALTI DISCREPANCY
SYSTEM RESET At CDU of ADRIS select OFF the respective IR（1,2,3,）
ADR FAULT
During 15 sec,and then select NAV AUTO TEST—5sec + aligment
IR FAULT
If unsuccessful reset C/B during 15 sec for A319,A320 C/B：ADIRU 1＞＞F6，F7
HDG= Heading
ADIRU 2＞＞N5，N7，N9，N11
ATT= Attitude
ADIRU 3＞＞N4，N6，N8，N10
ALTI=ALTITUTE
For A321 C/B：ADIRU 1＞＞F6，F7 ADIRU 2＞＞N4，N6，N8，N10 ADIRU 3＞＞N3，N5，N7，N9 AUTO TEST 5 SEC
RA 1（2）FAULT
C/B：RA 1＞＞K11 RA 2＞＞K12 AUTO TEST 5 SEC
ILS（MMR【Multi-Mode Receiver】）1（2）FAULT C/B：ILS（MMR）1＞＞G12 ILS（MMR）2＞＞K9（L7 for A321） AUTO TEST 5SEC GPWS FAULT
C/B：P6，P7 AUTO TEST 5 SEC
TCAS FAULT（IF INSTALLED）
C/B：K10
OVER SPEED PRED W/S DET FAULT（IF INSTALLED） GPS1（2）FAULT（IF INSTALLED） FM/GPS POS DISAGREE（IF INSTALLED） GPWS TERR DET FAULT（IF INSTALLED） FLIGHT/CONTROR ＊ ADR DISAGREE ＊ IR DISAGREE
Air Data Referance Inertial Referance
35 OXYGEN SYSTEM COMPUTER
PANEL
DESIGNATION
49VU
OXYGEN/PASSEN
IDNT C.B HA08
GER/ACTUATION 49VU
OXYGEN/PASSEN
HA07
GER/ACTUATION 49VU
OXYGEN/PASSEN
HA06
GER/ACTUATION 49VU
OXYGEN/PASSEN
HA05
GER/ACTUATION 49VU
OXYGEN/PASSEN
HA04
GER/CTL & WARN 49VU
OXYGEN/PASSEN
HA03
GER/CTL & WARN 49VU
OXYGEN/PASSEN
HA02
GER/CTL & WARN 49VU
OXYGEN/CREW/O XY/SPLY
HA01
NOTE
REF
℃
-10
0
10
20
30
40
50
TEMPER
℉
14
32
50
68
86
104
122
656 681
706
731
756
781
806
926
959
992
1024 1057
ATURE
MIN＊＊ BOTTLE 2 CREW PRESSUR MEMBERS E （PSI）
861 2 CREW MEMBERS +1 OBS 1090 2 CREW MEMBERS +2 OBS AMM 35-10-00-991-00800-06-B/SHEET 1
893
1132 1173 1215 1256 1298 1339
36 PNEUMATIC SYSTEM
L/R WING LOOP
COMPUTER
PANEL
DESIGNATION
IDNT
C.B
NOTE
BMC 1(E1-3)
49VU
AIR BLEED/ENG 1/CTL
1HA1
D12
36-11-34
※ BLD TEMP
49VU
AIR BLEED/ENG 1/MONG
122VU
AIR BLEED/ENG 2/CTL
122VU
AIR BLEED/ENG 2/MONG
49VU
AIR BLEED/X FEED/VALVE/BAT
49VU
AIR BLEED/ENG 1/CTL
D12
49VU
AIR BLEED/ENG 1/MONG
D11
122VU
AIR BLEED/ENG 2/CTL
Z23
122VU
AIR BLEED/ENG 2/MONG
Z22
122VU
AIR BLEED/X FEED
Z20
D11
200+/-15 度 BMC 2(E2-3)
X FEED
1HA2
Z23 Z22
6HV
D13
VALVE
VALVE/NORM 36 - PNEUMATIC NOTE：reset C/B during 10 sec at feast, unless otherwise specified ECAM WARNING
SYSTEM RESET
BLEED 1（2）OFF ENG1 （2）BLEED FAULT
Reset C/B From BMC（see below） Oeb 100-3（MSN 185-395）
ENG1（2）BLEED NOT CLSD
Reset C/B From BMC（see below）
ENG 1（2）BLEED ABNORM PR APU BLEED FAULT
Reset C/B From BMC（see below）
＊ L（R）WING LEAK ＊ ENG 1（2）BLEED LEAK APU BLEED LEAK
Reset C/B From BMC（see below）
XBLEED FAULT
Reset C/B From BMC（see below）
ENG HP VALVE FAULT
Reset C/B From BMC（see below）
＊ L（R）WING LEAK DET FAULT ENG 1（2）（1+2）BLEED LOO TEMP ＊ MONITORING FAULT
Reset C/B From BMC（see below） C/B：BMC 1＞＞D11，D12 BMC 2＞＞Z22，Z23 AUTO TEST 22 sec
49 AIRBOIRNE AUXLARY POWER SYSTEM COMPUTER
PANEL DESIGNATION
IDNT
C.B
121VU
APU/APU/CTL
L42
121VU
APU/ECS/SPLY
L41
121VU
APU/OIL/HTR/SPLY
K41
NOTE
52 DOOR SYSTEM COMPUTER
PANEL DESIGNATION
IDNT
SLIDES
121VU
EIS/SLIDES/ARM & WARN/FLT
P11
121VU
EIS/SLIDES/SRM & WARN/GND
P10
DOOR
122VU
DOORS/PAX/XONG(COCKPIT DOOR)
當 CKPT DOOR LT
122VU
DOORS/CARGO
1MQ
亮，reset T13 等 sensor 冷卻
防 暴 門 密 碼：0 7 6 3 #
49 – AUXILIARY POWER UNIT NOTE：reset C/B during 10 sec at feast, unless otherwise specified ECAM WARNING AUTO（EMER）SHOUTDOWN
SYSTEM RESET RESET C/B：APU STOPPED APU MASTER SW ＞OFF RESER C/B ：L41，L42 AUTO TEST 3 sec
52 – DOOR NOTE：reset C/B during 10 sec at feast, unless otherwise specified ECAM WARNING ＊ L（R）FWD（AFT）AVIONICS ＊ CABIN(EMER EXIT) (CARGO) ＊ STAIRS【IF INSTALLED】
SYSTEM RESET
C.B
NOTE
T13
CODE：0763#
T12
密
（70）ENGINE SYSTEM COMPUTER PANEL DESIGNATION
IDNT
C.B
NOTE
EIU 1(E1-3) 49VU
1KS1
A04
73-25-34
121VU ENG/ENG 1/FDEC B/& EIU 1
R41
+A03
121VU ENG/IGN/ENG1/SYS B
P41
IGN SYS A
121VU ENG/IGN/ENG 1/SYS A BAT
P39
EIU 2(E2-3) 49VU
FUEL SOV OIL
ENG/1/FADEC A/& EIU 1
ENG/1/FADEC A/& EIU 2
1KS2
A05
121VU ENG/ENG 2/FDEC B
Q40
121VU ENG/IGN/ENG2/SYS B
P42
121VU ENG/IGN/ENG 2/SYS A BAT
P40
49VU
ENG/1/HP FUEL SOV
A01
49VU
ENG/2/HP FUEL SOV
A02
121VU ENG/ENG 1/OIL/PRESS&REV SNSR/CHAN A
N40
121VU ENG/ENG 2/OIL/PRESS&REV SNSR/CHAN A
N42
121VU ENG/ENG1/OIL/QTY
N39
121VU ENG/ENG2/OIL/QTY
N41
121VU ENG/ENG 1& 2/EVMU
R44
121VU ENG2/REV/LOCK
N45
121VU ENG1/REV/LOCK
N44
ON A/C 105-106
當 galley 水量小時,用 MCDU＞CFDS＞TEST＞EIU1＞EISCRETE OUTPUT＞APU BST。 70 - ENGINES NOTE：reset C/B during 10 sec at feast, unless otherwise specified ECAM WARNING
SYSTEM RESET
＊ FUEL FILTER CLOG
RESET’’ SDAC’’
＊ OIL FILTER CLOG
RESET’’ SDAC’’
HP FUEL VALVE
RESET C/B：ENG 1＞A1
ENG 2＞A2
＊ OIL LO PR
RESET C/B：ENG 1＞N40
ENG 2＞N42
IGN FAULT
RESET C/B：ENG 1＞P39，P41
＊ IGN A+B FAULT
ENG 2＞P40，P42 If unsuccessful reset FADEC’S（see procedure）
＊ FUEL CTL FAULT
For all of thes messages reset FADEC’S
REVERSER FAULT
（see procedure）
＊ REV PRESSURIZED REV SWITCH FAULT ＊ REVERSE UNLOCKED EIU FAULT ＊ OIL HI TEMP N1/N2/EGT OVERLIMIT
＊ N1/N2/EGT FF DISCREPANCY LOW N1 START VALVE FAULT START FAULT ENG DUAL FAILURE ENG FAIL ENG SHUT DOWN ONE TLA FAULT ＊ THR LEVER FAULT ＊ THR LEVER DISAGREE FLEX TEMP NOT SET ENG STALL ＊ COMPRESOR VANE ＊ OVSPD PROT FAULT
If the warning is triggered during eng start, shutdown the eng,And restar. If the warning is still present, shutdown the eng. Before calling maintenance, perfirm a reset of FADEC C/B’s During 2 min, and then make a third attempt. C/B：ENG 1 FADEC A ＞A4 ENG1 FADEC B ＞R41 ENG 2 FADEC A ＞A5 ENG 2 FADEC B ＞Q40
CTL VALVE FAULT【1】 CTL VALVE FAULT【2】 ＊ SENSOR/PROBES FAULT 【1】A320-211 【2】A320-214，A319，A321 BLEED STATUS FAULT
C/B：BMC 1＞D11，D12 BMC 2＞Z22，Z23 AUTO TEST 10 sec
＊ FADEC A（B）FAULT
ENG 1，2 STOPPED
＊ FADEC FAULT
ENG GWD PWR 1，2 P/B－OFF
Full Authorty Digital Engine Control
RESET C/B DURING 2 min C/B：ENG 1 FADEC A ＞A4 ENG1 FADEC B ＞R41 ENG 2 FADEC A ＞A5 ENG 2 FADEC B ＞Q40 AUTO TEST 2 sec
FADEC HI TEMP ＊ FADEC ALTERNATOR VIB SYS FAULT
THRUST LOCKED【1】＊ TYPE DISAGREE 【319】
