A319 & 320 Fault Verification Guide
April 26, 2017 | Author: Marcos Braga | Category: N/A
Short Description
Airbus Maintenance Task...
Description
BSBMW PISTA CI RCUI T BRE AKE R A319/320
RE F AMM 24-50-00-001
C I R C UI T BR E AK E R A319/320 P AN E L DE SI G N AT I O N
C I R C UI T BR E AK E R A319/320 LO C
AI R C O NDI T I O NI NG SYST E M
P AN E L DE SI G N AT I O N
LO C
122VU AIR COND/FLOW/MIXER/FLAP
V22
122VU AIR COND/FLOW/CTL & IND 2
V21
49VU AIR COND/RAM/AIR/INLET
D10
49VU AIR COND/CAB/PRESS CTL 1
D09
123VU AVNCS VENT/BLOWER FAN
AD10
49VU AIR COND/AVNCS VENT/CTL
D06
123VU AVNCS VENT/EXTC FAN
AE02
49VU AIR COND/FLOW/CTL & IND 1
D07
49VU AIR COND/AVNCS VENT CTL
D05
122VU AIRCO/LAV/GALL VENT CTL EXTR. FAN CTL
U21
122VU AIRCO/LAV/GALL VENT CTL EXTR. FAN SPLY
U19
49VU AUTO FLIGHT/FCU 1
B05
122VU AIR COND/ZONE TEMP CTL/28VDC/SYS 2
V20
49VU AUTO FLIGHT/FAC 1/28 VDC
B04
122VU AIR COND/ZONE TEMP CTL/28VDC/SYS 1
V19
49VU AUTO FLIGHT/FAC 1/26 VAC
B03
122VU AIR COND/ZONE TEMP CTL/115VAC/SYS 2
V18
49VU AUTO FLIGHT/FMGC/1
B02
122VU AIR COND/ZONE TEMP CTL/115VAC/SYS 1
V17
49VU AUTO FLIGHT/MCDU/1
B01
122VU AIR COND/PACK TEMP/CTL SYS1/2/115VAC
W22
122VU AIR COND/PACK TEMP/CTL SYS1/2/28VDC
W21
121VU AUTO FLIGHT/FCU 2
M21
122VU AIR COND/RECIRC FAN/R/CTL
W20
121VU AUTO FLIGHT/RUDDER/TRIM/IND
M20
122VU AIR COND/RECIRC FAN/R/SPLY
W18
121VU AUTO FLIGHT/FAC 2/ 28 VDC
M19
122VU AIR COND/PACK TEMP/CTL SYS 1/115VAC
X22
121VU AUTO FLIGHT/FAC 2/ 26 VAC
M18
122VU AIR COND/PACK TEMP/CTL SYS 1/28VDC
X21
121VU AUTO FLIGHT/FMGC 2
M17
122VU AIR COND/RECIRC FAN/L/CTL
X20
121VU AUTO FLIGHT/MCDU 2
N20
122VU AIR COND/RECIRC FAN/L/SPLY
X18
121VU AUTO FLIGHT/RUDDER/ARTF/FEEL
N17
122VU AIR COND CABIN PRESS./CTL/MAN
Y23
121VU AUTO FLIGHT/STICK//LOCK
N16
122VU AIR COND/CABIN PRESS./CTL 2
Y22
122VU AIR COND/PACK TEMP CTL SYS 2/2/28VDC
Y21
122VU AIR COND/PACK TEMP CTL SYS 2/2/115VAC
Y20
122VU AIR COND/PACK TEMP CTL SYS 2/1/28VDC
Y19
49VU COM/CVR/SPLY
E14
122VU AIR COND/PACK TEMP CTL SYS 2/1/115VAC
Y18
49VU COM/CVR/CTL
E13
49VU COM/RMP 1
G10
122VU AIR COND/AVNCS/VENT/MONG
Y17
AUT O F L I G H T
C O M M UNI C AT I O N
CIRCUIT BREAKER A319/320
CIRCUIT BREAKER A319/320
PAN EL DESI GN ATION
LO C
PAN EL DESI GN ATION
LO C
49VU
COM/VHF 1
G09
121VU
COM NAV/CIDS/DEU A NORM/R MID MZA/MZF
M12
49VU
COM/ÁUDIO/FLT/INTPH
G08
121VU
COM NAV/CIDS/DEU A NORM/L MID MZA/MZF
M11
49VU
COM/AUDIO/ACP/F/O
G07
121VU
COM NAV/CIDS/DEU A NORM/R FWD MZA/MZF
M10
49VU
COM/AUDIO/ACP/CAPT
G06
121VU
COM NAV/CIDS/DEU A NORM/L FWD MZA/MZF
M09
49VU
COM/CIDS/DEU A ESS/LINE 2
G05
121VU
COM NAV/CIDS/DEU B/NORM MZA/MZF
M08
49VU
COM/CIDS/DEU A ESS/LINE 1
G04
121VU
COM NAV/CIDS/PROG &/TST PNL MZA/MZF
M07
49VU
COM/CIDS DEU B/ESS
G03
121VU
COM NAV/CIDS/DIR NORM 2 MZA/MZF
M06
49VU
COM/CIDS/DIR 1 AND 2 ESS MZG
G02
121VU
COM NAV/CIDS/DIR NORM 1 MZA/MZF
M05
49VU
COM DIR ESS 2 PT-MZA/MZF
G02
121VU
COM/CIDS/FWD ATTND/PNL MZA/MZF
Q14
49VU
COM DIR ESS 1 PT-MZA/MZF
G01
121VU
SATCOM MZG/MZJ
K01
49VU
COM HF 1
HA14
121VU
COM NAV/CIDS/FWD ATTND/PNL MZG/MZJ
Q14
121VU
COM NAV/RMP 3
L03
121VU
COM NAV/VHF 2
L02
121VU
COM NAV/VHF 3
L05
121VU
COM NAV/CIDS/FWD ATTND/PNL MZG/MZH
M14
121VU
COM NAV/CIDS/DEU A NORM/R AFT MZG/MZJ
M13
121VU
COM NAV/CIDS/DEU A NORM/L AFT MZG/MZJ
M12
121VU
COM NAV/CIDS/DEU A NORM/R MID MZG/MZJ
M11
49VU
ELEC/LT/CTL
H10
121VU
COM NAV/CIDS/DEU A NORM/L MID MZG/MZJ
M10
49VU
ELEC/AC BUS/8XP/MONG
H11
121VU
COM NAV/CIDS/DEU A NORM/R FWD MZG/MZJ
M09
121VU
COM NAV/CIDS/DEU A NORM/L FWD MZG/MZJ
M08
105VU
ELEC/CSM/G/EV AUTO/SPLY
C01
121VU
COM NAV/CIDS/DEU B NORM MZG/MZJ
M07
105VU
ELEC/HOT BUS/702PP SPLY
D02
121VU COM NAV/CIDS/PROG AND TEST PNL MZG/MZJ
M06
105VU
ELEC/HOT BUS/701PP SPLY
D01
121VU
COM NAV/CIDS/DIR 1 AND 2/NORM MZG/MZJ
M05
105VU
ELEC/HOT BUS/702PP SPLY
E02
121VU
COM NAV/SELCAL
M04
105VU
ELEC/HOT BUS/701PP SPLY
E01
121VU
COM NAV/ACP/THIRD/OCCPNT
M02
105VU
ELEC/ STATIC INV/CNTOR/CTL
G02
121VU
EIS/HORN/SPLY
P09
105VU
ELEC/STAT INV/BUS 901XP SPLY
H02
121VU
COM NAV/CIDS/DEU A NORM/R AFT MZA/MZF
M14
105VU
ELEC/BAT BUS/REF/BCL 1
AS01
121VU
COM NAV/CIDS/DEU A NORM/L AFT MZA/MZF
M13
105VU
ELEC/BAT BUS/REF/BCL 2
AS01
E L E T R I C AL P O W E R
CIRCUIT BREAKER A319/320
CIRCUIT BREAKER A319/320
PAN EL DESI GN ATION
LO C
PAN EL DESI GN ATION
LO C
105VU
ELEC/BAT REF/BCL 1
AS01
122VU
ELEC/REFLNG/ON/BAT
U28
105VU
ELEC/BAT REF/BCL 2
AS01
122VU
ELEC/CNTOR/DC BUS/TIE 1/FAULT
U24
122VU
ELEC/AC PWR/SVCE/CTL
V29
106VU
AC ESS BUS/STBY/CNTOR/CTL
B08
122VU
ELEC/BUS/2XP/CTL
V27
106VU
AC ESS BUS/EMER/CNTOR/CTL
B07
122VU
ELEC/AC/BUS 1/CTL
V25
106VU
26VAC/ESS BUS/SPLY
B06
122VU
ELEC/TR 2/FAULT/DC BUS TIE/CONFIG
W30
106VU
CSM/G/EV/MAN/SPLY
B04
122VU
ELEC/TR 1/FAULT/DC BUS TIE/CONFIG
W29
106VU
AC ESS/BUS NORM/CNTOR/CTL
B03
122VU
ELEC/CNTOR/ESS/DC BUS/TIE
W26
106VU
AC ESS/BUS/EMER/CNTOR/SPLY
C08
122VU
ELEC/CNTOR/DC BUS/TIE
W25
106VU
EMER/SHED/CNTOR/SPLY
C07
122VU
ELEC/EXT PWR/LT CLT/AVAIL
X31
106VU
AC ESS BUS/EMER/STBY/CNTOR/SPLY
C06
122VU
ELEC/EXT PWR/LT CLT/NOT IN/USE
X30
106VU
AC ESS BUS/MONG/SPLY
C05
122VU
ELEC/EXT PWR/CTL
X29
106VU
AC/SHED/ESS BUS/CNTOR/CTL
C04
122VU
ELEC/EXT PWR/COCKPIT/AVAIL/LT
X28
106VU
ESS TR/CNTOR/CTL
C02
122VU
ELEC/TR 2/MONG
X26
106VU
ESS TR/SPLY
AS01
122VU
ELEC/TR 1/MONG
X25
122VU
ELEC/DC/SVCE/BUS
X24
122VU
ELEC/GALLEY/CNTOR
S28
122VU
APU GEN/EGIU 2/28VDC
Y31
122VU
ELEC/REFLNG/NORM
S27
122VU
GEN 2/EGIU 2/28VDC
Y30
122VU
ELEC/GEN 2/OFF/BTC 2 SPLY
T31
122VU
ELEC/APU/GCU
Y25
122VU
ELEC/GEN 1/OFF/BTC 2 SPLY
T30
122VU
ELEC/GPCU
Y24
122VU
ELEC/GEN 2/OFF/BTC 1 SPLY
T29
122VU
ELEC/EXT PWR/EGIU 1/28VDC
Y31
122VU
ELEC/GEN 1/OFF/BTC 1 SPLY
T28
122VU
ELEC/GEN 1/EGIU 1/28VDC
Z30
122VU ELEC/GCU 2
T27
122VU
ELEC/EMER AUTO 2
Z26
122VU
ELEC/GCU 1
T26
122VU
ELEC/EMER GEN AUTO 1
Z25
122VU
ELEC/IDG 2/DISC
T25
122VU
ELEC/DC BUS/TIE 2/APU START
W31
122VU
ELEC/IDG 1/DISC
T24
122VU
ELEC/GALY & CAB CTL
S26
122VU
ELEC/DC SVCE/BUS/ON TR 2
U30
122VU
ELEC/GALY & CAB/FAULT/LT CTL
S25
122VU
ELEC/RFL/SPLY/LOGIC
U29
122VU
ELEC/GALY & CAB/GND/FLT/LOGIC
S24
CIRCUIT BREAKER A319/320
CIRCUIT BREAKER A319/320
PAN EL DESI GN ATION
LO C
PAN EL DESI GN ATION
LO C
122VU
ELEC/DC SHED BUS/CNTR
U26
123VU
AFT GALLEY/FEEDER B
AD09
122VU
ELEC/AC SHED BUS/CNTR
U25
123VU
MAIN FWD GALLEY/FEEDER C
AE10
123VU
SHED BUS/218XP/220XP SPLY
AC02
123VU
GALLEY PWR –E-
AE10
123VU
APU GEN/EGIU 2/115VAC
AA08
124VU
SVCE/601PP/602PP/SPLY
BB01
123VU
EXT PWR/EGIU 1/115VAC
AA07
124VU
TR 2/CNTOR/SPLY
BC01
123VU
SVCE/BUS 2/214XP SPLY
AA05
124VU
DC SVCE/602PP/SPLY
BD01
123VU
BUS 1/131XP-A/SPLY
AB12
124VU
206PP/208PP/SPLY
BE01
123VU
BUS 1/103XP/SPLY
AB11
124VU
204PP/SPLY
BF01
123VU
TR 1/SPLY
AB10
124VU
202PP/SPLY
BG01
123VU
TR 2/SVCE/BUS 2/SPLY
AB08
124VU
SHED BUS 210PP/212PP/SPLY
BA01
123VU
GND/PWR/PROT
AB07
123VU
SVCE/BUS 2/212XP SPLY
AB05
125VU
BAT BUS/301PP/SPLY
CC01
123VU
TR 2/214XP/SPLY
AB04
125VU
101PP/SPLY
CD01
123VU
BUS 2/204XP/SPLY
AB02
125VU
103PP/SPLY
CE01
123VU
BUS 2/213XP-A/SPLY
AB01
125VU
TR 1/CNTOR/SPLY
CF01
123VU
AC ESS/BUS ON/BUS 1
AC12
123VU
AC ESS/BUS ON/BUS 2
AC01
123VU
BUS 1/101XP/SPLY
AD11
123VU
GALLEY D
AD04
122VU
COCKPIT SEATS/SEAT CTL/F/O
U14
123VU
BUS 2/212XP/SPLY
AD03
122VU
COCKPIT SEATS/SEAT CTL/CPT
U11
123VU
BUS 2/202XP/SPLY
AD02
2001VU VACUUM CLEANER SOCKET CARGO Z0261
123VU
GEN 1/EGIU 1/115VAC
AF12
123VU
BUS 1/110XP/SPLY
AF11
123VU
BUS 2/210XP/SPLY
AF02
123VU
GEN 2/EGIU 2/115VAC
AF01
49VU
ENGINE 2/FIRE DET./LOOP B
A07
123VU
MAIN FWD GALLEY FEEDER F
AC10
49VU
ENGINE 1/FIRE DET./LOOP A
A06
123VU
MAIN AFT GALLLEY FEEDER A
AF04
49VU
AIR COND/SDCU/CHAN 1
C06
E Q UI P M E NT /F UR NI SH I NG S SYST E M
F01
F I R E P R O T E C T IO N SYST E M
CIRCUIT BREAKER A319/320
CIRCUIT BREAKER A319/320
PAN EL DESI GN ATION
LO C
PAN EL DESI GN ATION
LO C
121VU
APU/FIRE AND OVHT/DET/LOOP B
L44
105VU
FLT CTL/ELAC 1/STBY SPLY
A01
121VU
APU/FIRE AND OVHT/DET/LOOP A
L43
105VU
FLT CTL/SEC 1/STBY SPLY
B01
121VU
APU/AUTO/EXTIG/GND/TEST
L40
121VU
APU/FIRE/EXTIG/SQUIB B
L39
121VU
FLIGHT CONTROLS/WTB/FLP/SYS 2
P20
121VU
APU/FIRE/EXTIG/SQUIB A
L38
121VU
FLIGHT CONTROLS/WTB/SLT/SYS 2
P19
121VU
APU/FIRE/LP VALVE/NORM
M42
121VU
FLIGHT CONTROLS/SLT/PS/IND 2
P16
121VU APU/FIRE/LP VALVE/STBY
M41
121VU
FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS 2
Q21
121VU
ENGIN/ENG 1 AND 2 FIRE EXTIG/BTL 1/SQUIB B
Q44
121VU
FLIGHT CONTROLS/FCDC 2/SPLY
Q20
121VU
ENGIN/ENG 1 AND 2 FIRE EXTIG/BTL 1/SQUIB A Q43
121VU
FLIGHT CONTROLS/SEC 3/SPLY
Q19
121VU
ENGIN/ENG 1 AND 2 FIRE EXTIG/BTL 2/SQUIB B
Q42
121VU
FLIGHT CONTROLS/SEC 2/SPLY
Q18
121VU
ENGIN/ENG 1 AND 2 FIRE EXTIG/BTL 2/SQUIB A Q41
121VU
FLIGHT CONTROLS/THS ACTR/MOT 3
Q17
121VU
ENGINE/ENG 2/FIRE DET/LOOP A
Q39
121VU
FLIGHT CONTROLS/THS ACTR/MOT 1
Q16
121VU
ENGINE/ENG 1/FIRE DET/LOOP B
Q38
121VU
FLIGHT CONTROLS/SLT/CTL/SYS 2
R21
121VU
FLIGHT CONTROLS/ELAC 2/NORM/SPLY
R20
122VU
AIR COND/SDCU/CHAN 2
T18
122VU
AIR COND/CARGO/FIRE/EXTIG
T19
122VU
FLIGHT CONTROLS/WTB/FLP/SYS 1
S07
122VU
FLIGHT CONTROLS/WTB/SLT/SYS 1
S06
F L I G H T C O NT RO L S SYT E M F UE L SYST E M 49VU
FLIGHT CONTROLS/SLT FLP/POS IND 1
B12
49VU
FUEL/SMOKE/CONFIG/PUMP CTL
A14
49VU
FLIGHT CONTROLS/ELAC 1/NORM/SPLY
B11
49VU
FUEL FQI CHAN 1
A13
49VU
FLIGHT CONTROLS/FCDC 1/SPLY
B10
49VU
FUEL/X FEED/VALVE/MOT 1
A12
49VU
FLIGHT CONTROLS/THS/ACTR/MOT 2
B09
49VU
FUEL/X FR VALVE 1/WING R
A11
49VU
FLIGHT CONTROLS/SEC 1/NORM/SPLY
B08
49VU
FUEL/X FR VALVE 1/WING L
A10
49VU
FLIGHT CONTROLS/FLP/CTL AND MONG/SYS 1
B07
49VU
FUEL/LP VALVE/MOT 1/ENG 2
A09
49VU
FLIGHT CONTROLS/SLT/CTL AND MONG/SYS 1
B06
49VU
FUEL/LP VALVE/MOT 1/ENG 2
A08
49VU
APU/FUEL/BLOW OFF/PUMP
B14
105VU
FLIGHT CONTROLS/ELAC 2/STBY SPLY
A02
CIRCUIT BREAKER A319/320
CIRCUIT BREAKER A319/320
PAN EL DESI GN ATION
LO C
PAN EL DESI GN ATION
LO C
121VU
APU/FUEL/BLOW OFF/CTL
K39
123VU
L WING TK/PUMP 1/STBY SPLY
AD12
121VU
FUEL FQI CHANNEL 1 AND 2
L26
123VU
R WING TK/PUMP 1/STBY SPLY
AE12
121VU
FUEL/HI/LVL/SPLY
L25
121VU
FUEL/RFL/DFL/SPLY
L24
121VU
FUEL/RFL/DFL/XFR/DEFUEL/VALVE
L23
121VU
APU/FUEL/LP VALVE/CTL
M40
49VU
HYD/FIRE VALVE/Y/ENG 2
C14
121VU
APU/FUEL/LP VALVE/SPLY
M39
49VU
HYD/FIRE VALVE/G/ENG 1
C13
121VU
APU/FUEL/PUMP/CTL
M38
49VU
HYD/RAT/CTL
D14
121VU
FUEL FQI CHANN 2
M27
49VU
HYD/HYD POWER/B WARN & CTL
C12
121VU
FUEL/LP VALVE/MOT 2/ENG 2
M26
49VU
HYD/HYD/PRESS XMTR
C11
121VU
FUEL/LP VALVE/MOT 2/ENG 1
M25
121VU
FUEL/X FEED/VALVE/MOT 2
M24
121VU
HYDRAULIC/SOL VALVES/G/Y/B/LEAK TEST
N35
121VU
FUEL/X FR VALVE 2/WING R
M23
121VU
HYDRAULIC/SOL VALVES/G/Y/PTU
N34
121VU
FUEL/XFR VALVE 2/WING L
M22
121VU
HYDRAULIC/LOW/LVL/IND
N32
121VU
FUEL/L WING TK/PUMP 2 SPLY
N26
121VU
HYDRAULIC/HYD POWER Y
N30
121VU
FUEL/L WING TK/PUMP 1 SPLY
N23
121VU
HYDRAULIC/HYD/QTY IND
P35
121VU
FUEL/R WING TK/PUMP 2 SPLY
Q26
121VU
HYDRAULIC/RAT/SPLY/EXTN/SOL 1
P33
121VU
FUEL/R WING TK/PUMP 1 SPLY
Q23
121VU
HYDRAULIC/Y HYD/PUMP ENG 2/MONG
Q37
121VU
FUEL/PUMPS 2 R CTL AND L IND
R29
121VU HYDRAULIC/Y HYD/PUMP ENG 2/CTL
Q36
121VU
FUEL/PUMPS 1 R CTL AND L IND
R28
121VU
HYDRAULIC/G HYD/PUMP ENG 1/CTL
R35
121VU
FUEL/PUMPS 2 L CTL AND R IND
R24
121VU
HYDRAULIC/G HYD/PUMP ENG 1/MONG
R34
121VU
FUEL/PUMPS 1 L CTL AND R IND
R23
121VU
FUEL/CTR TK/PUMP 2 SPLY
P26
123VU
B HYDRAULIC/ELEC PUMP
AB09
121VU
FUEL/CTR TK/PUMP 1 SPLY
P23
123VU
Y HIDRAULIC/ELEC/PUMP
AB06
121VU
FUEL/CTR TK/PUMP/AUTO/CTL
R27
123VU
Y HIDRAULIC/ELEC/ELEC PUMP NORM
AB03
121VU
FUEL/CTR TK/PUMPS 1 AND 2 CTL AND IND
R26
121VU
FUEL/CTR TK/PUMPS 1 AND 2 CTL AND IND
R25
H I DR AUL I C P O W E R SYST E M
CIRCUIT BREAKER A319/320 PAN EL DESI GN ATION
CIRCUIT BREAKER A319/320 LO C
ICE AND RAIN PROTECTION SYS
PAN EL DESI GN ATION
LO C
122VU
Z10
ANTI ICE/PROBES/P 2/T 2/ENG 1
122VU ANTI ICE/PROBES 2/PHC 49VU
ANTI ICE/PROBES AOA 1
D04
49VU
ANTI ICE/PROBES PHC 1
D03
49VU
ANTI ICE/PROBES PITOT 1
49VU
ANTI ICE/RAIN/RPLNT/CAPT
49VU 49VU
Y12
122VU
ANTI ICE/RAIN/RPLNT/F.O –MZC/MZF/MZG/MZJ W11
D02
123VU
ANTI ICE WINDSHIELD L
AF10
D01
123VU ANTI ICE WINDSHIELD R
AF03
ANTI ICE/WING CTL
C02
2000VU WATER SYSTEM ICE PROT CTL
D08
ANTI ICE/WING/MONG
C01
2000VU WATER SYSTEM ICE PROT HTR
D07
122VU
ANTI ICE/WINDOWS R
W14
122VU
ANTI ICE/WHC 2
W13
122VU
ANTI ICE/FIRST OFFICER WIPER
W12
49VU
EIS/ECAM/CTL/PNL
E12
122VU
ANTI ICE/ENG 2
W10
49VU
EIS/DMC 1/CTL/SPLY
E11
122VU
ANTI ICE/WINDOWS L
X14
49VU
EIS/DMC 3/STBY/SPLY
E10
122VU
ANTI ICE/WHC 1
X13
49VU
EIS/DMC 1/SWTG
E09
122VU
ANTI ICE/ CAPT WIPER
X12
49VU
EIS/RLY/BOX/CAPT
E08
122VU
ANTI ICE/ENG 1
X10
49VU
EIS/DMC 3/SWTG
E07
122VU
ANTI ICE/PROBES/PHC 3
Y16
49VU
EIS/ECAM DU/UPPER/SWTG
E06
122VU
ANTI ICE PROBES
Y15
49VU
EIS/ECAM DU/UPPER/SPLY
E05
122VU
ANTI ICE PROBES
Y14
49VU
EIS/PFD CAPT/SWTG
E04
122VU
ANTIICE PROBES 2/AOA
Y13
49VU
EIS/PFD CAPT/SPLY
E03
122VU
ANTI ICE/PROBES AND SENSORS 2/STATIC
Y11
49VU
CLOCK/NORM/SPLY
F11
122VU
ANTI ICE/PROBES AND SENSORS 3/PITOT
Z16
49VU
CAPT/LOUD SPKR
F10
122VU
ANTI ICE/PROBES 3/AOA
Z15
49VU
SDAC 1 AND 2/28VDC/ AC ESS BUS
F05
122VU
ANTI ICE/PROBES
Z14
49VU
SDAC 1/SPLY
F04
122VU
ANTI ICE/PROBES AND SENSORS 1/STATIC
Z13
49VU
SDAC 2/26VAC SYNC/AC ESS BUS
F03
122VU
ANTI ICE/PROBES AND SENSORS 1/STATIC
Z12
49VU
SDAC 1/26VAC SYNC/AC ESS BUS
F02
122VU
ANTI ICE/PROBES/P 2/T 2/ENG 2
Y10
49VU
NAV/DME 1
G14
I NDI C AT I NG R E C O R DI NG SYST E M
CIRCUIT BREAKER A319/320
CIRCUIT BREAKER A319/320
PAN EL DESI GN ATION
LO C
PAN EL DESI GN ATION
LO C
49VU
EIS/ND CAPT/SWTG
E02
121VU
EIS/SDAC 2/BUS 2/26VAC SYNC AC
Q03
49VU
EIS/ND CAPT/SPLY
E01
121VU
EIS/SDAC 1/BUS 2/26VAC SYNC AC
Q02
49VU
FWS/FWC 1/SPLY
F01
121VU
EIS/ECAM DU/LOWER/SPLY
R11
121VU
EIS/ECAM DU/LOWER/SWTG
R10
106VU
EMER/GEN/REF
B05
121VU
EIS/DMC 2/SWTG
R08
106VU
DC/BUS 1 AND 2/MONG
C03
121VU
EIS/RLY/BOX/FIRST OFFICER
R07
121VU
EIS ND/FIRST OFFICER/SWTG
R06
121VU
CLOCK/STBY/SPLY –PTMZC/MZD
N02
121VU
EIS PFD/FIRST OFFICER/SWTG
R05
121VU
PTR/SPLY
J21
121VU
EIS ND/FIRST OFFICER
R04
121VU
CFDS/TEST PLUG 2
J20
121VU
EIS PFD/FIRST OFFICER
R03
121VU
CFDS/TEST PLUG 1
J19
121VU
CLOCK/STBY/SPLY –PT-MZA/MZF/MZG/MZH
N03
121VU
CFDS/CFDIU/SPLY
J18
121VU
DATA LOADER/SPLY
J16
121VU
CFDS/CFDIU/BACKUP
J17
121VU
AIDS/DMU AND QAR
K15
121VU
RCDR/ACCLRM
K18
121VU
RCDR/FDIU AND QAR
K17
121VU
RCDR/DFDR
K16
121VU
COM NAV/DME 2
K06
49VU
LANDING GEAR Y BRK/PRESS IND
C10
121VU
EIS/FIRST OFFICER/LOUD SPKR
P08
49VU
LANDING GEAR/LGCIU/SYS 1/NORM
C09
121VU
EIS/SDAC 1 AND 2/DOOR DET PAX
P05
121VU
EIS/SDAC 1 AND 2/BUS1/28VDC
P04
121VU HYDRAULIC/BRK FAN WHEELS 3 & 4
L35
121VU
EIS/SDAC 1 AND 2/BUS 2/28VDC
P03
121VU
HYDRAULIC/BRK FAN WHEELS 1 & 2
L32
121VU
EIS/SDAC 1 AND 2/DOOR DET AVCNS
P02
121VU
HYDRAULIC/BRK FAN CTL
M32
121VU
EIS/DMC 3/SPLY
Q09
121VU
HYDRAULIC/BRK TEMP DET UNIT
M37
121VU
EIS/DMC 2/SPLY
Q08
121VU
HYD BRAKING AND STEERING SYS2/ SPLY
M36
121VU
EIS/FWC 2/SPLY
Q07
121VU
HYD BRAKING AND STEERING SYS 2/CTL
M35
121VU
EIS/SDAC 2/SPLY
Q06
121VU
HYD BRAKING AND STEERING SYS 1/CTL
M34
121VU
EIS/SDAC 2/BUS 1/26VAC SYNC AC
Q05
121VU
HYD BRAKING AND STEERING SYS 1 IND/SPLY
M33
121VU
EIS/SDAC 1/BUS 1/26VAC SYNC AC
Q04
121VU
HYDRAULIC/PARK BRK/CTL/STBY
N37
L ANDI NG G E AR SYST E M
CIRCUIT BREAKER A319/320
CIRCUIT BREAKER A319/320
PAN EL DESI GN ATION
LO C
PAN EL DESI GN ATION
LO C
121VU
HYDRAULIC/PARK BRK/CTL/NORM
N36
122VU
LIGHTING/EXT LT/RWY TURN OFF L
W06
121VU
HYDRAULIC/LGCIU SYS 2
O35
122VU
LIGHTING/EXT LT/RWY TURN OFF R
W05
121VU
HYDRAULIC/LGCIU SYS 1/GRND SPLY
Q34
122VU
LIGHTING/EXT LT/WING AND ENG SCAN R
W03
122VU
LIGHTING/EXT LT/WING AND ENG SCAN L
W02
122VU
LIGHTING/WHL WELL/LTG DOME
X08
122VU
LIGHTING/WHL WELL/LTG OUT
X07
L I G H T S SYST E M 49VU
LIGHTING EMER LT/CKPT DOME
H08
122VU
LIGHTING/TST BOARD SPLY
X06
49VU
LIGHTING EMER LT/CABIN
H07
122VU
LIGHTING/ANN LT SPLY/XFMR BUS 2
X05
49VU
LIGHTING EMER LT/CABIN –PTMZG/MZH
H06
122VU
LIGHTING/ANN LT SPLY/XFMR BUS 1
X04
49VU
LIGHTING EMER LT/CABIN
H05
122VU
LIGHTING/ANN LT SPLY/XFMR/STAT INV
X03
49VU
LIGHTING/XFMR/115V.5V/ESS BUS
H03
122VU
LIGHTING/CKPT DOME
Y06
49VU
LIGHTING/ICE AND STBY COMP LIGHT
H04
122VU
LIGHTING/INSTL LT/GLARE SHLD
Y05
122VU
LIGHTING/INSTL LT/MAIN INST/PNL AND PED
Y04
122VU
LIGHTING/EXT LT/NAV 1 AND LOGO LIGHT
T03
122VU
LIGHTING/INSTL LT OVHD PNL
Y03
122VU
LIGHTING/EXT LT/NAV 2 AND LOGO LIGHT
T02
122VU
LIGHTING/AVNCS COMPT/OUT 115VAC
Z09
122VU
LIGHTING LANDING LT R/CTL
T07
122VU
LIGHTING/AVNCS COMPT/OUT 28 VDC
Z08
122VU
LIGHTING LANDING LT R/SPLY
T06
122VU
LIGHTING/AVNCS COMPT DOME
Z07
122VU
LIGHTING LANDING LT L/CTL
T05
122VU
LIGHTING/FLOOD FIRST OFFICER SIDE
Z06
122VU
LIGHTING LANDING LT L/SPLY
T04
122VU
LIGHTING/FLOOD CAPT SIDE
Z05
122VU
LIGHTING EXT LT BEACON UPPER
U06
122VU
LIGHTING/FLOOD CTR INST PNL
Z04
122VU
LIGHTING EXT LT BEACON LOWER
U03
2000VU AIR CONDTN COMPT OUTLET
B08
122VU
LIGHTING/CABIN/EMER LT
V07
2000VU CARGO COMPT LIGHT-LDG AERA
B06
122VU
LIGHTING/WING STROBE
V05
2000VU CARGO COMPT LIGHT-AFT
B05
122VU
LIGHTING/LOGO LEFT
V03
2000VU CARGO COMPT LIGHT-FWD
B04
122VU
LIGHTING/LOGO RIGH
V02
2000VU PASSENGER READING LIGHT
G07
122VU
LIGHTING/EXT LT/TAXI AND TAKE OFF/CTL
W09
2000VU PASSENGER READING LIGHT
G06
122VU
LIGHTING/EXT LT/TAXI AND TAKE OFF/TAXI
W08
2000VU PASSENGER READING LIGHT
G05
122VU
LIGHTING/EXT LT/TAXI AND TAKE OFF/TO
W07
2000VU PASSENGER READING LIGHT
G04
CIRCUIT BREAKER A319/320
CIRCUIT BREAKER A319/320
PAN EL DESI GN ATION
LO C
PAN EL DESI GN ATION
LO C
2000VU PASSENGER READING LIGHT
G03
121VU
ADIRS/ADIRU 2 PWR/SHED –PT-MZI/MZJ
N10
2000VU PASSENGER READING LIGHT
G02
121VU
ADIRS/ADIRU 3 PWR/SWTG –PT-MZI/MZJ
N09
2000VU CABIN LIGHT POWER-CEILING AFT
H08
121VU
ADIRS/ADIRU 2/26VAC AND AOA –PT-MZI/MZJ
N08
2000VU CABIN LIGHT POWER-CEILING AFT
HO7
121VU
ADIRS/ADIRU 3/26VAC AND AOA –PT-MZI/MZJ
N07
2000VU CABIN LIGHT POWER-CEILING FWD
H06
121VU
AIDRS/ADIRU 2/115VAC –PT-MZI/MZJ
N06
2000VU CABIN LIGHT POWER-CEILING FWD
H05
121VU
ADIRS/ADIRU 3/115VAC –PT-MZI/MZJ
N05
2000VU CABIN LIGHT POWER-WINDOW AFT
H04
121VU
ADIRS/ADIRU 2/28VDC –PTMZI/MZJ
N04
2000VU CABIN LIGHT POWER-WINDOW AFT
H03
121VU
ADIRS/ADIRU 3/28VDC –PT-MZI/MZJ
N03
2000VU CABIN LIGHT POWER-WINDOW FWD
H02
121VI
COM NAV/RADAR 1
K13
2000VU CABIN LIGHT POWER-WINDOW FWD
H01
121VU
COM NAV/RAD ALTIMETER 2
K12
2000VU LIGHT-ATTND WORK
J05
121VU
COM NAV/RAD ALTIMETER 1
K11
2000VU LIGHT-CABIN ENTRY
J04
121VU
COM NAV/ILS 2 –PTMZA/MZB
K09
121VU
COM NAV/VOR 2
K08
121VU
COM NAV/ATC 2
K07
121VU
EIS/GPWS/115VAC
P07
NAVI G AT I O N SYST E M 49VU
NAV STBY ALTIMETER
F14
121VU
EIS/GPWS/28VDC
P06
49VU
NAV VOR DME RMI
F13
121VU
COM NAV/RADAR 2 –PT-MZF
K14
49VU
NAV STBY HORIZONT
F12
121VU
COM NAV/ADF 2
K02
49VU
NAV PROBES ADIRU 3 PWR SWTG
F09
121VU
ADIRS/ADIRU 2/PWR/SHED –PT-MZA/ZF/ZG/ZH
N11
49VU
NAV PROBES ADIRU 1 AND AOA 1/26VAC
F07
121VU
ADIRS/ADIRU 3/PWR/SWTG –PT-MZA/ZF/ZG/ZH
N10
49VU
NAV PROBES ADIRU 1/115VAC
F06
121VU
ADIRS/ADIRU 2/26VAC AND AOA-MZA/ZF/ZG/ZH N09
49VU
NAV VOR 1
G13
121VU
ADIRS/ADIRU 3/26VAC AND AOA-MZA/ZF/ZG/ZH N08
49VU
NAV ILS 1 –PTMZA/MZB
G12
121VU
ADIRS/ADIRU 2/115VAC –PT-MZA/ZF/ZG/ZH
N07
49VU
NAV ATC 1
G11
121VU
ADIRS/ADIRU 3/115VAC –PT-MZA/ZF/ZG/ZH
N06
49VU
NAV ADF 1
H14
121VU
ADIRS/ADIRU 2/28VDC –PT-MZA/ZF/ZG/ZH
N05
49VU
NAV MMR 1-PTMZA/MZB
G12
121VU
ADIRS/ADIRU 3/28VDC –PT-MZA/ZF/ZG/ZH
N04
121VU
COM NAV/MMR 2 –PTMZB/ZC
L07
121VU
COM NAV/MMR 2 –PT-MZA/ZF/ZG/ZH
K09
105VU
ADIRS/ADIRU 1/28VDC
C02
CIRCUIT BREAKER A319/320 PAN EL DESI GN ATION
CIRCUIT BREAKER A319/320 LO C
PAN EL DESI GN ATION
OXIGEN SYSTEM
LO C
DOORS SYSTEM
49VU
OXYGEN/PASSENGER/ACTUATION
HA08
49VU
OXYGEN/PASSENGER/ACTUATION
HA07
121VU
EIS/SLIDES/ARM AND WARN GND
P10
49VU
OXYGEN/PASSENGER/ACTUATION
49VU
OXYGEN/PASSENGER/ACTUATION
HA06
122VU
DOORS CARGO
T12
HA05
122VU
DOORS PAX MONG
T13
49VU
OXYGEN/PASSENGER/CTL AND WARN
HA04
49VU
OXYGEN/PASSENGER/CTL AND WARN
HA03
49VU
OXYGEN/PASSENGER/CTL AND WARN
HA02
49VU
OXYGEN/CREW/OXYGEN/SPLY
HA01
P NE UM AT I C SYST E M 49VU
AIR BLEED/ENG 1 CTL
D12
49VU
AIR BLEED/ENG 1 MONG
D11
49VU
AIR BLEED/X FEED VALVE/BAT
D13
E NG I NE SYST E M 49VU
ENGINE 2/FADEC A AND EIU 2
A05
49VU
ENGINE 1/FADEC A AND EIU 1
A04
49VU
ENGINE 1 AND 2 ING SYS A
A03
49VU
ENGINE 2 HP FUEL SOV
A02
49VU
ENGINE 1 HP FUEL SOV
A01
121VU
ENGINE IGN ENG 2 SYS B
P42
121VU
ENGINE IGN ENG 1 SYS B
P41
122VU AIR BLEED/ENG 2 CTL
Z23
121VU
ENGINE IGN ENG 2 SYS A BAT
P40
122VU
AIR BLEED/ENG 2 MONG
Z22
121VU
ENGINE IGN ENG 1 SYS A BAT
P39
122VU
AIR BLEED/X FEED VALVE NORM
Z20
121VU
ENGINE ENG 2 FADEC B
Q40
121VU
ENGINE ENG 1 AND 2 EVMU
R44
121VU
ENGINE ENG 1 FADEC B AND EIU 1
R41
121VU
ENG/ENG 2 OIL PRESS AND REV SNSR CHAN A
N42
AI R BO R NE AUXI L I AR Y P O W E R SYS 121VU
APU/APU CTL
L42
121VU
ENG/ENG 2 OIL QTY AND VER SNSR CHAN B
N41
121VU
APU/ECB SPLY
L41
121VU
ENG/ENG 1 OIL PRESS AND VER SNSR CHAN A
N40
121VU
APU/OIL HTR SPLY
K41
121VU
ENG/ENG 1 OIL QTY AND VER SNSR CHAN B
N39
121VU
ENGINE 2 VER LOCK
N45
121VU
ENGINE 1 VER LOCK
N44
ABREVIAT URAS A319/320
ABREVIAT URAS A319/320
A/D
ANALOG TO DIGITAL CONVERTER
ADS
AIR DATA SYSTEM
A/F
AUTO FLIGHT
ADU
ALIGN DISPLAY UNIT
A/G
AIR TO GROUND
AEVC
AVIONICS EQUIPMENT VENTILATION COMPUTER
A/R
AUDIO REPRODUCER
AFC
AUTOMATIC FREQUENCY CONTROL
A/S
AUTO STABILIZATION
AFCS
AUTOMATIC FLIGHT CONTROL SYSTEM
A/SKID
ANTI-SKID
AFECU
AUTOMATIC FIRE EXTINGUISHER CONTROL UNIT
AADC
ANALOG AIR DATA COMPUTER
AFS
AUTOMATIC FLIGHT SYSTEM
AAP
ADITIONAL ATTENDENT PANEL
AHRS
ATTITUDE AND HEADING REFERENCE SYSTEM
ABD
AIRBUS DIRECTIVES
AIDS
AIRCRAFT INTEGRATED DATA SYSTEM
ACARS
AIRCRAFT COMM. ADRESS. REPORT SYS
ALTU
ANNUNCIATOR LIGHT TEST UNIT
ACC
ACTIVE CLEARENCE CONTROL
AMU
AUDIP MANAGEMENT UNIT
ACCEL
ACCELERATION/ACCELERATE
AOA
ANGLE OF ATTACK
ACCLRM
ACCELEROMETER
AOHX
AIR/OIL HEAT EXCHANGER
ACMM
ABBREVIATED COMPONENT MAINT MANUAL
AP/FD
AUTO PILOT/FLIGHT DIRECTOR
ACMR
AIRCRAFT CONFIGURATION MANAG.RULES
APLC
AIRCRAFT POWER LINER CONDITIONER
ACMS
AIRCRAFT CONDITION MONITORING SYSTEM
APPU
ASYMETRIC POSITION PICK OFF UNIT
ACOB
AUTOMATIC CALL OUT BOX
APU AFE
APU AUTO. FIRE EXTINGUISHER CONTROL UNIT
ACOC
AIR COOLED OIL COOLER
ASP
AUDIO SELECTOR PANEL
ACP
AREA CALL PANEL
AT
AUTOTHRUST
ACU
ANTENNA COUPLER UNIT
ATCSS
AIR TRAFIC CONTROL DATA LINK SIGNALL SYS
ADAU
AUXILIARY DATA ACQUISITION UNIT
ATSU
AIR TRAFIC SERVICE UNIT
ADC
AIR DATA COMPUTER
AVRS
AUDIO/VIDEO RECORDING SYSTEM
ADG
AIR DRIVE GENERATOR
BCDS
BITE CENTRALIZED SYSTEM
ADI
ATTITUDE DIRECTOR INDICATOR
BFDAS
BASIC FLIGHT DATA ACQUISITION SYSTEM
ADIRS
AIR DATA/INERTIAL REFERENCE SYSTEM
BIU
BITE INTERFACE UNIT
ADIRU
AIR DATA/INERTIAL REFERENCE UNIT
BMC
BLEED MONITORING COMPUTER
ADM
AIR DATA MODULE
BSCU
BRAKE /STEERING SYSTEM UNIT
ADPM
AIRCRAFT DEACTIVATION PROCEDURES MANUAL
BTR
BUS TIE RELAY
ADR
AIR DATA REFERENCE
BYDU
BACK-UP YAW DAMPER UNIT
ABREVIAT URAS A319/320
ABREVIAT URAS A319/320
CAS
COMPUTED AIR SPEED
EPSU
EMERGENCY POWER SUPLLY UNIT
CBMS/U
CIRCUIT BREAKER MONITORING SYSTEM/UNIT
EWD
ENGINE/WARNING DISPLAY
CCS
CABIN COMMUNICATIONS SYSTEM
FADEC
FULL AUTHORITY DIGITAL ENGINE CONTROL
CECAM
CENTRALIZED CABIN MONITORING
FAP
FORWARD ATTENDENT PANEL
CFDIU
CENTRALIZED FAULT DISPLAY INTERFACE UNIT
FC
FULLY CLOSED
CFDS
CENTRALIZED FAULT DISPLAY SYSTEM
FCDC
FLIGHT CONTROL DATA CONCENTRATOR
CIDS
CABIN INTERCOMMUNICATION DATA SYSTEM
FCMC
FUEL CONTROL AND MONITORING COMPUTER
CLOG
CLOGGING
FCMS
FUEL CONTROL AND MONITORING SYSTEM
CMC
CENTRALIZER MAINTENANCE COMPUTER
FCPC
FLIGHT CONTROL PRIMARY COMPUTER
CMS
CABIN MANAGEMENT SYSTEM
FCSC
FLIGHT CONTROL SECONDARY COMPUTER
CPC
CABIN PRESSURE CONTROLLER
FCU
FLIGHT CONTROL UNIT
CPCS/U
CABIN PRESSURE CONTROL SYSTEM/UNIT
FCV
FLOW CONTROL VALVE
CPMS/U
CABIN AND PASSENGER MANAGEMENT SYS/UNIT
FDIU
FLIGHT DATA INTERFACE UNIT
DADC/S
DIGITAL AIR DATA COMPUTER/SYSTEM
FDU
FIRE DECTECTION UNIT
DCDU
DATA CONTROL AND DISPLAY UNIT
FG
FLIGHT GUIDANCE
DMC
DISPLAY MANAGEMENT COMPUTER
FIDS
FAULT ISOLATION DETECTION SYSTEM
DSCS
DOOR AND SCAPE SLIDES CONTROL SYSTEM
FMA
FLIGHT MODE ANNUNCIATOR
EADI
ELECTRONIC ATTITUDE DIRECTOR INDICATOR
FMGEC
FLIGHT MANAGENT GUIDANCE ENVELOP COMPT
ECAM
ELECTRONIC CENTRALIZED AIRCRAFT MONITORI
FMGES
FLIGHT MANAGENT GUIDANCE ENVELOPE SYS
ECP
ECAM CONTROL PANEL
FMV
FUEL METERING VALVE
ECS
ENVIRONMENTAL CONTROL SYSTEM
FPEEPMS
FLOOR PROXIMITY EMRG. ESCAP PATH MK. SYS
EEC
ENGINE ELECTRONIC CONTROL
GCR
GENERATOR CONTROL RELAY
EFCC/S
ELECTRONIC FLIGHT CONTROL COMPUTER/SYST.
HCU
HYDRAULIC CONTROL UNIT
EGIU
ELECTRICAL GENERATOR INTERFACE UNIT
HEGS
HYDRAULIC ELECTRICAL GENERATING SYSTEM
EIU
ENGINE INTERFACE UNIT
HMU
HYDROMECHANICAL UNIT
EIUVMU
ENGINE INTERFACE/VIBRATION MONIT. UNIT
HPTACC
HIGH PRESSURE TURBINE ACTIVE CLEARNCE CTL
ELAC
ELEVATOR AILERON COMPUTER
HSMU
HYDRAULIC SYSTEM MONITORING UNIT
EMLS
EMERGENCY LIGHTING SYSTEM
LA
LINEAR ACCELEROMETER
EMU
ENGINE MAINTENANCE UNIT
LCIT
LOAD COMPRESSOR INLET TEMPERATURE
ABREVIAT URAS A319/320
ABREVIAT URAS A319/320
LGCIU
LANDING GEAR CONTROL INTERFACE UNIT
RAT
RAM A IR TURBINE
LLDC
LOW LEVEL DIRECT CURRENT VOLTAGE
RCCB
REMOTE CONTROL CIRCUIT BREAKER
LMS
LEAKAGE MEASUREMENT SYSTEM
RLA
REVERSER LEVER ANGLE
LOP
LOW OIL PRESSURE
RMP
RADIO MANGEMENT PANEL
LPTACC
LOW PRESS TURBINE ACTIVE CLEARENCE CTL
SDAC
SYSTEM DATA ACQUISITION CONCENTRATOR
LVDT
LINEAR VARIABLE DIFFERENTIAL TRANSDUCER
SDCU
SMOKE DETECTION CONTROL UNIT
MCDU
MULTIPURPOSE CONTROL DISPLAY UNIT
SFCC
SLAT FLAP CONTROL COMPUTER
MDDU
MULTIPURPOSE CONTROL DISPLAY UNIT
SIC
SYSTEM ISOLATION CONTACTOR
MÊS
MAIN ENGINE START
SSTU
SIDE STICK TRANSDUCER UNIT
MICBAC
MICRO-SYSTEM BUS ACCESS CHANNEL
TCAS
TRAFFIC ALERT COLLISION AVOIDANCE SYSTEM
MMR
MLTI MODE RECEIVER
THS
TRIMMABLE HORIZONTAL STABILIZER
MSU
MODE SELECTOR UNIT(IRS)
TLA
THROTTLE LEVER ANGLE
MSW
MICROSWITCH
TLU
TRAVEL LIMITATION UNIT
N/WS
NOSE WHEEL STEERING
TRA
THROTTLE RESOLVER ANGLE
OMS
ONBOARD MAINTENANCE SYSTEM
TRDV
THRUST REVERSER DIRECTINAL VALVE
OOT
OIL OUTLET TEMPERATURE
TRPV
THRUST REVERSER PRESSURIZING VALVE
OPV
OVERPRESURE VALVE
TTS
TRIM TANK SYSTEM
PC
PACK CONTROLLER
VBV
VARIABLE BLEED VALVE
PCU
PASSANGER CONTROL UNIT
VCO
VOLTAGE CONTROLLED OSCILLATOR
PCU
POWER CONTROL UNIT
VCU
VIDEO CONTROL UNIT
PES
PASSANGER ENTERTAINMENT SYSTEM
WBC/S
WEIGHT AND BALANCE COMPUTER/SYSTEM
PHC
PROBE HEAT COMPUTER
WHC
WINDOW HEAT COMPUTER
PIU
PASSENGER INFORMATION UNIT
WIPCU
WATER ICE PROTECTION CONTROL UNIT
PSCU
PROXIMITY SWITCH CONTROL UNIT
WIPDU
WATER ICE PROTECTION DATA UNIT
PSDU
POWER SUPPLY DECOUPLING UNIT
WTB
WING TIP BRAKE
PSS/U
PASSENGER SERVICES SYSTEM/UNI
WXR
WEATHER RADAR
PVIS
PASSENGER VISUAL INFORMATION SYSTEM
XDCR
TRANSDUCER
RACC
ROTOR ACTIVE CLEARENCE CONTROL
ZFCG
ZERO FUEL CENTER OF GRAVITY
RACSB
ROTOR ACTIVE CLEARENCE START BLEED
A319/320 P R E SSÃO DO S P NE US MAIN LANDING GEAR 210 PSI NOSE LANDING GEAR 178 PSI MAIN LANDING GEAR 168 A 189 TROCAR PNEU NOSE LANDING GEAR 143 A 161 TROCAR PNEU MAIN LANDING GEAR 0 A 168 TROCAR O PAR NOSE LANDING GEAR 0 A 143 TROCAR O PAR TORQUE DAS RODAS LOCK BOLT 35.39 A 39.89 Lbs/Pol MLG 1° 300.14 Lbs/Ft 2° 149.70 Lbs/Ft NLG 1º 160.76 Lbs/Ft 2º 80.01 Lbs/Ft F O NT E : L I NE CH E CK SUP P O R T I NG DAT A
M AX. DE F ASAG E M DE I ND. AL T I T UDE A-319 FLIG H T L E VE L
ADR 1 ADR 1/ 2/ ST DBY SP E E D ADR 2 F t 3 Ft AL T NO P F D NO P F D ADR 1/2 3 Ft
M AX. DE F ASAG E M DE I ND. AL T I T UDE A-319 FLIG H T L E VE L
ADR 1 ADR 1/ 2/ ST DBY SP E E D ADR 2 F t 3 Ft AL T NO P F D NO P F D ADR 1/2 3 Ft
G ND
---------
20
20
------
G ND
-------
6
6
6
50
50
65
125
50
4
7
55
80
185
100
4
5
8
90
135
295
200
3
5
9
130
195
390
300
C AS 2 5 0 KTS C AS 2 5 0 KTS C AS 3 0 0 KTS M AC H 0.78
4
300
C AS 2 5 0 KTS C AS 2 5 0 KTS C AS 3 0 0 KTS M AC H 0.78
3
5
9
390
M AC H 0.78
130
195
445
390
M AC H 0.78
3
4
8
100 200
R E F : D.E . A31934-001/ 34-13-00-810-998
R E F : D.E . A31934-002/ 34-13-00-810-998
M AX. DE F ASAG E M DE I ND. AL T I T UDE A-320 ADR 1 ADR 1/ 2/ ST DBY F L I G H T SP E E D ADR 2 F t 3 Ft AL T L E VE L NO P F D NO P F D ADR 1/2 /3 F t
M AX. DE F ASAG E M DE I ND. AI R SP E E D A-320 ADR 1 ADR 1/ 2/ ST DBY F L I G H T SP E E D ADR 2 F t 3 Ft AI S ADR L E VE L NO P F D NO P F D 1/2/3 F t
G ND
---------
20
20
-------
G ND
-------
6
6
6
50
50
65
130
50
4
7
55
80
185
100
4
5
8
90
135
295
200
3
5
9
130
195
390
300
C AS 2 5 0 KTS C AS 2 5 0 KTS C AS 3 0 0 KTS M AC H 0.78
4
300
C AS 2 5 0 KTS C AS 2 5 0 KTS C AS 3 0 0 KTS M AC H 0.78
3
5
9
390
M AC H 0.78
130
195
445
390
M AC H 0.78
3
4
8
100 200
R E F : D.E . A32034-001/ 34-13-00-810-998
R E F : D.E . A32034-002/ 34-13-00-810-998
I NG L Ê S T É C NI C O R E F E R Ê NC I A R ÁP I D A 01-ACCOMPLISHED THRU CHECK 02-ACCOMPLISHED DAILY CHECK 03-ACCOMPLISHED WEEKLY CHECK 04-ACFT DISPATCHED ACCORDING MEL... 05-NO AVAILABLE SPARE PART 06-PERFOMED OPERATIONAL TEST ON GROUND ...NO FAULTS FOUND ...THE SYSTEM IS OK 07-SWAPPED ( )WITH( )... ...TO BE REASEARCHED ...BOTH SYSTEM WORKED NORMAL ON GROUND ...THE FAULT REMAIN ...THE CHANGEND OF SIDE 08-PERFORMED TROUBLESHOOTING ...THE FAULTS 09-REPLACED ( ) AND OPERATIONAL TEST... ...ACCORDING TO MAINT. MANUAL ...IN UNIT(SELF TEST) 10-REPLACED NOSE WHEEL (LH/RH) /MAIN WHEEL DUE... ...NORMAL WEAR ...DEEP CUT ...LEAKAGE 11-REPALCED BRAKE # DUE... ...NORMAL WEAR ...LEAKAGE 12-THE PLUG... ...HAS BEEN CLANED ...HAS BEEN LOCKED 13-SENSOR WITH ERRONEUS(FALSE) INDICATIONS 14-MISSING 15-DEACTIVETED HYDRAULIC PUMP ON ENG # DUE... ...LEAKEGE 16-RETORQUED THE LINES, AFTER TEST OK
I NG L Ê S T É C NI C O R E F E R Ê NC I A R ÁP I D A 01-E F E T U AD A I N SP . DE T R ÂNSI T O 02-R E AL I Z ADO C H E C K DI ÁR I O 03-R E AL I Z ADO C H E C K SE M AN AL 04-AC F T DE SP AC H AD A D E AC O R DO M E L ... 05-Ñ P O SSUÍ M O S M AT E R I AL E ST Q 06-E F E T U ADO T E ST E O P E R AC I O N AL NO SO L O ... ...NE NH UM A P ANE F O I AC H AD A... ...O SI ST E M A E ST A O K 07-F O I I NVE R T I DO ( )C O M ( )... ...P AR A SE R P E SQ UI SADO ...NO SO L O AM BO S SI ST . O P E R AM NO R M AL M E NT ...A P ANE AI ND A C O NT I NU A ...A P ANE I N VE T E U DE L ADO 08-F E I T O P E SQ UI SA ...A P ANE E ... 09-F O I SUBST .( ) E F E I T O T E ST E O P E R AC I O N AL ...DE AC O R DO M ANU AL M NT ...N A UNI D ADE 10-SUBST . R O D A DE N AR I Z (L H /R H ) / T R E M P R I NC . DE VI DO ... ...DE SG AST E NO R M AL ...C O R T E P R O F UNDO ...VAZ AM E NT O 11-SUBT I T UI DO F R E I O # D E VI DO ...DE SG AST E NO R M AL ...VAZ AM E NT O 12-O P L UG (C O N E C T O R )... ...F O I L I M P O ...F O I T R AVADO 13-SE NSO R C O M I NDI C AÇ ÃO E R R O NE A 14-F AL T AN DO 15-DASAT I VAD A BO M B A H I D .(L H /R H ) DO M O T O R # DE VI DO ... ...VAZ AM E NT O 16-E F E T U ADO R E AP E R T O D AS L I NH AS AP Ó S T E ST E O K .
AT A P R O BLE M O R M SG VENT AVIONCS FAULTS
C B T O R E SE T
C B T O R E SE T
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION HOW LONG THE COMPUTER MUST BE DE-ENERGIZED:1S A/C CONFIGURATION: A/C ON GROUND AND BLOWER AND EXTRACT PUSH-BUTTONS ON VENTILATION PANEL:AUTO DITCHING PUSH-BUTTON: OFF
VU 122 Y17 AVNC S VE NT M O NG I F NO H E L P , T H E N R E SE T : VU 49 D5 AVNCS VENT CTL 21 VU 49 D6 AVNCS VENT CTL IF NO HELP, THEN RESET: VU 123 AE2 AVNCS VENT EXTC FAN 1-CONDITIONS OF POWER-UP TESTS INITIALIZATION HOW LONG THE COMPUTER MUST BE DE-ENERGIZED:1S A/C CONFIGURATION: A/C ON GROUND AND BLOWER AND EXTRACT PUSH-BUTTONS ON VENTILATION PANEL:AUTO DITCHING PUSH-BUTTON: OFF
2-DURATION:85 SEC FLIGHT DECK EFFECTS: BLOWER AND EXTRACT LOCAL FAULTS SMOKE AT GEN 1 LINE SKIN VALVES MOVING TO FULLY OPEN POSITION
2-DURATION:85 SEC FLIGHT DECK EFFECTS: BLOWER AND EXTRACT LOCAL FAULTS SMOKE AT GEN 1 LINE SKIN VALVES MOVING TO FULLY OPEN POSITION
3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED
3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED
TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TROUBLESHOOTING
TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TROUBLESHOOTING
21
VU 122 AVNCS VENT MONG
AT A P R O BLE M O R M SG
IF NO HELP, THEN RESET VU 49 D5 AVNCS VENT CTL VU 49 D6 AVNCS VENT CTL
VE N T AVI O NC S E XT R AC T F AUL T
ATA P R O BLE M O R M SG
21
C B T O R E SE T
COND. TRIM AIR DISREGARD IF THE WARNING SYS FAULT AND AND MSG “TRIM AIR HI PR” MSG “TRIM AIR HI IS TRIGGERED WHEN ALL TRIM PR” AIR VALVES ARE CLOSED REF FLT MANUAL 7-60
AT A P R O BLE M O R M SG C ABI N T R I M AI R VAL VE M SG
21
C B T O R E SE T VU 122 V17 Z O N T E M P C T L SYS 1 VU 122 V18 Z O N T E M P C T L SYS 2 VU 122 V19 Z O N T E M P C T L SYS 1 VU 122 V20 Z O N T E M P C T L SYS 2 R E SE T C B IN AC C O R DANC E W I T H T H E F O L L O W I N G P R O C E DU R E
3-RESULTS OF POWER-UP TESTS
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED
HOW LONG THE COMPTER MUST BE DE-ENERGIZED:200S A/C CONFIGURATION: A/C ON GROUND AND BOTH PACK SELECTED: OFF FLOW CONTROL VALVES: CLOSED
TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TROUBLESHOOTING
NOTE: BOTH PACK CONTROLLERS ENERGIZED AND HAVING FINISHED THEIR POWER-UP TESTS PLUS 5 SEC. DELAY FOR CONFIRMATION 2-PROGRESS OF POWER-UP TESTS DURATION: 36 SEC. FLIGHT DECK EFFECTS: 3 TRIM AIR VALVES ARE MOVING FROM COOL TO HOT AND FROM HOT TO COOL. 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TROUBLESHOOTING
ATA P R O BLE M O R M SG
22
AUTO FLIGHT A/THR LIMITED WARNING MSG
AT A P R O BLE M O R M SG
C B T O R E SE T MSG IS DISPLAYED WHEN AUTO THR ENGAGED AND THE THROTTLES ARE BELOW THE CL DETENT. MOVE THROTTLES PER FLT MANUAL 7-50
C B T O R E SE T
AUT O F L T A/T H R UP P E R E C AM M SG AF T E R O F F M SG E NG I NE ST AR T AND BE F O R E T .O . T H R U ST I S AP P L I E D (O N 22 T H E G R O UND). T H I S M SG SH O UL D D E DI SR E G AR DE D BY F L I G H T C R E W P E R F L T M ANU AL 7-50 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG
C B T O R E SE T
FCU FAULTS
AT A P R O BLE M O R M SG
C B T O R E SE T
VU 49 B5 FCU1 VU 121 M21 FCU2 RESET CB’S IN ACCORDANCE 22 WITH THE FOLLOWING PROCEDURE 1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
F M G C M SG VU 49 B2 F M G C 1 “ O P P O SI T E F M I N VU 121 M17 FMGC 2 P R O G R E SS O F VU 49 D6 AVNCS VENT CTL 22 F M A SH O WS RESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE O F F SI DE F D’S” 1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >7 MIN ON BOTH FCU’S A/C CONFIGURATION: A/C ON GROUND
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >4 SEC. A/C CONFIGURATION: A/C ON GROUND WITH ENGINES STOPPED
2- PROGRESS OF POWER-UP TESTS DURATION: 10 SEC FLIGHT DECK EFFECTS: ECAM STATUS PAGE: FCU 1&2 INOP – AP 1&2 INOP – A/THR INOP
2- PROGRESS OF POWER-UP TESTS DURATION:120 SEC FLIGHT DECK EFFECTS: ECAM STATUS PAGE: AP 1&2 INOP
3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED
3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED
TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TROUBLESHOOTING
TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TROUBLESHOOTING
AT A P R O BLE M O R M SG
22
FMGC MSG “SET OFFSIDE RANGE MODE”
C B T O R E SE T
AT A P R O BLE M O R M SG
VU 49 B2 FMGC 1 VU 121 M17 FMGCU 2 RESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
AUT O P I L O T #1 F AU L T
22
C B T O R E SE T VU 49 B2 F M G C 1 RESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >1 SEC A/C CONFIGURATION: A/C ON GROUND
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >4 SEC. A/C CONFIGURATION: A/C ON GROUND WITH ENGINES STOPPED
2- PROGRESS OF POWER-UP TESTS DURATION: 120 SEC FLIGHT DECK EFFECTS: ECAM STATUS PAGE: AP# 1 E 2 INOP
2- PROGRESS OF POWER-UP TESTS DURATION:120 SEC FLIGHT DECK EFFECTS: ECAM STATUS PAGE: AP #1 E 2 INOP
3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED
3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED
TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TROUBLESHOOTING
TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TROUBLESHOOTING
AT A P R O BLE M O R M SG 22
AUTO PILOT #2 FAULT
C B T O R E SE T
AT A P R O BLE M O R M SG
VU 121 M17 FMGCU 2 RESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
22
F AC F AU L T S SYST E M #1
C B T O R E SE T R E SE T F AC #1 P U SH BUT T O N I F NO H E L P , T H E N R E SE T VU 49 B3 F AC 1 26 VAC VU 49 B4 F AC 1 28 VDC RESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >4 SEC A/C CONFIGURATION: A/C ON GROUND WITH ENGINES STOPPED
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >4 SEC. A/C CONFIGURATION: 1-A/C ON GROUND WITH ENGINES STOPPED FOR ELECTRICAL POWER-UP TESTS, 2-A/C ON GORUND AND HYDRAULICALLY ENERGIZED FOR YAW DAMPER POWER LOOP POWER-UP TESTS
2- PROGRESS OF POWER-UP TESTS DURATION: 120 SEC FLIGHT DECK EFFECTS: ECAM STATUS PAGE: AP# 1 E 2 INOP 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TROUBLESHOOTING
2- PROGRESS OF POWER-UP TESTS DURATION:1 –90 SEC 2 –5 SEC FLIGHT DECK EFFECTS: AUTO FLT RUDDER TRIM 1(2) AUTO FLT RUD TRAV LIM 192) AUTO FLT YAW DAMPER 1(2) FLT CTL PANEL: FAULT FLASHES ON FAC 1 PUSHBUTTON 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TROUBLESHOOTING
AT A P R O BLE M O R M SG 22
FAC FAULTS SYSTEM #2
C B T O R E SE T R E SE T F AC #2 P U SH BUT T O N I F NO H E L P , T H E N R E SE T VU 49 B3 F AC 1 26 VAC VU 121 M 19 F AC 2 28 VDC
AT A P R O BLE M O R M SG 22
C B T O R E SE T
DUAL C AT I I I M SG VU 49 B4 F AC 1 28 VAC VU 121 M 19 F AC 2 28 VDC RESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
RESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >4 SEC. A/C CONFIGURATION: 1-A/C ON GROUND WITH ENGINES STOPPED FOR ELECTRICAL POWER-UP TESTS, 2-A/C ON GORUND AND HYDRAULICALLY ENERGIZED FOR YAW DAMPER POWER LOOP POWER-UP TESTS
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >4 SEC. A/C CONFIGURATION: 1-A/C ON GROUND WITH ENGINES STOPPED FOR ELECTRICAL POWER-UP TESTS, 2-A/C ON GORUND AND HYDRAULICALLY ENERGIZED FOR YAW DAMPER POWER LOOP POWER-UP TESTS
2- PROGRESS OF POWER-UP TESTS DURATION:1 –90 SEC 2 –5 SEC FLIGHT DECK EFFECTS: AUTO FLT RUDDER TRIM 1(2) AUTO FLT RUD TRAV LIM 1(2) AUTO FLT YAW DAMPER 1(2) FLT CTL PANEL: FAULT FLASHES ON FAC 2 PUSHBUTTON
2- PROGRESS OF POWER-UP TESTS DURATION:1 –90 SEC 2 –5 SEC FLIGHT DECK EFFECTS: AUTO FLT RUDDER TRIM 1(2) AUTO FLT RUD TRAV LIM 192) AUTO FLT YAW DAMPER 1(2) FLT CTL PANEL: FAULT LEGEND FLASHES
3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED
3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED
TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG 22
MCDU FAULT SYSTEM #1
C B T O R E SE T
AT A P R O BLE M O R M SG
VU 49 B1 M C DU 1 RESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
22
M C DU F AU L T SYST E M #2
C B T O R E SE T VU 121 N20 M C DU 2 RESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >200 MS. A/C CONFIGURATION: A/C ON GROUND
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >200 MS. A/C CONFIGURATION: A/C ON GROUND
2- PROGRESS OF POWER-UP TESTS DURATION:45 SEC
2- PROGRESS OF POWER-UP TESTS DURATION:45 SEC
FLIGHT DECK EFFECTS: MCDU SCREEN IS BLANK
FLIGHT DECK EFFECTS: MCDU SCREEN IS BLANK
3-RESULTS OF POWER-UP TESTS TESTS PASS:
3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED
ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TROUBLESHOOTING
TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TROUBLESHOOTING
AT A P R O BLE M O R M SG 22
AUTO FLT RUD TRV LIM SYS FAULT MSG
C B T O R E SE T
AT A P R O BLE M O R M SG
R E SE T F AC 1 AND F AC 2 P USH BUT T O N SW I T C H E S
R U DDE R T R A V E L L I M I T SYST E M #1
22
C B T O R E SE T VU 49 B3 F AC 1 26 VAC VU 49 B4 F AC 2 28 VDC I F NO H E L P , T H E N R E SE T : VU 49 B2 F M G C 1 (SE E C H 22, AP #1 F AUL T F O R P R O C E DUR E ) RESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TROUBLESHOOTING
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >4 SEC. A/C CONFIGURATION: 1-A/C ON GROUND WITH ENGINES STOPPED FOR ELECTRICAL POWER-UP TESTS, 2-A/C ON GORUND AND HYDRAULICALLY ENERGIZED FOR YAW DAMPER POWER LOOP POWER-UP TESTS 2- PROGRESS OF POWER-UP TESTS DURATION:1 –90 SEC 2 –5 SEC FLIGHT DECK EFFECTS: AUTO FLT RUDDER TRIM 1(2) AUTO FLT RUD TRAV LIM 192) AUTO FLT YAW DAMPER 1(2) FLT CTL PANEL: FAULT LEGEND FLASHES 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG 22
R U DDE R T R A V E L L I M I T SYST E M #2
C B T O R E SE T VU 121 M18 FAC 2 26VAC VU 121 M19 FAC 2 28VDC IF NO HELP, THEN RESET: VU 121 M17 FMGC 2 (SEE CH 22, AP #2 FAULT FOR PROCEDURE) RESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >4 SEC. A/C CONFIGURATION: 1-A/C ON GROUND WITH ENGINES STOPPED FOR ELECTRICAL POWER-UP TESTS, 2-A/C ON GORUND AND HYDRAULICALLY ENERGIZED FOR YAW DAMPER POWER LOOP POWER-UP TESTS 2- PROGRESS OF POWER-UP TESTS DURATION:1 –90 SEC 2 –5 SEC FLIGHT DECK EFFECTS: AUTO FLT RUDDER TRIM 1(2) AUTO FLT RUD TRAV LIM 1(2) AUTO FLT YAW DAMPER 1(2) FLT CTL PANEL: FAULT LEGEND FLASHES 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG 23
C I DS SYST E M F AU L T S
C B T O R E SE T AT T E M P T A R E SE T AT P T P F I R ST , I F NO H E L P , T H E N R E SE T : NO T E R E SE T C .B.’S T O GE T H E R VU 49 G 2 C I D DI R 1& 2 E SS VU 121 M 5 C I DS DI R 1& 2 NO R M RESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 110 SEC; 2- 30 SEC. A/C CONFIGURATION: 1-A/C ON GROUND WITH BOTH CABIN DOORS CLOSED 2-A/C ON GROUND WITH ENGINES STOPPED AND A CABIN DOOR OPEN 2- PROGRESS OF POWER-UP TESTS DURATION:1 –50 SEC 2 –120 SEC FLIGHT DECK EFFECTS: CIDS 1 ON THEN OFF AFTER 30 SEC CIDS 2 ON THEN OFF AFTER 80 SEC AUDIO CONTROL PANEL “ATT LIGHT IS FLASHING” CABIN AFFECTS: 1- CABIN LIGHTS ARE OFF DURING 1SEC 2-CABIN LIGHTS AND PAX ATT LIGHTS ARE FLASHING 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
ATA P R O BLE M O R M SG 23
F L T AT T ND/P NL L O C K E D UP
AT A P R O BLE M O R M SG 23
P AX E NT E R T AI NM E NT W I L L NO T T U R N O N O R O FF
AT A P R O BLE M O R M SG 23
C B T O R E SE T VU 2000 F 6 C ABI N C O M SYS P E S I F NO H E L P , T H E N R E SE T : AL L DE U’S VU 121 M 7 T H R O UG H M 13
C B T O R E SE T
C B T O R E SE T
SE AT VI DE O SYS R E SE T I NDI VI DU AL VI DE O UNI T P R O BL E M S UNI T , SM AL L H O L E J U ST F W D O F SC R E E N O N T H E SAM E P AN E L I S R E SE T BUT T O N(O NO FF)
AT A P R O BLE M O R M SG 23
VU 121 M 14 C I DS F W D AT T ND/P N L
P AX SE AT AUDI O VU 2000 C ABI N C O M SYS P E S I NO P
AT A P R O BLE M O R M SG 23
C B T O R E SE T
R M P F AUL T S
C B T O R E SE T T UR N AF F E C T E D R M P O F F T H E N O N T O R E SE T
AT A P R O BLE M O R M SG 23
ACP FREQ’S WILL NOT CHANGE FROM THE STANDBY TO ACTIVE WINDOWS
C B T O R E SE T T R UN AF F E C T E D R M P O F F T H E N O N T O R E SE T I F NO H E L P , T H E N R E S E T :
VU 49 B2 F M G C 1 VU 121 M 17 F M G C 2 RESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >4 SEC. A/C CONFIGURATION: A/C ON GROUND WITH ENGINES STOPPED 2- PROGRESS OF POWER-UP TESTS DURATION:120 SEC FLIGHT DECK EFFECTS: ECAM STATUS PAGE: AP 1(2) INOP 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TROUBLESHOOTING
ATA P R O BLE M O R M SG 23
T C AS I NO P M S G
AT A P R O BLE M O R M SG 23
C B T O R E SE T VU 121 K 10 T C AS NO T E SY S T E ST T H R U M C DU AL SO W O R K S
C B T O R E SE T
C O M VH F CHECK: E M I T T I NG F AUL T T R AN SM I T I O N K E Y O N AUDI O P AN E L SI DE ST I C K R ADI O SE L H AND M I K E SE L NO T I N T R AN S P O SI T I O N I F NO T F O UND I N T R ANS P O S R E SE T : VU 49 G 9 VH F 1* VU 121 L 4 VH F 2* VU 121 L 5 VH F 3* IF NO H E L P L E AVE C .B. O P E N ( P U L L E D) * R E F F L I G H T M ANU AL 7-58
AT A P R O BLE M O R M SG 23
C B T O R E SE T
VH F SY ST E M I NO P VU 49 G 9 VH F 1(SY S1) VU 121 L 4 VH F 2(SY S2) VU 121 L 5 VH F 3(SYS3)
AT A P R O BLE M O R M SG
C B T O R E SE T
ECAM MSG RELATED TO TRIPPED GREEN CB’S
NO R E Q U I R E M E NT H O W E VE R , I F T I M E P E R M I T S 24 R E SE T M AY BE AT T E M P T E D , I F UNSUC C E SF UL , DO NO T M AK E A SE C O ND AT T E M P E T F L T M ANU AL 7-57 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TROUBLESHOOTIMG
AT A P R O BLE M O R M SG
C B T O R E SE T
E NG I NE 1(2) E NG I NE (S) M UST BE SH UT G E NE R AT O R O N DO W N 24 L I NE ( G R E E N VU 122 T 26 G C U 1 (E N G 1) L I NE ) AND VU 122 T 27 G C U 2 (E N G 2) P AR AM E T E R S NO T RESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE SH O W N 1-CONDITIONS OF POWER-UP TESTS INITIALIZATION HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 15MS. A/C CONFIGURATION: 1-A/C ON GROUND WITH ENGINES STOPPED 2- PROGRESS OF POWER-UP TESTS DURATION: 30 MS FLIGHT DECK EFFECTS: NONE 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TROUBLESHOOTING
AT A P R O BLE M O R M SG 24
NO “AVAIL” GREEN LEGEND DISPLAYED ON “EXT PWR” PUSHBUTTON SWITCH
C B T O R E SE T E NG I NE S AN D AP U SH UT DO W N AND G R O UND P O W E R C O NNE C T E D VU 122 Y24 G P C U RESET CB’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: NONE A/C CONFIGURATION: 1-A/C ON GROUND, ENGINES STOPPED, APU STOPPED GROUND POWER UNIT CONNECTED TO THE A/C 2- PROGRESS OF POWER-UP TESTS DURATION: 35 MS FLIGHT DECK EFFECTS: NONE 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG
C B T O R E SE T
BA T T E R Y R E SE T SH I P S B AT T E R I E S O N E C H AR G E L I M I T E R AT A T I M E W I T H AP U 24 (BC L ) O P E R AT I N G I F H E L P , T H E N R E SE T : VU 105 N/A B AT R E F BL C 1 VU 105 N/A B AT BUS R E F BL C 1 VU 105 N/A B AT R E F BL C 2 VU 105 N/A B AT BUS R E F BL C 2 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TROUBLESHOOTING
AT A P R O BLE M O R M SG
AT A P R O BLE M O R M SG
R E SE T T /R T H R O U G H M C DU O R R E SE T AL L T H R E E USI N G G U AR DE D BUT T O N O N 103 VU P AN E L I N E L E C T R I C AL B AY
C R E W SE AT P R O BL E M S
C B T O R E SE T
3-RESULTS OF POWER-UP TESTS TESTS PASS:
VU 122 U11 C K P T SE AT C T L C AP T 25 VU 122 U14 C K P T SE AT C T L F /O ADDT I O N AL C .B. I S L O C AT E D UNDE R E AC H SE AT O N T H E C O N T R O L BO X 3-RESULTS OF POWER-UP TESTS TESTS PASS:
ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED
ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED
TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TROUBLESHOOTING
TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TROUBLESHOOTING
24
TRANSFORMER RECTIFIER FAULTS
C B T O R E SE T
AT A P R O BLE M O R M SG 26
FWD AND AFT CARGO DETECT MSGS
C B T O R E SE T VU 49 C6 SDCU CHAN 1 VU 122 T18 SDCU CHAN2 NOTE: RESET C.B.’S TOGETHER IF NO HELP, THEN RESET: VU 49 C6 SDCU CHAN1 VU 122 T18 SDCU CHAN 2 VU 49 AFT CARGO VENT&HTG FAN
AT A P R O BLE M O R M SG 26
F W D AND AF T C AR G O H E AT DE T E C T F AUL T S
C B T O R E SE T VU 49 AF T C AR G O VE NT & H E AT C T L /M O NG VU 122 S22 AF T C AR G O VE N T & H T G F AN RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 200 MS A/C CONFIGURATION: 1-A/C ON GROUND
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 200 MS A/C CONFIGURATION: 1-A/C ON GROUND
2- PROGRESS OF POWER-UP TESTS DURATION: 10 SEC FLIGHT DECK EFFECTS: NONE
2- PROGRESS OF POWER-UP TESTS DURATION: 10 SEC FLIGHT DECK EFFECTS: NONE
3-RESULTS OF POWER-UP TESTS TESTS PASS:
3-RESULTS OF POWER-UP TESTS TESTS PASS:
ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED
ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED
TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG 26
LAV SMOKE DETECT MSG
C B T O R E SE T VU 49 C6 SDCU CHAN 1 VU 122 T18 SDCU CHAN2 RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 200 MS A/C CONFIGURATION: 1-A/C ON GROUND 2- PROGRESS OF POWER-UP TESTS DURATION: 10 SEC FLIGHT DECK EFFECTS: NONE 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG 27
SI DE ST I C K P R I O R T Y M SG
C B T O R E SE T F AC 1& 2 SW I T C H E S SE C 1,2 & 3 SW I T C H E S E L AC 1& 2 SW I T C H E S
3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG
C B T O R E SE T
AT A P R O BLE M O R M SG
C B T O R E SE T
SEC 1,2 OR 3 FAULTS
USE PUSH BUTTON SWITCHES FIRST IF NO HELP, THEN RESET
E L AC 1 O R 2 F AU L T S
USE PUSH BUTTON SWITCHES FIRST IF NO HELP, THEN RESET VU49 B11 ELAC1 NORM SPLY ELAC 1 VU105 N/A ELAC1 STBY SPLY ELAC1 VU121 R20 ELAC2 SPLY ELAC 2 VU105 N/A ELAC2 STBY SPLY ELAC2 RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
27
VU 49 B8 1 NORM SPLY SEC 1 VU105 N/A SEC1 STBY SPLY SEC1 VU 121 Q18 SEC 2 SPLY SEC 2 VU 121 Q19 SEC 3 SPLY SEC3 RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
27
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 5SEC A/C CONFIGURATION: HYDRAULIC SYSTEM DE-PRESSURIZED
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 30 MS BY C/B OR RESET PUSHBUTTON OFF THEN ON A/C CONFIGURATION: HYDRAULIC SYSTEM DE-PRESSURIZED
2- PROGRESS OF POWER-UP TESTS DURATION: 18 SEC FLIGHT DECK EFFECTS: ECAM F/CTL PAGE: SEC AMBER IND., ASSOCIATED ELEVATORS CROSSED, ASSOCIATED SPOILERS AMBER CROSSED THEN FLASHING AT THE END OF THE TEST. ECAM WARNING:F/CTL SEC 1(2)(3) FAULT DURING AROUND 23 SEC. FLT CONTROL PANEL: SEC FAULT LEGEND IS FLASHING AT THE BEGINNING AND AT THE END OF TEST. 3-RESULTS OF POWER-UP TESTS TESTS PASS:
2- PROGRESS OF POWER-UP TESTS DURATION: 8 SEC FLIGHT DECK EFFECTS: ECAM F/CTL PAGE: ELAC AMBER INDICATION AND ASSOCIATED AILERON SERVO CONTROL AMBER BOXED ECAM WARNING: F/CTL ELAC1(2) FAULT DISPLAYED DURING 8 SEC. IF SUBSEQUENT TO C/B RESET NOTE: NONE IF SUBSEQUENT TO PUSHBUTTON RESET FLT CONTROL PANEL:FAULT LEGEND ILLUMINATED DURING 8SEC. 3-RESULTS OF POWER-UP TESTS TESTS PASS:
ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
ATA P R O BLE M O R M SG 27 F L I G H T C O N T R O L F L AP S L O C K E D O UT
AT A P R O BLE M O R M SG 27
FLT/CTL MSG WITH SLAT/FLAP FAULTS
C B T O R E SE T M UST P E R F O M E D W I N G T I P BR AK E (W T B ) R E SE T T H R O U G H M C DU P E R AM M 27-50-00 P G 209-211 (H YD M UST BE O F F )
C B T O R E SE T VU 49 B6 SLT CTL & MONG SYS 1 VU 49 B7 FLP CTL 7 MONG SYS 1 VU 121 R21 SLT CTL SYS 2 VU 121 Q21 FLP CTL & MONG SYS 2 RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 200 MS A/C CONFIGURATION: A/C ON GROUND WITH ENGINES STOPPED AND NEW DATE FROM CFDS 2- PROGRESS OF POWER-UP TESTS DURATION: 2 SEC FLIGHT DECK EFFECTS: ECAM WARNING: IF HYDRAULIC PRESSURIZED: FLT CTL SLAT SYS 1(2) OR FLAP SYS1(2) FAULT IF HYDRAULIC CIRCUIT NOT PRESSURIZED:NONE 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG
C B T O R E SE T
FLT/CTL VU 49 B10 FCDC 1 SPLY MAINTENANCE VU 121 Q20 FCDC 2 SPLY RESET C.B.’S IN ACCORDANCE WITH MSG(CAN BE THE FOLLOWING PROCEDURE DEFERRED) 1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
27
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >3SEC A/C CONFIGURATION: A/C ON GROUND AND ENGINES STOPPED 2- PROGRESS OF POWER-UP TESTS DURATION: 3 SEC FLIGHT DECK EFFECTS: ECAM WARNING:F/CTL FCDC 1(2) FAULT DURING 3 SEC. 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG SL O W SL AT S
27
C B T O R E SE T VU 49 B6 SLT CTL & MONG SYS 1 VU 121 R21 SLT CTL SYS 2 RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION HOW LONG THE COMPUTER MUST BE DEENERGIZED:>200 MS A/C CONFIGURATION: A/C ON GROUND WITH ENGINES STOPPED AND NEW DATE FROM CFDS 2- PROGRESS OF POWER-UP TESTS DURATION: 2 SEC FLIGHT DECK EFFECTS: ECAM WARMING: IF HYDRAULIC PRESSURIZED: FLT CTL SLAT SYS 1(2) OR FLAP SYS1(2) FAULT IF HYDRAULIC CIRCUIT NOT PRESSURIZED:NONE 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG FQI INOP
28
C B T O R E SE T VU 49 A13 FQI CHAN 1 VU 121 M27 FQI CHAN 2 VU 121 L26 FQI CHAN 1&2 RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
AT A P R O BLE M O R M SG 28
F U E L AP U L P VAL VE F AU L T M SG . T R I G G E R E D W H E N T H E AP U M AST E R SW I S SE L E C T E D O F F DU R I N G N A E M E R SH UT DO W N O R SH UT DO W N
C B T O R E SE T CYCLING THE MASTER SWITCH ON THEN OFF MAY CLEAR THIS MSG REF FLT MANUAL 7-114 RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >1SEC A/C CONFIGURATION: A/C ON GROUND AND REFUEL PANEL DOOR OPEN 2- PROGRESS OF POWER-UP TESTS DURATION: 80 SEC MAXIMUM FLIGHT DECK EFFECTS: ECAM FUEL PAGE: INTER-CELL TRANSFER VALVE INDICATION MOVING, AMBER “XXX” IN PLACE OF FUEL QUANTITY INDICATIONS THEN NORMAL INDICATONS ARE DISPLAYED 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
ATA P R O BLE M O R M SG H YD R E VS L O W 29 P R E SSUR E M SG
ATA P R O BLE M O R M SG P T U F AU L T S (NO T 29 C AUS E D BY C AR G O
C B T O R E SE T T O C L E AR : R U N E N G I NE S O R P R E SSUR I ZE H YDR AU L IC R E SE R VO IR S WI T H AP U. NO T E : TH IS H AP P E NS AF T E R WO R K IN G O N H YDR AUL I C SY S T E M
C B T O R E SE T VU 121 N34 SO L VAL VE G /Y P TU
C AUS E D BY C AR G O DO O R O P E R A T I O N AF T E R E NG I NE S S T AR TS)
ATA P R O BLE M O R M SG P T U F AU L T S 29
C B T O R E SE T
SE E NO T E S TH AT F O L L O W R E G AR D I NG F AUL T S F AUL T S C AUSE D BY C AR G O R E SE T WI T H E N G IN E S R UNN IN G : DO O R O P E R AT IO N WI TH I N A)R E SE T M E SS AG E US IN G 30 SE C O NDS AF TE R SE C O ND M AS T E R /C AU T I O N P USH BU T TO N E NG I NE S T AR T AND P T U S WI T C H E S E C AM F AI L UR E M E SS AG E S B)SE L E C T H YD P AG E O N E C AM N O T E : T H I S P R O C E DU R E C )SE L E C T Y H YD E L E C P M P O N W I L L NO T R E SE T R E AL P T U D)SE L E C T Y H YD E L E C P M P O F F F A I L U R E S O R H I DE R E A L E ) WAI T A M IN IM UN O F 30 SE C F AUL T S I N TH E P TU SYS T E M F )C YC L E P TU S WI T C H F R O M O N TO O F F TO O N G )SE L E C T#1 E N G I NE G R E E N H YD PM P OFF H )SE L E C T#1 E N G I NE G R E E N H YD PM P ON I ) S E L E C T # 2 E N G I N E Y H YD P M P O F F P TU SH O UL D O P E R AT E G R E E N TO YE L L O W J )SE L E C T#2 E N G IN E Y E L L O W H YD PM P ON K )E C AM SH O UL D BE NO R M AL
AT A P R O BLE M O R M SG 30
ANTI ICE L ( R ) WINDSHIELD
C B T O R E SE T IF THE WARNING OCCURS ON THE GROUND WITH OAT GREATER THAN 40 DEG C AND AC PACKS OFF, 5 MIN AFTER BOTH PACKS ARE SELECTED ON, RESET CB’S VU 121 X13 WHC 1 (LEFT SIDE) VU 122 W13 WHC 2 (RIGHT SIDE)
AT A P R O BLE M O R M SG 30
W I ND SH I E L D H E AT F AU L T S
C B T O R E SE T VU 122 X13 1(LEFT SIDE) VU 122 X14 WINDOW L HEAT VU 122 W13 WHC 2 (RIGHT SIDE) VU 122 W14 WINDOWS R HEAT RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 5SEC A/C CONFIGURATION: A/C ON GROUND
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 5SEC A/C CONFIGURATION: A/C ON GROUND
2- PROGRESS OF POWER-UP TESTS DURATION: 5 SEC FLIGHT DECK EFFECTS: NONE
2- PROGRESS OF POWER-UP TESTS DURATION: 5 SEC FLIGHT DECK EFFECTS: NONE
3-RESULTS OF POWER-UP TESTS TESTS PASS:
3-RESULTS OF POWER-UP TESTS TESTS PASS:
ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG 30
FWD (AFT) DRAIN MASTER ECAM MSG
C B T O R E SE T VU 2000 D1 FWD DRAIN MASTER VU 2001 D5 AFT DRAIN MASTER
AT A P R O BLE M O R M SG ANT I I C E M SG S
30
C B T O R E SE T VU 49 D3 ANT ICE PROBES PHC 1 VU 122 Y12 ANTI ICE PROBES PHC2 VU 122 Y16 ANTI ICE PROBES PHC 3 RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 1SEC A/C CONFIGURATION: A/C ON GROUND 2- PROGRESS OF POWER-UP TESTS DURATION: 2 SEC FLIGHT DECK EFFECTS: NONE 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
ATA P R O BLE M O R M SG 30 ANT I I C E P R O BE
C B T O R E SE T
ATA P R O BLE M O R M SG 30 ANT I I C E P R O BE
C B T O R E SE T
ATA P R O BLE M O R M SG 30 ANT I I C E P R O BE
C B T O R E SE T
VU49 D2 P I T O T 1 M SG S SY ST E M #1 VU 122 Z 13 AT AT I C 1 VU49 D4 AO A 1 VU 122 Z 12 T AT 1 I F NO H E L P , T H E N R E SE T : VU49 F 7 ADI R U 1& AO A 26 VAC VU49 T 6 ADI R U 1 115 VA VU 105 N/A ADI R U 1 28 VDC
VU 122 Y14 P I T O T 2 M SG S SY ST E M #2 VU 122 Y11 ST AT I C 2 VU 122 Y13 AO A 2 VU 122 Y15 T AT 2 I F NO H E L P , T H E N R E SE T : VU 121 N9 ADI R U 2 26 VAC & AO A VU 121 N7 ADI R U 2 115 VAC VU121 N5 ADI R U 2 28 VDC VU 121 N11 ADI R U 2 P W R SH E D
VU 122 Z 16 P I T O T 3 M SG S SY ST E M #3 VU 122 Z 14 ST AT I C 3 VU 122 Z 15 AO A 3 I F NO H E L P , T H E N R E SE T : VU 121 N8 ADI R U 3 26 VAC & AO A VU 121 N6 ADI R U 3 115 VAC VU 121 N4 ADI R U 3 28 VDC VU 49 F 9 ADI R U 3 ST W G SP L Y VU 121 N10 ADI R U 3 ST W G SP L Y 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG 31
DMC FAULT MSG EIS DMC 1,2 OR 3
C B T O R E SE T VU 49 E11 EIS DMC 1 SPLY (SYS1 VU 121 Q8 EIS DMC 2 SPLY(SYS) VU 121 Q9 EIS DMC 3 SPLY (SYS3) VU 49 E10 EIS DMC 3 STBY SPLY (SYS3) RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
AT A P R O BLE M O R M SG 31
UNAB L E T O SWI T C H D U
C B T O R E SE T VU 49 E4 EIS PFD CAPT SWTG VU 49 E2 EIS ND CAPT SWTG VU 121 R5 EIS PFD F/O SWTG VU 121 R6 EIS ND F/O SWTG VU 49 E6 EIS ECAM DU UPPER SWTG VU 49 E6 EIS ECAM DU UPPER SWTG VU 121 R10 ECAM DU LOWER SWTG RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >1SEC A/C CONFIGURATION: A/C ON GROUND 2- PROGRESS OF POWER-UP TESTS DURATION: 4 SEC FLIGHT DECK EFFECTS: ECAM WARNING:EIS DMC 1 OR 2 OR 3 FAULT NOTE: A DIAGONAL IS DISPLAYED ON THE THRRE ASSOCIATED DIPLAYED UNITS 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG 31
NO AIDS INDICATION DISPLAYED ON THE MCDU MENU PAGE
C B T O R E SE T
AT A P R O BLE M O R M SG
VU 121 K15 AIDS DMU & QAR RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
ADI R U F AUL T
31
C B T O R E SE T VU 49 F6 ADIRU A 115 VAC SYS1 VU 105 ADIRS ADIRU 1 28VDC VU 121 N7 ADIRU 2 115VAC (SYS2) VU 121 N5 ADIRU 2 28VDC (SYS2) VU 121 N6 ADIRU 3 115VAC (SYS3) VU 121 N4 ADIRU 3 28VDC (SYS3) RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >1SEC A/C CONFIGURATION: A/C ON GROUND
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 15 SEC
2- PROGRESS OF POWER-UP TESTS DURATION: 40 SEC FLIGHT DECK EFFECTS: ECAM WARNING: NONE NOTE: A DIAGONAL IS DISPLAYED ON THE THREE ASSOCIATED DISPLAY UNITS 3-RESULTS OF POWER-UP TESTS TESTS PASS: AIDS PROMPT RETURNS ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
A/C CONFIGURATION: A/C ON GROUND AND IR 1(2)(3) ROTARY BUTTON (LOCATED ON THE ADIRS PANEL) SWITCHED TO OFF FOR 15 SEC, THEN TO NAV. 2- PROGRESS OF POWER-UP TESTS DURATION: 5 SEC FLIGHT DECK EFFECTS: ADIRS PANEL: “ON BAT” LEGEND ILLUMINATED FOR 5 SEC, 2 SEC AFTER POWER-UP TEST INITIALIZATION. 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG 31
ECAM PAGE(S) LOCKED (I.E. DOORS-WHEELS ETC.)
C B T O R E SE T VU 49 F1 FWS FWC 1 SPLY VU121 Q7 EIS FWC 2 SPLY & QAR RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
AT A P R O BLE M O R M SG
C B T O R E SE T
SD AC 1 O R 2 F AU L T S
VU 49 F2 SDAC 1 26VAC SYNC AC ESS BUS VU 49 F4 SDAC 1 SPLY VU121 Q3 SDAC1 26VAC SYNC AC VU121 Q4 SDAC1 26VAC SYNC AC VU 121 P4 SDAC 1 28 VAC VU 49 F5 SDAC1&2 28VAC ESS BUS VU121 Q2 SDAC2 26VAC SYNC AC VU121 Q5 SDAC2 26VAC SYNC AC VU 121 Q6 SDAC 2 SPLY VU 121 P3 SDAC 2 28 VAC
31
RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: >1SEC A/C CONFIGURATION: A/C ON GROUND
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 1 SEC
2- PROGRESS OF POWER-UP TESTS DURATION: 50 SEC FLIGHT DECK EFFECTS: ECAM WARNING: “EIS 1(2) FWS FAULT”
A/C CONFIGURATION: A/C ON GROUND 2- PROGRESS OF POWER-UP TESTS DURATION: 5 SEC FLIGHT DECK EFFECTS: ECAM WARNING: “EIS 1(2) SDAC FAULT”
3-RESULTS OF POWER-UP TESTS TESTS PASS: AIDS PROMPT RETURNS
3-RESULTS OF POWER-UP TESTS TESTS PASS:
ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG 32
LGCIU FAULTS SYSTEM #1
C B T O R E SE T VU 49 C9 L/G LGCIU SYS1 VU 121 Q34 HYD LGCIU SYS 1 SPLY
AT A P R O BLE M O R M SG 32 L G C I U F AUL T S SYST E M #2
C B T O R E SE T VU121 Q35 HYD LGCIU SYS 2 RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 1 SEC
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 1 SEC
A/C CONFIGURATION: A/C ON GROUND
A/C CONFIGURATION: A/C ON GROUND
2- PROGRESS OF POWER-UP TESTS DURATION: 210 MSEC FLIGHT DECK EFFECTS: LGCIU 1 LDG GEAR PANEL “UNLK” RED INDICATIONS ARE FLASHING BRIEFLY LGCIU 2: NONE
2- PROGRESS OF POWER-UP TESTS DURATION: 210 MSEC FLIGHT DECK EFFECTS: LGCIU 2 LDG GEAR PANEL “UNLK” RED INDICATIONS ARE FLASHING BRIEFLY LGCIU 1: NONE
3-RESULTS OF POWER-UP TESTS TESTS PASS:
3-RESULTS OF POWER-UP TESTS TESTS PASS:
ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
ATA P R O BLE M O R M SG BSC U F AUL T S 32
C B T O R E SE T
I F A/C NO T M O VI N G T UR N NO SE W H E E L ST E E R I N G AND ANT I SK D O F F T H E N O N, I F NO H E L P , SE E BSC U SY ST E M F AU L T S 1& 2 O N F O L L O W I N G P AG E S. 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
ATA P R O BLE M O R M SG BSC U F AUL T S 32 SYST E M #1
C B T O R E SE T VU 121 M 33 BSC U SYS1 SP L Y VU 121 M 34 BSC U SYS1 C T L RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 1 SEC A/C CONFIGURATION: A/C ON GROUND 2- PROGRESS OF POWER-UP TESTS DURATION: 1 SEC FLIGHT DECK EFFECTS: NONE 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG 32
BSCU FAULTS SYSTEM #2
C B T O R E SE T VU 121 M 35 BSC U SYS2 C T L VU 121 M 36 BSC U SYS2 SP L Y RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 1 SEC A/C CONFIGURATION: A/C ON GROUND 2- PROGRESS OF POWER-UP TESTS DURATION: 1 SEC FLIGHT DECK EFFECTS: NONE 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG 32 NO BR AK E T E M P S DI SP L AY S
C B T O R E SE T VU121 M32 BRK TEMP DET UNIT RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
ATA P R O BLE M O R M SG 33 N O L I G H T I N M L G
C B T O R E SE T VU 2001 F 5 L I G H T SE C 19
WH E E L
ATA P R O BLE M O R M SG 33 AP U AR E A L I G H T S
C B T O R E SE T VU 2001 F 6 AP U SVC L I G H T
I NO P
ATA P R O BLE M O R M SG C ABI N L I G H T S 33
C B T O R E SE T
ATA P R O BLE M O R M SG C ABI N L I G H T S 33
C B T O R E SE T
R E SE T #2 C I DS T H R O U G H M C DU W I L L NO T T UR N I F NO H E L P , T H E N R E SE T : ON VU 121 M 8 T H R U M 13 DE U
C H E C K I F C O R R E C T L AM P I NST AL L E D I F C H E C K C I D S T H R O UG H T H E P T P F O R F AI L E D DE U AND R E SE T DE U I F P O SSI BL E . NO T E : AL L L I G H T S C O NT R O L L E D BY T H E F AI L E D DE U W I L L R E M I AN O N BR I G H T 3-RESULTS OF POWER-UP TESTS TESTS PASS: R E M AI NS O N BR I G H T W H E N SE L E C T E D O F F O R DI M
ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG DAR MSG
34
C B T O R E SE T M SG M AY B E R E L AT E D T O M E DI A(T AP E ) B E I N G F U L L VU 121 K 15 DM U & Q AR VU 121 K 17 F DI U & Q AR VU 121 K 18 AC C L M
AT A P R O BLE M O R M SG 34
F L T R E C O R DE R P R O BL E M I N FL I GH T O R R E C M SG
C B T O R E SE T VU 121 K17 FCDR FDIU & QAR RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 1 SEC
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 1 SEC
A/C CONFIGURATION: A/C ON GROUND AND ENGINES STOPPED
A/C CONFIGURATION: A/C ON GROUND AND ENGINES STOPPED
2- PROGRESS OF POWER-UP TESTS DURATION: 40 SEC FLIGHT DECK EFFECTS: MCDU “4 SEC
A/C CONFIGURATION: A/C ON GROUND AND ENGINES STOPPED
A/C CONFIGURATION: 1-A/C ON GROUND AND ENGINES STOPPED FOR ELECTTRICAL POWER-UP TESTS 2-A/C ON GROUND AND HYDRAULICALLY ENERGIZED FOR YAW DAMPER POWER LOOP POWER-UP TESTS 2- PROGRESS OF POWER-UP TESTS DURATION: 1- 90 SEC 2- 5 SEC FLIGHT DECK EFFECTS: AUTO FLT RUDDER TRIM 1(2) AUTO FLT RUD TRAV LIM 1(2) FLT CTL PANEL-“FAUTL” LEGEND FLASHES
2- PROGRESS OF POWER-UP TESTS DURATION: 25 SEC MAX FLIGHT DECK EFFECTS: ECAM WARNING:”RECORDER FDIU FAULT” IS DISPLAYED 3 SEC 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG 35
C B T O R E SE T
O2 LOW PRESSURE I NSUR E C R E W O 2 SUP P L Y MSG SWI T C H I S O N
3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
ATA P R O BLE M O R M SG BM C 36
ATA P R O BLE M O R M SG AI R R (L ) W I N G 36
BL E E D L E AK (O R AP U BL E E D L E AK ) M SG AF T E R E L E C T R I C AL T R AN SI E NT S AR E A L I G H T S I NO P 3-RESULTS OF POWER-UP TESTS PASS:
C B T O R E SE T VU 49 D11 AI R BL E E D E N G 1 M O NG (BM C 1) VU 122 Z 22 AI R B L E E D E N G 2 M O NG (BM C 2)
C B T O R E SE T R E SE T AF F E C T E D BL E E D P USH BUT T O N SW I T C H O N T O O F F T O O N T O C L E AR M SG . R E F . F L T M ANU AL BUL L E T I N 95-01
TESTS
ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG 36
LEFT WING LEAK MSGS
C B T O R E SE T VU 49 D11 AI R BL E E D E N G 1 M O NG (BM C 1) VU 49 D12 AI R BL E E D E N G 1 C T L
AT A P R O BLE M O R M SG 36
R I GH T W I NG L E AK M SG
RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
C B T O R E SE T VU 122 Z22 AIR BLEED ENG 2 MONG(BMC 2) VU 122 Z33 AIR BLEED ENG 2 CTL RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 1 SEC
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 1 SEC
A/C CONFIGURATION: A/C ON GROUND
A/C CONFIGURATION: A/C ON GROUND
2- PROGRESS OF POWER-UP TESTS DURATION: 10 SEC FLIGHT DECK EFFECTS: ECAM BLEED PAGE: BLEED TEMPERATURE INDICATION RESET TO 0 DEG. ENG 1 (2) BLEED AND APU BLEED PUSHBUTTON; LIGHT FLASHING
2- PROGRESS OF POWER-UP TESTS DURATION: 10 SEC FLIGHT DECK EFFECTS: ECAM BLEED PAGE: BLEED TEMPERATURE INDICATION RESET TO 0 DEG. ENG 1 (2) BLEED AND APU BLEED PUSHBUTTON; LIGHT FLASHING 3-RESULTS OF POWER-UP TESTS TESTS PASS:
3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG 36
CROSS BLEED VALVE MSG
C B T O R E SE T VU 49 D13 AI R BL E E D XF E E D VAL VE B AT VU 122 Z 20 AI R B L E E D XF E E D VAL VE NO R M AL RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
AT A P R O BLE M O R M SG 36
C R O SS BL E E D F AU L T S USE I N ADDI T I O N T O XF E E D VAL VE F AU L T S(M SG )
C B T O R E SE T VU 49 D11 AIR BLEED ENG 1 MONG(BMC 1) VU 49 D12 AIR BLEED ENG 1 CTL VU 122 Z 22 AIR BLEED ENG 1 MONG(BMC 2) VU 122 Z33 AIR BLEED ENG2 CTL VU 49 F4 SDAC 1 SPLY VU 121 Q SDAC 2 SPLY RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 1 SEC A/C CONFIGURATION: A/C ON GROUND 2- PROGRESS OF POWER-UP TESTS DURATION: 5 SEC FLIGHT DECK EFFECTS: ECAM WARNING; “EIS SINGLE SDAC FAULT 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
ATA P R O BLE M O R M SG 38 L O SS O F W AT E R
C B T O R E SE T VU 2000 D3 W AT E R SY ST E M
Q U ANT I T Y
ATA P R O BLE M O R M SG 38 T O I L E T W I L L N O T F L USH
ATA P R O BLE M O R M SG 38 G AL L E Y W AT E R
C B T O R E SE T VU 2001 B1 VAC T O I L E T SY S L AV VU 2001 B3 VAC T O I L E T SY S L AV VU 2001 B4 VAC T O I L E T SY S L AV
C B T O R E SE T
R E M O VE AF T G AL L E Y R I G H T C O F F E E M AK E R AND P L AC E F I NG E R T I P O VE R DR AI N T U BE , T H I S W I L L R E SE AT T H E C H E C K VAL VE 3-RESULTS OF POWER-UP TESTS TESTS PASS: SYS NO I SE
ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG 49
APU BLEED FAULTS
C B T O R E SE T SH UT DO W N AP U AND R E SE T C .B.’S VU 121 L 41 E C B SP L Y VU 121 L 42 AP U C T L
AT A P R O BLE M O R M SG 49
AP U W I L L NO T SH UT DO W N
C B T O R E SE T OPEN THESE C.B.’S VU 121 L42 APU CTL I F NO H E L P , T H E N R E SE T ; VU 121 L 41 E C B SP L Y
RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
3-RESULTS OF POWER-UP TESTS
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: NONE
TESTS PASS:
A/C CONFIGURATION: A/C ON GROUND AND APU STOPPED APU CONTROL PANEL; MASTER SWITCH”ON’ 2- PROGRESS OF POWER-UP TESTS DURATION: 3 SEC MAX FLIGHT DECK EFFECTS: APU CONTROL PANEL; ‘FAULT ON MASTER SWITCH PUSH-BUTTON 3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG
SE L E C T AP U E L E C O F F AND R E SE T T O O N I F NO H E L P , T H E N R E SE T : VU 1211 Y25 E L E C AP U G C U
AT A P R O BLE M O R M SG
C B T O R E SE T
1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
TRUN FADEC PUSHBUTTON SWITCH ON THEN OFF TO RESET FADEC IF NO HELP, THEN RESET VU49 A4 ENG1 FADEC A& EIU 1 VU121 R 41 E NG 1 F ADE C B & E I U1 VU49 A5 E N G 2 F ADE C A& E I U 2 VU 121 Q 40 E N G 2 F ADE C A& E I U 2 1-CONDITIONS OF POWER-UP TESTS INITIALIZATION
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 15 MS
HOW LONG THE COMPUTER MUST BE DE-ENERGIZED: 1 SEC
A/C CONFIGURATION: A/C ON GROUND AND ENGINE STOPPED
A/C CONFIGURATION: A/C ON GROUND AND ENGINE STOPPED
2- PROGRESS OF POWER-UP TESTS DURATION: 30 MS FLIGHT DECK EFFECTS: NONE
2- PROGRESS OF POWER-UP TESTS DURATION: 2 SEC MAX FLIGHT DECK EFFECTS: NONE
3-RESULTS OF POWER-UP TESTS TESTS PASS:
3-RESULTS OF POWER-UP TESTS
49
APU ELEC NO VOLTS OR FREQS
C B T O R E SE T
RESET C.B.’S IN ACCORDANCE WITH THE FOLLOWING PROCEDURE
73
F AD E C F AUL T M SG S “ E N G 1(2) F AD E C F AUL T O R “ E NG 1(2) F ADE C A O R B F AU L T NO T R E L AT E D T O R E AL F AI L UR E
TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
AT A P R O BLE M O R M SG 73
C B T O R E SE T
ENG 1(2) EPR R E C O V E R Y O F E P R O N BO T H MODE FAULT MSG E NG I NE S M AY AT T E M P E D BY SW I T C H I N G O F F E AC H E N G I N E ” S N 1 M O DE S W I T C H R E F F L T M ANU AL 7-86
3-RESULTS OF POWER-UP TESTS TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TROUBLESHOOTING
AT A P R O BLE M O R M SG
C B T O R E SE T
MAINTENANCE ACTION REQUIRED! EXCEPT WHEN WARNING IS TEMPORARILY DISPLAYED DURING ENGINE START WITH ENGINE OLI TEMP. BETWEEM 10° - 32° C REF. FLT MANUAL 7-80 3-RESULTS OF POWER-UP TESTS
79
E NG 1(2) O I L FILTER C LO G
TESTS PASS: ABOVE MENTIONED FAULT MSG NO LONGER DISPLYED TESTS FAIL: (FAULT CONFIRMED) PROCEED TO MEL/TSM FOR DEFERAL/TS
A320-232 F AUL T VE R I F I C AT I O N G UI DE
T H I S DO C UM E NT I S F O R T R AI NI NG P UR P O SE S O NLY AND W I L L NO T BE R E VI SE D AL W AYS R E F E R T O UA M ANUAL S F O R C UR R E NT AP P R O VE D P R O C E DUR E S
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