(FMA) Flight Mode Annunciator Bank Angle Attitude Data
Altitude Scale
Speed Scale
Vertical Speed
Flight Director Bars Fixed ACFT Symbol
Current Altitude Gnd Reference Elevation
Radio Altitude
Barometric Altimeter Reference
ILS Ident ILS Freq. DME Heading Distance
Track
ILS Course
Glide Slope Localizer
5
5
10
5
E/WD
10
N1
86.7
5
10
CL
86.7
10
670
EGT
92.5
N2
92.5
4600
F.F
4700
86.7%
FOB:
36000
S
F LA P
LBS
665
°C
F
FULL
AUTO FLT FAC 1 FAULT -FAC 1....................OFF THEN ON .IF UNSUCCESSFUL: -FAC 1....................................OFF
ELECTRONIC ENTRAILIZED C AIRCRAFT MONITOR
ENGINE
F. USED LBS 1900
1900
OIL
17.5
QT
17. 5
V IB
(N1 )
2. 0
2.0
V IB
(N2 )
0.7
0.7
AIR
LDG ELEV P
SD
6. 6
AUTO
600 FT
CAB V/S
PSI
FT/MN
-100 CKPT 76
TAT -16 ° C SAT -26 °C
FWD °F 74
AFT 74 74
18
CAB ALT
FT
2950
GW H
56
136200
L BS
Engine Thrust Limit and N1 Rating Limit.
Primary Engine Parameters
Total Fuel Onboard
Slat/Flap Position Memo or Warning/Caution
Messages
EMERGENCY Cancel System Pages Take-off config. test ALL
STATUS CLEAR
RECALL
CLEAR
31-21
SPEED
GS
L OC
CAT 3
AP1 + 2
DUAL DUAL
1FD2 A/T HR
MDA 1023
13 5 T AS 15 0 280 15 /
28
03 0 10
10
T
28
140
10
02 5
10
31 32
T
I
% 7. 6 8
LC
000 63 :
B OF
S BL
KMS P 30L
7.
. 5
T GE 1
280 15 /
28
29
30
NA RC O 295 31
27
32
26
5.
1 F. F
SPEED
0.7 NM 02:31
GI S
LOC
30 31 35
T
20
20
10
10
16 0
KMSP 30L
03 0
T
0064
7
28
14 0
30
29 .5
7 . 5
5
12 0
5
10
NA RC O
02 5
10
.
2000
OM T
VO R1
N O NE HT FF O . . 11 .. .. .. . . . . .. .. .. .. 1 C AF-
ADF
MS P
20 00 80 60 40 20 00 80
7
NARC O
29.92 QNH
1FD2 A/T HR
4000
TL UAF 1 CAF TLF OT UA
28 29
AP1+ 2
T
h
18 0
OM IMSP 110.3 5.7 NM 27
CAT 3 DUAL DUAL MDA 1023
K
33
1500
076
C°
2 N
29
0074
LL UF
5
ILS APP
150 G S 135 T A S
1
5
01
1
S 5.
5
68
MSPT 5
01
566
PAL F
7.
1
7
2000
5
01
1N
68
T
T
F
30 7
5
01
h
T
.5
1 1
LT K
33
MSP
20 00 80 60 40 20 00 80
7 120
30
1500
20
1 160
295 0.7 NM 02:31
NARC O
29
27 26
20
T
ILS APP
GS
4000
180
: L UF S SE C CUS NU F I.
7.6 NM
T
VO R1 MSP
7.6 NM
ADF
IMSP 110.3 5.7 NM 27
28 29
30 31 3
5
FF O . . . . . .. .. .. .. .. . . . .. .. .. . . . . .. .. .. .. 1 C AF-
1 1 1
T
L L H H
EN I GNE
) 1 N( E
0.
B I V
2
) 2 N( 7.
0.
2
0091
DES U. F SBL
B I V
0
7.
5.
0
0091
L I O
71
5.
TQ
71
EK I
R I A
TF 006 NM / TF H
OTUA
VELE GDL I SP
S/ V BAC
6.
6
P
001-
I U
TF . ni m
TLA BAC
TF A F° D WF 47 47 47
0592
h
T PKC 67
T . ni m
h
S BL T H
U
002631
WG 65 H
81
C° C°
6162-
TAT TAS
29.92 QNH
1
SPEED
GS
L OC
CAT 3
AP1 + 2
DUAL DUAL
1FD2 A/T HR
MDA 1023
13 5 T AS 15 0 280 15 /
28
03 0 10
10
T
28
140
10
02 5
10
31 32
T
I
% 7. 6 8
LC
000 63 :
B OF
S BL
KMS P 30L
7.
280 15 /
. 5
T GE 1
29
30
NA RC O 295 31 32
5.
1 F. F
SPEED
0.7 NM 02:31
GI S
LOC
30 31 35
T
20
20
10
10
16 0
KMSP 30L
03 0
T
0064
7
28
14 0
30
29 .5
7 . 5
5
12 0
5
10
NA RC O
02 5
10
.
2000
OM T
VO R1
N O NE HT FF O . . 11 .. .. .. . . . . .. .. .. .. 1 C AF-
ADF
MS P
20 00 80 60 40 20 00 80
7
NARC O
29.92 QNH
1FD2 A/T HR
4000
TL UAF 1 CAF TLF OT UA
28 29
AP1+ 2
T
h
18 0
OM IMSP 110.3 5.7 NM 27
CAT 3 DUAL DUAL MDA 1023
K
33
1500
076
C°
2 N
29
0074
LL UF
5
28
27 26
5
01
1
S 5.
5
ILS APP
150 G S 135 T A S
1
68
MSPT 5
01
566
PAL F
7.
1
7
2000
5
01
1N
68
T
T
F
30 7
5
01
h
T
.5
1 1
LT K
33
MSP
20 00 80 60 40 20 00 80
7 120
30
1500
20
1 160
295 0.7 NM 02:31
NARC O
29
27 26
20
T
ILS APP
GS
4000
180
: L UF S SE C CUS NU F I.
7.6 NM
T
VO R1 MSP
7.6 NM
ADF
IMSP 110.3 5.7 NM 27
28 29
30 31 3
5
FF O . . . . . .. .. .. .. .. . . . .. .. .. . . . . .. .. .. .. 1 C AF-
1 1 1
T
L L H H
EN I GNE
) 1 N( E
0.
B I V
2
) 2 N( 7.
0.
2
0091
DES U. F SBL
B I V
0
7.
5.
0
0091
L I O
71
5.
TQ
71
EK I
R I A
TF 006 NM / TF H
OTUA
VELE GDL I SP
S/ V BAC
6.
6
P
001-
I U
TF . ni m
TLA BAC
TF A F° D WF 47 47 47
0592
h
T PKC 67
T . ni m
h
S BL T
002631
WG
U
65 H
81
C° C°
6162-
TAT TAS
H
SENSOR AND COMPUTER INPUTS FOR: -NAVIGATION AND AFS -ENGINE FADEC SYSTEMS -FUEL QTY – WEIGHT & BALANCE SYS.
29.92 QNH
1
SPEED
GS
L OC
CAT 3
AP1 + 2
DUAL DUAL
1FD2 A/T HR
MDA 1023
13 5 T AS 15 0 280 15 /
28
03 0 10
10
T
28
140
10
02 5
10
31 32
T
I
% 7. 6 8
LC
000 63 :
B OF
S BL
KMS P 30L
7.
. 5
T GE 1
280 15 /
28
29
30
NA RC O 295 31
27
32
26
5.
1 F. F
SPEED
0.7 NM 02:31
GI S
LOC
30 31 35
T
20
20
10
10
16 0
KMSP 30L
03 0
T
0064
7
28
14 0
30
29 .5
7 . 5
5
12 0
5
10
NA RC O
02 5
10
.
2000
OM T
VO R1
N O NE HT FF O . . 11 .. .. .. . . . . .. .. .. .. 1 C AF-
ADF
MS P
20 00 80 60 40 20 00 80
7
NARC O
29.92 QNH
1FD2 A/T HR
4000
TL UAF 1 CAF TLF OT UA
28 29
AP1+ 2
T
h
18 0
OM IMSP 110.3 5.7 NM 27
CAT 3 DUAL DUAL MDA 1023
K
33
1500
076
C°
2 N
29
0074
LL UF
5
ILS APP
150 G S 135 T A S
1
5
01
1
S 5.
5
68
MSPT 5
01
566
PAL F
7.
1
7
2000
5
01
1N
68
T
T
F
30 7
5
01
h
T
.5
1 1
LT K
33
MSP
20 00 80 60 40 20 00 80
7 120
30
1500
20
1 160
295 0.7 NM 02:31
NARC O
29
27 26
20
T
ILS APP
GS
4000
180
: L UF S SE C CUS NU F I.
7.6 NM
T
VO R1 MSP
ADF
7.6 NM
IMSP 110.3 5.7 NM 27
28 29
30 31 3
5
29.92 QNH
FF O . . . . . .. .. .. .. .. . . . .. .. .. . . . . .. .. .. .. 1 C AF-
1 1 1
T
L L H H
EN I GNE
) 1 N( E
0.
B I V
2
) 2 N( 7.
0.
2
0091
DES U. F SBL
B I V
0
7.
5.
0
0091
L I O
71
5.
TQ
71
EK I
R I A
TF 006 NM / TF H
OTUA
VELE GDL I SP
S/ V BAC
6.
6
P
001-
I U
TF . ni m
TLA BAC
TF A F° D WF 47 47 47
0592
h
T PKC 67
T . ni m
h
S BL T
U
002631
WG 65 H
81
C° C°
6162-
TAT TAS
H
ACFT SYSTEM SENSOR AND COMPUTER INPUTS FOR: -AMBER CAUTIONS -ACFT SYSTEMS SYNOPTICS -DIGITAL FLT DATA RECORDER
1
SPEED
GS
L OC
CAT 3
AP1 + 2
DUAL DUAL
1FD2 A/T HR
MDA 1023
13 5 T AS 15 0 280 15 /
28
03 0 10
10
T
28
140
10
02 5
10
31 32
T
I
% 7. 6 8
LC
000 63 :
B OF
S BL
KMS P 30L
7.
280 15 /
. 5
T GE 1
29
30
NA RC O 295 31 32
5.
1 F. F
SPEED
0.7 NM 02:31
GI S
LOC
30 31 35
T
20
20
10
10
16 0
KMSP 30L
03 0
T
0064
7
28
14 0
30
29 .5
7 . 5
5
12 0
5
10
NA RC O
02 5
10
.
2000
OM T
VO R1
N O NE HT FF O . . 11 .. .. .. . . . . .. .. .. .. 1 C AF-
ADF
MS P
20 00 80 60 40 20 00 80
7
NARC O
29.92 QNH
1FD2 A/T HR
4000
TL UAF 1 CAF TLF OT UA
28 29
AP1+ 2
T
h
18 0
OM IMSP 110.3 5.7 NM 27
CAT 3 DUAL DUAL MDA 1023
K
33
1500
076
C°
2 N
29
0074
LL UF
5
28
27 26
5
01
1
S 5.
5
ILS APP
150 G S 135 T A S
1
68
MSPT 5
01
566
PAL F
7.
1
7
2000
5
01
1N
68
T
T
F
30 7
5
01
h
T
.5
1 1
LT K
33
MSP
20 00 80 60 40 20 00 80
7 120
30
1500
20
1 160
295 0.7 NM 02:31
NARC O
29
27 26
20
T
ILS APP
GS
4000
180
: L UF S SE C CUS NU F I.
7.6 NM
T
VO R1 MSP
7.6 NM
ADF
IMSP 110.3 5.7 NM 27
28 29
30 31 3
5
FF O . . . . . .. .. .. .. .. . . . .. .. .. . . . . .. .. .. .. 1 C AF-
1 1 1
T
L L H H
EN I GNE
) 1 N( E
0.
B I V
2
) 2 N( 7.
0.
2
0091
DES U. F SBL
B I V
0
7.
5.
0
0091
L I O
71
5.
TQ
71
EK I
R I A
TF 006 NM / TF H
OTUA
VELE GDL I SP
S/ V BAC
6.
6
P
001-
I U
TF . ni m
TLA BAC
TF A F° D WF 47 47 47
0592
h
T PKC 67
T . ni m
h
S BL T
U
002631
WG 65 H
81
C° C°
6162-
TAT TAS
H
ACFT SYSTEM SENSOR AND COMPUTER INPUTS FOR: -RED WARNINGS -FLT PHASE COMPUTATION -A/C SYSTEM SYNOPTICS -DFDR
29.92 QNH
1
SPEED
GS
LO C
-
-
CAT3 DUAL DUAL
AP1+ 2
MDA 1023
A/THR
1FD2
ENGINE G S 13 5T A S 15
0 F.USED 28 LBS
280 15 / 190 0
27
4000
OIL QT
26
18 0
17. 5
20
20
16 0
03 0 10
10
28
14 0
10
02 5
10
OM IMSP 110.3 5.7 NM 27
28
29
30
31 3 5
29.92 QNH
31
2. 0 32
1500
17. 5
VIB
(3N2 )
0. 7
0. 7
5
5
LDG ELEV
30 7
P
6. 6
600
AUTO
AFT 74 74
5
CAB ALT NARCO
CL
86. 7 %
EGT
FOB:
10
36000
LBS
FLAP
F
665
°C
S
92. 5
N2
92. 5
4600
F.F
4700
FULL
. 5
FT .
2950
AUTO FLT FAC 1 FAULT -FAC 1................. ...OFF THEN ON
GW
18
10
86.7
5
10
FT/MN 7
.
VOR1
TAT -16 ° C MS P SAT -26 °C 7. 6 NM
FT
CAB V/S
PSI
-100
FWD °F T 74
5
N1
670
.5 5
10
86.7
3
KMSP 30 L
AIR
CKPT 76
2000
29 5 (N1 ) 0. 7 NM 2. 0 02:31
NARCO
VIB
30
190 0
MSP
20 00 80 60 40 20 00 80
7 12 0
ILS APP 29
H
56
136200 ADF
.IF UNSUCCESSFUL: -FAC 1............. .............. .........OFF
L BS T T
-
-
-
-
ENGINE 5
190 0
10
F.USED LBS
FAILED E/W D AUTO SWITCHING
17. 5 5
10
EGT
670
°C
N2
92. 5 4600
6. 6 F.F
CKPT 76
FWD °F 74
P
VIB
(N1 )
2. 0
2. 0
CL V I B 86. 7 % (N2 )
86.7
OIL QT
17. 5
AIR
10
190 0
N1
86.7
5
5
FOB:
10
0. 7 0. 7 36000 LBS
665
LDG ELEV 92. 5
S
AUTO
FLAP
600
FT
F
CAB V/S FT/MN FULL -100
PSI
4700
AFT 74
CAB ALT
FT
2950
AUTO FLT FAC 1 FAULT
74
-FAC 1................. ...OFF THEN ON .IF UNSUCCESSFUL: -FAC 1............. .............. .........OFF TAT -16 °C
SAT -26
°C
18
H
GW
136200
L BS
56 T T
-
-
T T
FCU FLIGHT CONTROL UNIT EFIS Control Panel
AFS Control Panel
EFIS Control Panel
PFD CONTROL
FLIGHT DIRECTOR pb
G/S and LOC pb
ND CONTROL
WARNING/CAUTION MESSAGES
ADVISORY MODE
Title & corresponding Parameter Pulsing
180
BITE FAILURES
CFDS
(CENTRALIZED FAULT DISPLAY SYSTEM) FAILURE
FAILURE
CLASS 1
CLASS 2
FAILURE CLASS 3 T T
LEVEL 3
LEVEL 2
LEVEL 1 T
T
T
T
.
CORRECTIVE T
in
T
T
T
C
CAUT
T
T
P
ACTION TO BE
ACTION TO BE
PREFORMED Or MEL Deferral
PREFORMED IN
T
T
I
T
T
ECAM T
T
Display + CFDS
T
ECAM T
I
I
K
Display + CFDS
T
.
MASTER
WARN
ECAM
T
T
T
C
P
I
MASTER
h
T
T T
T
T T
CORRECTIVE in
h
“A” CHECK
T
h
U LK
U
T
Display + CFDS .
Indicated on STATUS page MAINTENANCE .
DECEL
Indicated ONLY in CFDS -
T
-
-
STS
-
-
H
H
SC
DE C
-
-
T
-
CRC
T
K
h
+ CFDS h
h
CRC = CONTINUOUS REPETIVE CHIME SC = SINGLE CHIME
-
ECAM WARNINGS
U
-
E/W Display
CLASS 1
OPERATIONAL CONSEQUENCE
STATUS Display
CLASS 2
NO IMMEDIATE OPERATIONAL CONSEQUENCE
CFDS only
CLASS 3
NO CONSEQUENCE ON AIRCRAFT Only found in CFDS
SAFETY
TYPE 1 SYS CFDIU BITE OTHER USERS
ARINC 429 BUS
TYPE 2 SYS CFDIU
BITE DISCRETE
OTHER USERS ARINC 429 BUS
TYPE 3 SYS CFDIU BITE DISCRETE
CFDS
ATA 31
3251 and A319
ON GROUND
IN FLIGHT
CFDS MENU
MAINT MENU
/ F OR
RUMBA
F RD
MCDU
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