(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
Glide Slope Localizer
5
5
10
N1
86.7
5
E/WD
10
CL
86.7
5
10
EGT
665
92.5
N2
92.5
4600
F.F
4700
°C
FOB:
10
670
86. 7%
S
36000
LBS
FLAP
F
FULL
AUTO FLT FAC 1 FAULT -FAC 1....................OFF THEN ON .IF UNSUCCESSFUL: -FAC 1....................................OFF
ELECTRONIC CENTRAILIZED AIRCRAFT MONITOR
ENGINE
F. USED LBS
1900
OIL
17.5
QT
VIB
(N1)
1900
2. 0
2.0
VIB
(N2)
17. 5
0.7
0.7
AIR
LDG ELEV P
SD
6. 6
600 FT
AUTO
PSI
CAB V/S
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
LBS
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
SPEED
GS
LOC
CAT3
A P 1+ 2
DUAL DUAL
1FD2 A/THR
MDA 1023
G S1
35 TA S1 50 2 8 0 / 1 5
2 8
2 7
4000
ILS APP
T
20
20
10
10
1 160
03 0
T
28
140
10
02 5
10
T
I
0.7 NM 02:31
% . 6 8 L C 7 T
S B L 0 0 0 6 3 : B O F
KMSP 30L
T
F
30 5 . 7
7 . 5 5
2000
5
0 1
5
0 1
150 G S1 3 5 TA S 2 8 0 / 1 5
1
7 . 6 8
1
6 2
3 0
NARCO 295 3 1
T G E
. 2 9 5
2 N
. 2 9 5
0 0 7 4
1 F F .
0 0 6 4
28
29
30
31
35
29.92 QNH
T
1
11 N O N E H T F F O . . . . . . . . . . . . . . . . . . . . 1 C A F -
ADF
MS P
: L U F S S E C C U S N U F I .
7.6 NM
T
20
20
10
10
10
10
03 0
28
14 0
30 5 . 7
12 0
5
7.6
T
IMSP 110.3 5 . 7 N M 27
28
29
30
31
L L H
E N I G N E
) 1 N (
B I V
. 2 0
. 2 0
E
) 2 N (
B I V
. 0 7
. 7
0 0 9 1 . 7 1 5
0
D E S U F . S B L L I O
0 0 9 1 . 7 1 5
T Q
E K I
R I A
T F 0 0 6 N M / T F H
O T U A V E L E G D L
S / V B A C
S I P 6 . 6 P
0 0 1 -
I U
T F . n i m
T L A B A C
0 5 9 2
h
T F A F ° D W F 4 7 4 7 4 7
T P KC 6 7
T . n i m
h
S B L T H
U
0 0 2 6 3 1 W G
1 6 5 H 8
C ° C°
6 1 - T A T 6 2 - T A S
.
OM
ADF NM
02 5
2000
VOR1 MSP
20 00 80 60 40 20 00 80
7
7 . 5 5
T
H
1FD2 A/THR
16 0
F F O . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 C A F -
1 1 1
AP1+ 2
h
18 0
NARCO
VOR1
CAT3 DUAL DUAL MDA 1023
T
T L U A F 1 C A F T L F O T U A
IMSP 110.3 5 . 7 N M 27
T
KMSP 30L
0 7 6
C °
LOC
K
5
0 1
1
5 6 6
GI S
4000
MSPT 5
0 1
SPEED
0.7 NM 02:31 3 3
1500
NARCO
OM
ILS APP 2 9
3 2
T
P A L F S
L L U F
5
1 N
7 . 6 8
2 8
2 7
h
3 3
1500
1 1
LT K
MSP
20 00 80 60 40 20 00 80
7 120
N A R C O 295
3 1 3 2
6 2
180
30
2 9
35
29.92 QNH
1
SPEED
GS
LOC
CAT3
A P 1+ 2
DUAL DUAL
1FD2 A/THR
MDA 1023
G S1
35 TA S1 50 2 8 0 / 1 5
2 8
2 7
4000
ILS APP
T
20
20
10
10
1 160
03 0
T
28
140
10
02 5
10
T
I
0.7 NM 02:31
% . 6 8 L C 7 T
S B L 0 0 0 6 3 : B O F
KMSP 30L
T
F
30 5 . 7
7 . 5 5
2000
5
0 1
5
0 1
150 G S1 3 5 TA S 2 8 0 / 1 5
1
7 . 6 8
1
6 2
3 0
NARCO 295 3 1
T G E
. 2 9 5
2 N
. 2 9 5
0 0 7 4
1 F F .
0 0 6 4
28
29
30
31
35
29.92 QNH
T
1
11 N O N E H T F F O . . . . . . . . . . . . . . . . . . . . 1 C A F -
ADF
MS P
: L U F S S E C C U S N U F I .
7.6 NM
T
20
20
10
10
10
10
03 0
28
14 0
30 5 . 7
12 0
5
7.6
T
IMSP 110.3 5 . 7 N M 27
28
29
30
31
L L H
E N I G N E
) 1 N (
B I V
. 2 0
. 2 0
E
) 2 N (
B I V
. 0 7
. 7
0 0 9 1 . 7 1 5
0
D E S U F . S B L L I O
0 0 9 1 . 7 1 5
T Q
E K I
R I A
T F 0 0 6 N M / T F H
O T U A V E L E G D L
S / V B A C
S I P 6 . 6 P
0 0 1 -
I U
T F . n i m
T L A B A C
0 5 9 2
h
T F A F ° D W F 4 7 4 7 4 7
T P KC 6 7
T . n i m
h
S B L T
0 0 2 6 3 1 W G
U
1 6 5 H 8
C ° C°
6 1 - T A T 6 2 - T A S
H
SENSOR AND COMPUTER INPUTS FOR: -NAVIGATION AND AFS -ENGINE FADEC SYSTEMS -FUEL QTY – WEIGHT & BALANCE SYS.
.
OM
ADF NM
02 5
2000
VOR1 MSP
20 00 80 60 40 20 00 80
7
7 . 5 5
T
H
1FD2 A/THR
16 0
F F O . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 C A F -
1 1 1
AP1+ 2
h
18 0
NARCO
VOR1
CAT3 DUAL DUAL MDA 1023
T
T L U A F 1 C A F T L F O T U A
IMSP 110.3 5 . 7 N M 27
T
KMSP 30L
0 7 6
C °
LOC
K
5
0 1
1
5 6 6
GI S
4000
MSPT 5
0 1
SPEED
0.7 NM 02:31 3 3
1500
NARCO
OM
ILS APP 2 9
3 2
T
P A L F S
L L U F
5
1 N
7 . 6 8
2 8
2 7
h
3 3
1500
1 1
LT K
MSP
20 00 80 60 40 20 00 80
7 120
N A R C O 295
3 1 3 2
6 2
180
30
2 9
35
29.92 QNH
1
SPEED
GS
LOC
CAT3
A P 1+ 2
DUAL DUAL
1FD2 A/THR
MDA 1023
G S1
35 TA S1 50 2 8 0 / 1 5
2 8
2 7
4000
ILS APP
T
20
20
10
10
1 160
03 0
T
28
140
10
02 5
10
T
I
0.7 NM 02:31
% . 6 8 L C 7 T
S B L 0 0 0 6 3 : B O F
KMSP 30L
T
F
30 5 . 7
7 . 5 5
2000
5
0 1
5
0 1
150 G S1 3 5 TA S 2 8 0 / 1 5
1
7 . 6 8
1
6 2
3 0
NARCO 295 3 1
T G E
. 2 9 5
2 N
. 2 9 5
0 0 7 4
1 F F .
0 0 6 4
28
29
30
31
35
29.92 QNH
T
1
11 N O N E H T F F O . . . . . . . . . . . . . . . . . . . . 1 C A F -
ADF
MS P
: L U F S S E C C U S N U F I .
7.6 NM
AP1+ 2 1FD2 A/THR
h
T
20
20
10
10
10
10
16 0
03 0
T
28
14 0
30 5 . 7
12 0
5
7.6
02 5
.
2000
OM T
VOR1
ADF
MSP
20 00 80 60 40 20 00 80
7
7 . 5 5
NARCO
VOR1
CAT3 DUAL DUAL MDA 1023
18 0
T L U A F 1 C A F T L F O T U A
IMSP 110.3 5 . 7 N M 27
T
KMSP 30L
0 7 6
C °
LOC
K
5
0 1
1
5 6 6
GI S
4000
MSPT 5
0 1
SPEED
0.7 NM 02:31 3 3
1500
NARCO
OM
ILS APP 2 9
3 2
T
P A L F S
L L U F
5
1 N
7 . 6 8
2 8
2 7
h
3 3
1500
1 1
LT K
MSP
20 00 80 60 40 20 00 80
7 120
N A R C O 295
3 1 3 2
6 2
180
30
2 9
NM
IMSP 110.3 5 . 7 N M 27
28
29
30
31
35
29.92 QNH
F F O . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 C A F -
1 1 1
T
L L H H
E N I G N E
) 1 N (
B I V
. 2 0
. 2 0
E
) 2 N (
B I V
. 0 7
. 7
0 0 9 1 . 7 1 5
0
D E S U F . S B L L I O
0 0 9 1 . 7 1 5
T Q
E K I
R I A
T F 0 0 6 N M / T F H
O T U A V E L E G D L
S / V B A C
S I P 6 . 6 P
0 0 1 -
I U
T F . n i m
T L A B A C
0 5 9 2
h
T F A F ° D W F 4 7 4 7 4 7
T P KC 6 7
T . n i m
h
S B L T
U
0 0 2 6 3 1 W G
1 6 5 H 8
C ° C°
6 1 - T A T 6 2 - T A S
H
ACFT SYSTEM SENSOR AND COMPUTER INPUTS FOR: -AMBER CAUTIONS -ACFT SYSTEMS SYNOPTICS -DIGITAL FLT DATA RECORDER
1
SPEED
GS
LOC
CAT3
A P 1+ 2
DUAL DUAL
1FD2 A/THR
MDA 1023
G S1
35 TA S1 50 2 8 0 / 1 5
2 8
2 7
4000
ILS APP
T
20
20
10
10
1 160
03 0
T
28
140
10
02 5
10
T
I
0.7 NM 02:31
% . 6 8 L C 7 T
S B L 0 0 0 6 3 : B O F
KMSP 30L
T
F
30 5 . 7
7 . 5 5
2000
5
0 1
5
0 1
150 G S1 3 5 TA S 2 8 0 / 1 5
1
7 . 6 8
1
6 2
3 0
NARCO 295 3 1
T G E
. 2 9 5
2 N
. 2 9 5
0 0 7 4
1 F F .
0 0 6 4
28
29
30
31
35
29.92 QNH
T
1
11 N O N E H T F F O . . . . . . . . . . . . . . . . . . . . 1 C A F -
ADF
MS P
: L U F S S E C C U S N U F I .
7.6 NM
T
20
20
10
10
10
10
03 0
28
14 0
30 5 . 7
12 0
5
7.6
T
IMSP 110.3 5 . 7 N M 27
28
29
30
31
L L H
E N I G N E
) 1 N (
B I V
. 2 0
. 2 0
E
) 2 N (
B I V
. 0 7
. 7
0 0 9 1 . 7 1 5
0
D E S U F . S B L L I O
0 0 9 1 . 7 1 5
T Q
E K I
R I A
T F 0 0 6 N M / T F H
O T U A V E L E G D L
S / V B A C
S I P 6 . 6 P
0 0 1 -
I U
T F . n i m
T L A B A C
0 5 9 2
h
T F A F ° D W F 4 7 4 7 4 7
T P KC 6 7
T . n i m
h
S B L T
U
0 0 2 6 3 1 W G
1 6 5 H 8
C ° C°
6 1 - T A T 6 2 - T A S
H
ACFT SYSTEM SENSOR AND COMPUTER INPUTS FOR: -RED WARNINGS -FLT PHASE COMPUTATION -A/C SYSTEM SYNOPTICS -DFDR
.
OM
ADF NM
02 5
2000
VOR1 MSP
20 00 80 60 40 20 00 80
7
7 . 5 5
T
H
1FD2 A/THR
16 0
F F O . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 C A F -
1 1 1
AP1+ 2
h
18 0
NARCO
VOR1
CAT3 DUAL DUAL MDA 1023
T
T L U A F 1 C A F T L F O T U A
IMSP 110.3 5 . 7 N M 27
T
KMSP 30L
0 7 6
C °
LOC
K
5
0 1
1
5 6 6
GI S
4000
MSPT 5
0 1
SPEED
0.7 NM 02:31 3 3
1500
NARCO
OM
ILS APP 2 9
3 2
T
P A L F S
L L U F
5
1 N
7 . 6 8
2 8
2 7
h
3 3
1500
1 1
LT K
MSP
20 00 80 60 40 20 00 80
7 120
N A R C O 295
3 1 3 2
6 2
180
30
2 9
35
29.92 QNH
1
SPEED
GS
LOC
-
-
CAT3 DUAL DUAL
A P1 + 2
MDA 1023
A/THR
1FD2
ENGINE GS 1 35 TAS 1
2 8 0 / 1 5 1900
2 7
4000
50 F.USED 2 8 LBS OIL QT
6 2
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 N M 27
28
29
30
31
35
29.92 QNH
3 1
5 (N1) 0. 7 NM 2. 0 3 2 0 2 : 3 1 VIB (N2) 3
1900 1500
17. 5
5
2. 0
0. 7
AIR
P
6. 6
600
AUTO
CAB V/S
PSI
-100
5 . 7 5
FWD °F T 74
AFT 74 74
CAB ALT 5
NARCO
86. 7
CL
86.7
FT/MN
5
10
86. 7 %
670
665
92. 5
N2
92. 5
4600
F.F
4700
°C
36000 LBS
FOB:
10
EGT
FT
S
FLAP
F
FULL
7 . 5
FT .
2950
AUTO FLT FAC 1 FAULT
.
18
10
-FAC 1....................OFF THEN ON
VOR1
TAT -16 °C MS P SAT -26 °C 7. 6 NM
5
N1
3
5
LDG ELEV
30
10
0. 7
KMSP 30 L
CKPT 76
2000
NARCO 29
VIB
30
MSP
20 00 80 60 40 20 00 80
7 12 0
ILS APP 2 9
GW H
56
136200 ADF
.IF UNSUCCESSFUL: -FAC 1....................................OFF
LBS T T
-
-
-
-
ENGINE 5
1900
10
F.USED LBS
86. 7
FAILED E/W D
17. 5 5
10
1900
N1
86.7
OIL QT
17. 5 5
10
665
92. 5
N2
LDG ELEV 92. 5
4600
6. 6 F.F
CKPT 76
FWD °F 74
P
FOB:
10
EGT °C
(N1) 2. 0
0. 7 0. 7 36000 LBS
S
AUTO
FLAP
600
F
FT
CAB V/S FT/MN FULL -100
PSI
4700
AFT 74
AUTO FLT FAC 1 FAULT
VIB 2. 0
CL VIB86. 7 % (N2)
670
AIR
AUTO SWITCHING
5
CAB ALT
FT
2950
74
-FAC 1....................OFF THEN ON .IF UNSUCCESSFUL: -FAC TAT 1....................................OFF -16 °C
SAT -26
°C
18
H
GW
136200
LBS
56 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
FAILURE
CLASS 1
CLASS 2
CLASS 3 T T
LEVEL 3
LEVEL 2
LEVEL 1 T
T
T
T
.
CORRECTIVE T
in
T
MASTER
WARN
CAUT
P
I
PREFORMED Or MEL Deferral
ECAM Display + CFDS
ECAM T
T
Display + CFDS
T
ECAM T
T
I
“A” CHECK
T
T
K
h
h
U
LK
U
DE CE L
DE C
T
Display + CFDS .
Indicated on STATUS page MAINTENANCE .
-
-
Indicated ONLY in CFDS -
T
-
T
-
-
SC
STS
-
-
H
H
CRC
T
T
PREFORMED IN
I
K
T
T
P
ACTION TO BE ACTION TO BE T
T
h
T
C
I
MASTER
T
.
T
T T
C
T
CORRECTIVE in
h
T
T
T
T T
+ 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
ON GROUND
IN FLIGHT
CFDS MENU
MAINT MENU
/ F OR
RUMBA
F RD
MCDU
EIS (DMC 1) TEST < SYSTEM TEST < DISPLAY TEST < I/P TEST < SYSTEM TEST RESULT < RETURN
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Last Leg ECAM Report
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