ATA 31 Airbus 330

December 24, 2018 | Author: pontoo | Category: N/A

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Short Description

ATA 31 Airbus 330...

Description

(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

ATA 31 Airbus 330

Short Description

Description

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