空客计算机重置(TSM)

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ECAM有警告怎么办？

拔跳开关！

怎么拔？

听师傅的！

有依据吗？

不需要！

不知在实际工作中，是否遇到相同的情景时，也会如此处理。
从你全世界路过的TSM24-00-00-810-818-A - Computer Reset

NOTE
This reset procedure is used when a computer does not operate correctly.
NOTE
The line maintenance personnel can use it a first time to avoid a computer replacement (a reset must be done for the applicable computer as indicated in the Computer Reset Table). But, if there is more than one reset for each flight cycle for a given computer, it is necessary to do the specific troubleshooting procedure for the applicable system. If after a reset, the computer operates correctly, no more action is necessary.

To do computer reset:

(a) Set the related normal cockpit control to OFF, or open the related circuit breaker as specified in the reset procedure.

(b) Wait 3 seconds if a normal cockpit control is used, or 5 seconds if a circuit breaker is used (unless a different time is indicated).

(c) Set the related normal cockpit control to ON, or close the related circuit breaker.

(d) Wait 3 seconds for the end of the reset.

2

1

Air Conditioning

CPC

CAB PR SYS 1(2) FAULT

For CPC 1:

- On panel 49VU, open the

circuit breaker 1HL（D09）.

FOR CPC 2:

- On panel 122VU, open the

circuit breaker 2HL（Y22）.

After five seconds, close the

circuit breaker.

CVC

AIR FWD (AFT) CRG VENT

FAULT

On panel 49VU:

- Open the circuit breaker 31HN（C07）

After five seconds, close the

circuit breaker.

AEVC

VENT AVNCS SYS FAULT

On panel 122VU:

- Open the circuit breaker 3HQ（Y17）.

After five seconds, close the

circuit breaker.

ACSC

AIR PACK 1(2) REGUL FAULT

For the ACSC 1:

- On panel 122VU, open

the circuit breaker 49HH（X22）,

circuit breaker 50HH（Y18）

and circuit breaker 51HH（X21）.

- On panel 49VU, open

the circuit breaker 52HH（D08）.

Then close the circuit breakers.

For the ACSC2:

- On panel 122VU, open

the circuit breaker 53HH（W22）,

circuit breaker 54HH（Y20）,

circuit breaker 55HH （W21）and

circuit breaker 56HH（Y21）.

Then close the circuit breakers.

ACHC

COND AFT CRG HEAT FAULT

On panel 49VU:

- Open the circuit breaker 31HN（C07）.

- After five seconds, close the circuit breaker.

2

2

Auto Flight

FAC1(2)

AUTO FLT YAW DAMPER 1(2)

FAULT

Open these C/Bs with the

Yellow and Green hydraulic

systems pressurized:

- for the FAC 1: on the

panel 49VU, C/B 5CC1（B04）

- for the FAC 2: on the

panel 121VU, C/B 5CC2（M19）

Then close the C/Bs after 10 seconds.

FAC 1+2

WINDSHEAR DET FAULT

REAC W/S DET FAULT

WINDSHEAR DET FAULT orREAC W/S DET FAULT

Open then close the C/Bs in

this the order:

- on the panel 49VU, C/B

5CC1（B04） and C/B 14CC1（B03）

- on the panel 121VU, C/B

5CC2 （M19）and C/B 14CC2（M18）.

FCU

AUTO FLT FCU 1(2) FAULT

For the FCU1:

- on the panel 49VU, open

the C/B 9CA1（B05）.

For the FCU2:

- on the panel 121VU, open

the C/B 9CA2（M21）.

Close the C/B after 5 seconds.

If the fault does not

continue, do a check of the

target and barometer

references shown, and

correct them if necessary

(reset successful).

If the fault continues, open

again the two C/Bs 9CA1（B05）

on 49VU and 9CA2（M21） on 121VU.

Close the C/Bs after 7 min,

with an interval less than

5 sec between side 1 and

side 2.

At least 30 sec are necessary

until the end of the FCU1

and FCU2 safety test.

If the fault does not

continue, do a check of the

target and barometer

references shown, and

correct them if necessary

(reset successful)

If the fault continues, end

of procedure (reset

unsuccessful).

MCDU

One MCDU locked or blank

Open then close the C/B of

the defective MCDU after 10

seconds:

- For the MCDU1: on the

panel 121VU or panel 49VU,

C/B 11CA1（B01）.

- For the MCDU2: on the

panel 121VU, C/B 11CA2（N20）.

FMGC

Both MCDUs locked or blank

FMGC malfunction & Both MCDUs locked or blank

On the panel 121VU or 49VU:

- open the FMGC 1 C/B 10CA1（B02）

and close it after 10 seconds.

When initiated engine

stopped

(aircraft in maintenance

configuration), the reset

will be followed by a

power-up test sequence of

around 90 seconds. During

this test sequence,

the system is unavailable.

If there is no reset of the

FMGC 1, do a reset of the

FMGC 2 on the panel 121VU:

- open the C/B 10CA2（M17） and

close it after 10 seconds.

2

3

Communications

CIDS

COM CIDS 1+2 FAULT

- Open the C/Bs in this order:

on the panel 49VU, C/B 150RH（G01）

on the panel 121VU, C/B 151RH（M05）

on the panel 49VU, C/B 157RH（G02）

on the panel 121VU, C/B 156RH（M06）

- After 10 seconds, close

the C/Bs in this order:

156RH（M06）, 157RH（G02）, 151RH（M05） and

150RH（G01）.

CIDS

Uncommanded EVAC horn

actuation

Press the EVAC/HORN SHUT

OFF switch.

If unsuccessful:

- Open the C/Bs in this order:

on the panel 49VU, C/B 150RH（G01）

on the panel 121VU, C/B 151RH（M05）

on the panel 49VU, C/B 157RH（G02）

on the panel 121VU, C/B 156RH（M06）

- After 10 seconds, close

the C/Bs in this order:

156RH（M06）, 157RH（G02）, 151RH（M05） and

150RH（G01）.

RMP

Frozen RMP

You must do a reset of all

the RMPs, one after the other.

On the RMP control panel:

- set the ON/OFF switch to OFF

- after 5 seconds, set the

ON/OFF switch to ON.

FAP

Frozen FAP

Open the C/Bs in this order:

On the panel 49VU, CB 171RH（H01）

On the panel 121VU, CB 170RH（Q14）

- After 10 seconds, close

the C/Bs in this order:

170RH（Q14）, 171RH（H01）

If unsuccessful:

on the panel 2000VU

- open the tape reproducer

/PRAM C/B 2RX.

After 10 seconds, close the

C/B.

SDU

COM SATCOM FAULT

On the panel 121VU:

- Open the C/B 102RV1（K01）.

- After 10 seconds, close

the C/B.

2

4

Electrical Power

GAPCU

GPU cannot be connected

to the aircraft

If at least one power source

(IDG 1 or IDG 2, APU GEN or

batteries) is connected to

the electrical network of

the aircraft:

- On the ELEC control panel 35VU:

. Push and release the

EXT PWR pushbutton switch.

If no power source is

connected to the electrical

network of the aircraft:

- On the ELEC control panel 35VU:

. Push the BAT 1 and BAT 2

pushbutton switches

(the OFF legend goes off).

2

7

Flight Controls

ELAC

F/CTL ELAC 1(2) FAULT

F/CTL ALTN LAW FAULT

Reset the defective ELAC:

- Make sure that the

hydraulic systems are

depressurized before the

reset.

- Set the ELAC pushbutton

switch to OFF, then to ON.

ELAC or SEC

ELAC or SEC malfunction

Reset the defective ELAC:

- Make sure that the

hydraulic systems are

depressurized before the

reset.

Open, then close the C/B of

the defective ELAC or SEC.

For the ELAC 1(2):

- On the panel 49VU, C/B 15CE1（B11）.

- On the panel 121VU, C/B 15CE2（R20）.

For the SEC 1(2)(3):

- On the panel 49VU, C/B 21CE1（B08）.

- On the panel 121VU, C/B

21CE2（Q18） or 21CE3（Q19）.

FCDC

E/W FCDC1(2) FAULT

On the panel 49VU:

- For FCDC1, open the C/B

20CE1（B10）.

- For FCDC2, open the C/B

20CE2（Q20）121VU.

- After 5 seconds, close

the C/Bs.

2

8

Fuel

FQIC

Loss of fuel quantity

indication

Loss of fuel quantity indication or,Simultaneous triggering

of FUEL L XFR VALVE CLOSED and FUEL R XFR VALVE CLOSED,

although FUEL SD indicates no anomaly.

On the overhead circuit

breaker panel 49VU:

- Open the C/B 1QT（A13）.

On the rear circuit

breaker panel 121VU:

- Open the C/Bs 2QT （M27）and 8QT（L26）.

After 5 seconds, close the

three C/B's.

3

0

Ice and Rain Protection

WHC

ANTI ICE L（R）/WINSHIELD

L(R)/WINSHIELD

Open then close the C/B of

the defective WHC.

For the WHC1:

- on the panel 122VU, C/B

5DG1（X13）.

For the WHC2:

- on the panel 122VU, C/B

5DG2（W13）.

3

1

Indicating/Recording Systems

FWC

FWS FWC 1(2) FAULT

Open then close the C/B of

the defective FWC

For the FWC1:

- on the panel 49VU, C/B 3WW（F01）

For the FWC2:

- on the panel 121VU, C/B

2WW（Q07）.

Wait 50 seconds after you

close the C/Bs.

DMC

EIS DMC 1(2)(3) FAULT

Open then close the

circuit breaker of

the defective DMC

For the DMC1:

- on the overhead C/B panel

49VU, the circuit breaker

10WT1（E11）.

For the DMC2:

- on the rear C/B panel

121VU, the circuit breaker

10WT2（Q08）.

For the DMC3:

- on the rear C/B panel

121VU, the circuit breaker

10WT3（Q09）.

PFD

CAPT PFD DU malfunction

On the CAPT lightning/loud

speaker control-panel 301VU,

turn the PFD potentiometer

from the BRT position to

the OFF position.

- Wait for more than five

seconds.

On the CAPT lightning/loud

speaker control-panel 301VU,

turn the PFD potentiometer

from the OFF position to

the BRT position.

ND

CAPT ND DU malfunction

On the CAPT lightning/loud

speaker control-panel 301VU,

turn the ND potentiometer

from the BRT position to

the OFF position.

- Wait for more than five

seconds.

On the CAPT lightning/loud

speaker control-panel 301VU,

turn the ND potentiometer

from the OFF position to

the BRT position.

PFD

F/O PFD DU malfunction

On the F/O lightning/loud

speaker control-panel 500VU,

turn the PFD potentiometer

from the BRT position to

the OFF position.

- Wait for more than five

seconds.

On the F/O lightning/loud

speaker control-panel 500VU,

turn the PFD potentiometer

from the OFF position to

the BRT position.

ND

F/O ND DU malfunction

On the F/O lightning/loud

speaker control-panel 500VU,

turn the ND potentiometer

from the BRT position to

the OFF position.

- Wait for more than five

seconds.

On the F/O lightning/loud

speaker control-panel 500VU,

turn the ND potentiometer

from the OFF position to

the BRT position.

EWD

EWD malfunction

On the ECAM control panel

turn the UPPER DISPLAY

potentiometer from the

BRT + position to the OFF

position.

- Wait for more than five

seconds.

On the ECAM control panel

turn the UPPER DISPLAY

potentiometer from the

OFF position to the BRT +

position.

SD

SD malfunction

On the ECAM control panel

turn the LOWER DISPLAY

potentiometer from the

BRT position to the OFF

position.

- Wait for more than five

seconds.

On the ECAM control panel

turn the LOWER DISPLAY

potentiometer from the

OFF position to the BRT

position.

3

2

Landing Gear

BSCU

Braking malfunction

On the panel 121VU:

- open the C/Bs 1GG（M34）,

2GG（M33）,3GG（M35） and 4GG（M36）

- after 5 seconds, close

the CB's

LGCIU

L/G LGCIU 1(2) FAULT

For the LGCIU 1:

- on the panel 121VU, open

the C/B 52GA（Q34）then on 49VU,

C/B 1GA（C09）. After 15 seconds,

close the C/B 1GA（C09） and C/B

52GA（Q34）

For the LGCIU 2:

- on the panel 121VU, open

the C/B 2GA（Q35）. After 15

seconds, close the C/B 2GA（Q35）

3

4

Navigation

MMR

NAV MMR 1(2) FAULT

For the MMR 1:

- On the panel 49VU, open

the C/B 42RT1（G12）.

- After 5 seconds, close the

C/B.

For the MMR 2:

- On the panel 121VU, open

the C/B 42RT2（L07）.

- After 5 seconds, close the

C/B.

TCAS

NAV TCAS FAULT

On the panel 121VU:

- Open the C/B 4SG（K10）.

- After 5 seconds, close

the C/B.

GPWC

NAV GPWS FAULT

On the panel 121VU:

- Open the C/B 3WZ（P07）.

- After 5 seconds, close

the C/B.

GPSSU

NAV GPS 1(2) FAULT

On the panel 121VU:

- For GPSSU1, open the C/B

2SN1.

- For GPSSU2, open the C/B

2SN2.

- After 5 seconds, close

the C/Bs.

XCVR-RA

NAV RA 1(2) FAULT

On the panel 121VU:

- For XCVR-RA 1, open the

C/B 1SA1（K11）.

- For XCVR-RA 2, open the

C/B 1SA2（K12）.

- After 5 seconds, close

the C/Bs.

4

6

Information Systems

ATSU

ATSU malfunction

On the rear circuit

breaker panel 121VU:

- Open the C/Bs in this

order: 3TX1（L16） and 5TX1（L15）.

- After 5 seconds, close

the C/Bs in this order:

5TX1（L15） and 3TX1（L16）.

7

0

Engine

FADEC+EIU

EIU

ENG 1(2) IGN A + B FAULT

On the overhead circuit-breaker panel

49VU and rear circuit-breaker panel

121VU, open then close the circuit

breakers of the defective FADEC.

For engine 1:

· 2KS1（A04） and 4KS1（R41）.

For engine 2:

· 2KS2（A05） and 4KS2（Q40）.

7

7

Engine Indicating

EVMU

Loss of the VIB N1

警告信息：

Loss of the VIB N1 and VIB

N2 indications on ENGINE SD page

On rear circuit breaker

panel 121VU:

- Open the engine/ENG1 and 2/EVMU

circuit breaker (1EV)（R44）.

- After five seconds, close the

engine/ENG1 and 2/EVMU

circuit breaker (1EV)（R44）.