NOTE : The computer reset procedure is not a troubleshooting procedure.
____ But, the line maintenance personnel can use it (to prevent technical delay) if the computers do not operate correctly. Then the aircraft can go to a local repair center for maintenance. If there is more than one reset for each flight leg for a given computer, it is necessary to do the specific troubleshooting procedure for the applicable system. If after the reset, the computer operates correctly, no troubleshooting is necessary.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞24-00-00∞∞∞∞∞∞∞∞∞∞Page 233
Aug 01/05 CES (1) 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.
C. Air Conditioning
(1) Computer Reset Table
|-----------------------------------------------------------------------------| | ATA | SYSTEM MALFUNCTION | COMPUTER | RESET | | | | | PROCEDURE | |-----------------------------------------------------------------------------| | | VENT AVNCS SYS FAULT | AEVC | On the panel 122VU: | | | | | - open the C/B 3HQ | | | | | After 1 second, close the | | | | | C/B | | 21 ------------------------------------------------------------------------| | | AIR PACK 1(2) REGUL FAULT | PACK | For the pack controller 1: | | | | CONTROLLER | - on the panel 122VU, open | | | | 1(2) | then close the C/B 2HH. | | | | | For the pack controller 2: | | | | | - on the panel 122VU, open | | | | | then close the C/B 22HH. | |-----------------------------------------------------------------------------|
D. Auto Flight
(1) Computer Reset Table
|-----------------------------------------------------------------------------| | ATA | SYSTEM MALFUNCTION | COMPUTER | RESET | | | | | PROCEDURE | |-----------------------------------------------------------------------------| | | AUTO FLT YAM DAMPER 1(2) | FAC1(2) | Open these C/Bs with the | | | FAULT | | Yellow and Green hydraulic | | | | | systems pressurized: | | | | | - for the FAC 1: on the | | | | | panel 49VU, C/B 5CC1 and | | | | | C/B 14CC1 | | | | | - for the FAC 2: on the | | | | | panel 121VU, C/B 5CC2 and | | | | | C/B 14CC2. |
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞24-00-00∞∞∞∞∞∞∞∞∞∞Page 234
Aug 01/05 CES
|-----------------------------------------------------------------------------|
| ATA | SYSTEM MALFUNCTION | COMPUTER | RESET |
| | | | PROCEDURE |
|-----------------------------------------------------------------------------|
| | | | Then close the C/Bs after 10|
| | | | seconds. |
| |-----------------------------------------------------------------------|
| | WINDSHEAR DET FAULT or | FAC 1+2 | Open then close the C/Bs in |
| | REAC W/S DET FAULT | | this the order: |
| | | | - on the panel 49VU, C/B |
| | | | 5CC1 and C/B 14CC1 |
| | | | - on the panel 121VU, C/B |
| | | | 5CC2 and C/B 14CC2. |
| |-----------------------------------------------------------------------|
| | AUTO FLT FCU 1(2) FAULT | FCU | For the FCU1: |
| | | | - on the panel 49VU, open |
| | | | the C/B 9CA1. |
| | | | For the FCU2: |
| | | | - on the panel 121VU, open |
| | | | the C/B 9CA2. |
| | | | Close the C/B after 5 |
| | | | seconds. |
R | | | |If the fault does not |
R | | | | continue, do a check of the |
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 電源 1(87)
