Reset is only possible on the ground.
 E. Failure Table
 -------------------------------------------------------------------------------
MONITORED  ECAM MESSAGE  WARNING  MOTOR  SYSTEM
 FAILURE  ------------------------------ STATUS  STATUS
 -------------- E/W CRT ---------------- SYS/STATUS CRT----------------- ----------- ----------- ----------
Asymmetry.  FLT CTL  INOP SYS  CAUTION  The two  Stopped.
 Runaway.  SLATS LOCKED  SLATS CAT 3  +  stopped  No reset
 Overspeed.  WING TIP BRK ON  Single  in flight
 Uncommanded  MAX SPEED...  chime
 movement.
 CSU  MAX SPEED ...  LDG DIST=x1.1*
 mechanical  CAT 2 ONLY
 failure -------------- --------------------------------- ----------- ----------- ----------
System  FLT CTL  INOP SYS  CAUTION  The two  Stopped.
 jam.  SLATS FAULT  CAT 3 SLATS  +  stopped  Reset if
 The two Slat  MAX. SPEED...  LOG DIST...  Single  failure
 Channels  SLATS LEVER...  CAT 2 ONLY  chime  disapp-
failed  ...RECYCLE  INCREASED FUEL  ears
 CONSUMP
 CSU failure
 (valid out-
of-detent
 for more than
 10 seconds) -------------- --------------------------------- ----------- ----------- ----------
Slats not in  CONFIG  WARNING
 T.O.  SLATS NOT IN  +
 config.  T.O. CONFIG  CIRC

 -------------------------------------------------------------------------------Slat Channel FLT CTL SLATS SLOW Stopped 1/2 failure SLATS SYS 1(2) speed CSU failure FAULT (invalid pattern) PPU Synchro.
 1EFF : ALL 1 27-81-00Page 40 1 1 May 01/05R 1 1 1CES 1

 -------------------------------------------------------------------------------
MONITORED  ECAM MESSAGE  WARNING  MOTOR  SYSTEM
 FAILURE  ------------------------------ STATUS  STATUS
 E/W CRT -------------------------- SYS/STATUS CRT-------------------- ------------ ---------- -----------
LVDT.
 Valve Block
 Solenoid.
 Low hydraulic
 pressure.
 Operation
 Mode Coding.
 SFCC DC
 supply
 synchro excitation supply. ---------------------------------------------- ------------ ---------- -----------
Hydraulic  SLATS SLOW  Stopped  1/2
 Motor jam ------------- -------------- ------------------- ------------ ---------- speed-----------
WTB supply.  FLT CTL
 WTB solenoid ------------- SLAT TIP BRK FAULT--------------------------------- ------------ ---------- -----------
ARINC 429
 Input/Output.
 Installation
 Coding

 -------------------------------------------------------------------------------
* Depending on the slat and flap position.
 F. Parameter List Refer to 27-51-00 for data on the parameter list.
 8. BITE
____ Not Applicable
 1EFF : ALL 1 27-81-00Page 41 1 1 May 01/05R 1 1 1CES 1

 SLATS ELECTRICAL CONTROL AND MONITORING - DEACTIVATION/REACTIVATION
___________________________________________________________________
 TASK 27-81-00-040-001
 Deactivation of the SFCC 2 Slat WTB Solenoids
 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
 START A TASK ON OR NEAR:

 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS

 -COMPONENTS THAT MOVE.
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

 1. Reason for the Job
__________________
 Refer to the MMEL TASK: 27-81-01
 Slats Electrical Control and Monitoring
 Slat Wing Tip Brakes Solenoids

 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 No specific safety barriers
 No specific warning notice

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM FLIGHT CONTROLS 飛行操縱7(57)