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 -------------------------------------------------------------------------------
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵7(57)
