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 -RCL key for recalling an alert which had been inhibited or suppressed.
 -STS key for calling the STATUS page on the lower ECAM DU.
 -2 CLR keys which enable the crew to clear the warning/caution messages and to get automatically the A/C system pages in relation with the detected warnings or cautions.
 -EMER CANC guarded key for cancelling any aural warning including GPWS ones.
 F. Drawing the crew menbers attention
 (1)
 By visual devices A red MASTER WARN light and an amber MASTER CAUT light are installed on the glareshield in front of each pilot as attention getters to draw his attention to the ECAM DUs if a warning or a caution occurs. These lights are of the spring-loaded pushbutton switch type. Each FWC controls both CAPT and F/O lights.

 (2)
 By aural devices Two loudspeakers are installed in the cockpit, one in front of each pilot. They provide the crew with general communication voices and sounds, GPWS aural warnings, automatic call-out synthetic voices, and at last warning and caution aural warnings. The ON/OFF and volume control potentiometers can only control the general communication voices and sounds.

 G. INT LT/ANN LT Switch
 (Ref. Fig. 012)

R **ON A/C 106-149, 303-399, 401-499,
 (Ref. Fig. 013)
 1EFF : ALL 1 31-61-00Page 23 1 1 Aug 01/05 1 1 1CES 1

 Wiring Diagram for the DUs - Activation
 of Warning Flag Pattern on the Ground
 Figure 012
 1EFF :  ALL  1  31-61-00 Page 24 
1  1  May 01/05
 1R 1 
1CES  1

 

 Warning, Flag Patterns During Cockpit Light Test on the Ground (EFIS part)

 Figure 013 
R 1EFF : 1 1 1CES  106-149, 303-399, 401-499,  1 111 31-61-00 Page 25 Aug 01/05

 

R  **ON A/C 001-049, 051-099, 101-105, 201-299, 301-302,
 (Ref. Fig. 014) **ON A/C 151-199,
R  (Ref. Fig. 014A) **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
 (Ref. Fig. 015) **ON A/C ALL
R  On the ground, when performing a cockpit light test (by means of the INT LT/ANN LT switch), all the DUs present fixed warning flag patterns, showing flags and annunciators at their proper location. This mode is inhibited in flight. **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
 The test is activated by the DMCS on reception of a ground discrete signal at their contact pin AB8F. 

R 1EFF : ALL 1 31-61-00Page 26 1 1 May 01/05 1 1 1CES 1

 Warning, Flag Patterns During Cockpit Light Test on the Ground (EFIS part)

 Figure 014 
R 1EFF : 001-049, 051-099, 101-105, 201-299, 1301-302, 1 1CES  1 111 31-61-00 Page 27 May 01/05

 

 Warning, Flag Patterns During Cockpit Light Test on the Ground (EFIS part)

R  Figure 014A 
R 1EFF :  151-199,  1  31-61-00 Page 28 
1  1  Feb 01/05
 1  1
 1CES  1

 

 Warning, Flag Patterns During Cockpit Light Test on the Ground (ECAM part)

 Figure 015 
R 1EFF :  001-049, 051-099, 101-105, 151-199,  1 Page 2931-61-00
 1201-299, 301-302,  1 May 01/05
 1  1
 1CES  1

 

 EIS - Component Location in the Cockpit
 Figure 016 (SHEET 1)

R 1EFF : 106-149, 303-399, 401-499, 1 31-61-00Page 30 1 1 Aug 01/05 1 1 1CES 1

 EIS - Component Location in the Cockpit
 Figure 016 (SHEET 2)

R 1EFF : 106-149, 303-399, 401-499, 1 31-61-00Page 31 1 1 Aug 01/05 1 1 1CES 1

 CONTROL PANEL - ECAM (6WT) - REMOVAL/INSTALLATION
_________________________________________________ TASK 31-61-12-000-001 Removal of the ECAM Control Panel (6WT)
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking caps
 No specific circuit breaker(s) safety clip(s)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
31-61-12-991-001 Fig. 401
 3. Job Set-up
__________ Subtask 31-61-12-865-050
 A. Open, safety and tag this(these) circuit breaker(s):
　
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