(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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