-
the skin-air inlet valve closes.
NOTE : If the VENT AVNCS SYS FAULT ECAM
____ warning comes into view on the upper ECAM DU, open and close circuit breaker 3HQ.If the warning goes out of view, no further action is required . If the warning is still in view, do the trouble shooting (Ref. TSM 21 PB 101).
On the DITCHING pushbutton switch:
-
the ON legend goes off.
On the PRESS page of the lower ECAM DU:
-
the skin air-outlet valve fully opens,
-
the skin air-inlet valve fully opens.
(2) Remove the access platform(s).
1EFF : ALL 1 21-26-00Page 521 1 1 May 01/04R 1 1 1CES 1
Subtask 21-26-00-860-059
B. Put the aircraft back to its initial configuration.
(1) Do the EIS stop procedure
(Ref. TASK 31-60-00-860-002).
Subtask 21-26-00-862-053
C. De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
Subtask 21-26-00-865-055
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1HL, 2HL, 3HL
1EFF : ALL 1 21-26-00Page 522 1 1 May 01/04R 1 1 1CES 1
TASK 21-26-00-710-008 Operational Test to Read the CFDS for CLASS 3 Faults of the AEVC
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 31-32-00-860-002 Procedure to Get Access to the SYSTEM REPORT/TEST/AIR COND Page 21-26-00-991-013 Fig. 501
3. Job Set-up
__________ Subtask 21-26-00-861-068
A. Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
NOTE : The energization of the aircraft electrical circuits starts a full
____ test of the ventilation system. The test continues for 2 minutes approximately.
1EFF : ALL 1 21-26-00Page 523 1 1 May 01/04R 1 1 1CES 1
Subtask 21-26-00-865-086
B. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AIR COND/AVNCS VENT/CTL 6HQ D06 49VU AIR COND/AVNCS VENT/CTL 5HQ D05 122VU AIR COND/AVNCS/VENT/MONG 3HQ Y17
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
123VU AVNCS VENT/EXTC/FAN 2HQ AE02 **ON A/C ALL
123VU AVNCS VENT/BLOWER/FAN 1HQ AD10 **ON A/C 301-399,
123VU AVNCS VENT/EXTC/FAN 2HQ AC04 **ON A/C ALL
Subtask 21-26-00-860-060
C. Aircraft Maintenance Configuration
(1) On one MCDU, get the SYSTEM REPORT/TEST/AIR COND page (Ref. TASK 31-32-00-860-002).
4. Procedure
_________ (Ref. Fig. 501/TASK 21-26-00-991-013) Subtask 21-26-00-710-065
A. Operational Test to Read the CFDS for CLASS 3 FAULTS of the AEVC
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On one MCDU, on the SYSTEM - the AEVC page comes into view. REPORT/TEST/AIR COND page:
-push the line key adjacent to
the AEVC indication.
2.
Push the line key adjacent to the - read the CLASS 3 FAULTS message. CLASS 3 FAULTS indication.
3.
On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.
5. Close-up
________ Subtask 21-26-00-860-061
A. Put the aircraft back to its initial configuration. Subtask 21-26-00-862-068
B. De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
1EFF : ALL 1 21-26-00Page 525 1 1 May 01/04R 1 1 1CES 1
CLASS 3 FAULTS from the CFDS Figure 501/TASK 21-26-00-991-013
1EFF : 1 1R 1CES ALL 1 11 1 21-26-00 Page 526 May 01/04
TASK 21-26-00-710-009 Operational Test to Read the CFDS for LAST LEG REPORT of the AEVC
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
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