-------------------------------------------------------------------------------
R R R R R R R R R R R R R R R  |LABEL : 067 | For BMC 2 | | |-----------------------------------------------------------------------------| | BIT | PARAMETER DEFINITION | STATUS 0 | STATUS 1 | COMMENTS | | | | | | | |-----------------------------------------------------------------------------| |-----------------------------------------------------------------------------| | 24 | | | | | |-----------------------------------------------------------------------------| | 25 | A/C A318 | NO | YES | Input AB 8A | |-----------------------------------------------------------------------------| | 26 | | | | | |-----------------------------------------------------------------------------| | 27 | HPV2 SOLENOID | NO COMMAND | COMMAND | | | | COMMAND | | | | |-----------------------------------------------------------------------------| | 28 | HPV2 SOLENOID | NO CONTROL | CONTROL | Output state | | | CONTROL | | | | |-----------------------------------------------------------------------------| | 29 | A/C A319 | NO | YES | Input AB 7A | -------------------------------------------------------------------------------
R  **ON A/C ALL
 5. Close-up________
 Subtask 36-11-00-860-063
 A. Put the aircraft back to its initial configuration.
 (1) On the MCDU, push the MCDU MENU mode key to get the MCDU MENU page.
 (2) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 TASK 36-11-00-710-002
 Operational Test to Read the CLASS III FAULTS
 1. Reason for the Job__________________
 To read the CLASS III FAULTS
 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
 31-32-00-860-011  Procedure to Get Access to the SYSTEM REPORT/TEST/PNEU Page
 3. Job Set-up__________
 Subtask 36-11-00-861-073
 A. Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002)

 Subtask 36-11-00-865-055
 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AIR BLEED/X FEED/VALVE/BAT 2HV D13 49VU AIR BLEED/ENG 1/CTL 3HA1 D12 49VU AIR BLEED/ENG 1/MONG 2HA1 D11 122VU AIR BLEED/ENG 2/CTL 3HA2 Z23 122VU AIR BLEED/ENG 2/MONG 2HA2 Z22 122VU AIR BLEED/X FEED VALVE/NORM 1HV Z20
 1EFF : ALL 1 36-11-00Page 530 1 1 Feb 01/05R 1 1 1CES 1

 Subtask 36-11-00-860-051
 C. Aircraft Maintenance Configuration
 (1)
 On the AIR COND panel 30VU:

 -
make sure that the ENG1 BLEED and ENG2 BLEED pushbutton switches are pushed (off legend are off),

 -
make sure that the X BLEED selector switch is at AUTO.

 (2)
 On one MCDU, get the SYSTEM REPORT/TEST PNEU menu page (Ref. TASK 31-32-00-860-011).

 4. Procedure
_________ Subtask 36-11-00-710-051
 A. Operational Test to Read the CLASS III FAULTS
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the MCDU:  On the MCDU:
 -push the line key adjacent to  - the BMC 1 (BMC 2) page comes into the BMC 1 (BMC 2) indication. view.
 2. On the MCDU:  On the MCDU:
 -push the line key adjacent to - the test result indication comes into the CLASS 3 FAULTS indication. view: either NO FAULT or LRU FAULT.
 3. On the MCDU:  On the MCDU:
 -push the MCDU MENU mode key. - the MCDU MENU page comes into view.
 5. Close-up
________ Subtask 36-11-00-862-051
 A. De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002).

 1EFF : ALL 1 36-11-00Page 531 1 1 Feb 01/05R 1 1 1CES 1

 TASK 36-11-00-710-003
 Operational Test of the Bleed Air System
 1. Reason for the Job
__________________
 To do a check of the bleed air system with engines and APU in operation
 2. Job Set-up Information
　
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