-------------------------------------------------------------------------------
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
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 PNEUMATIC 气源 1(56)
