-
ENG 1 and ENG 2 temperature: 200 plus 10.C or minus 40.C.
On the lower ECAM DU, the BLEED pageshows:
-APU BLEED VALVE crossline green,
-CROSSBLEED VALVE crossline green,
-PRV ENG 1 and ENG 2 in line green,
-HPV ENG 1 and ENG 2 in line green,
-
ENG 1 and ENG 2 pressure between 20 and 36psi,
-
ENG 1 and ENG 2 temperature between 150 and 200.C.
On the AIR COND panel 30VU:
-the ON legend of the APU BLEEDpushbutton switch comes on.
- on the lower ECAM DU, the BLEED page shows:
-APU BLEED VALVE in line green,
-CROSSBLEED VALVE in line green,
-PRV ENG 1 and ENG 2 crossline green,
-HPV ENG 1 and ENG 2 crossline green,
-pressure and temperature of BLEED APU.
1EFF : ALL 1 36-11-00Page 535 1 1 Feb 01/05R 1 1 1CES 1
5. Close-up
________
Subtask 36-11-00-860-053
A. Put the aircraft back to its initial configuration.
(1)
Stop the engines (Ref. TASK 71-00-00-710-028).
(2)
Stop the APU:
-GTCP 36-300 (Ref. TASK 49-00-00-860-004)
or
-APS 3200 (Ref. TASK 49-00-00-860-006)
or
-131-9(A) (Ref. TASK 49-00-00-860-009).
(3)
Do the EIS stop procedure
(Ref. TASK 31-60-00-860-002).
(4)
On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF.
(5)
De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
1EFF : ALL 1 36-11-00Page 536 1 1 Feb 01/05R 1 1 1CES 1
TASK 36-11-00-740-001
BITE Test of the BMC 1(2)
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
31-32-00-860-011 Procedure to Get Access to the SYSTEM REPORT/TEST/PNEU Page
3. Job Set-up__________
Subtask 36-11-00-861-072
A. Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002)
Subtask 36-11-00-865-075
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 537 1 1 Feb 01/05R 1 1 1CES 1
Subtask 36-11-00-860-062
C. Aircraft Maintenance Configuration
(1)
On the AIR COND panel:
-
make sure that the ENG 1(2) bleed pushbutton switches are pushed (OFF legends are off),
-
make sure that the crossbleed selector switch is at AUTO,
-
make sure that the APU BLEED pushbutton switch is released (ON legend is off).
(2)
Adjust the brightness of the MCDU screen.
(3)
On one MCDU, get the SYSTEM REPORT/TEST PNEU menu page (Ref. TASK 31-32-00-860-011).
4. Procedure
_________
Subtask 36-11-00-710-056-A
A. Bite test of the BMC 1(2)
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the MCDU:
-push the line key adjacent to the applicable BMC indication.
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(58)
