B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 36-11-58-991-001 Fig. 401
3. Job Set-up
__________
Subtask 36-11-58-861-050
A. Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
R 1EFF : 151-199, 401-499, 1 36-11-58Page 401 1 1 Aug 01/05 1 1 1CES 1 Subtask 36-11-58-941-050
B. Safety Precautions
(1)
Make sure that the engine 1(2) shutdown occured not less than 5 minutes before you do this procedure.
(2)
On the AIR COND panel 30VU:
-
make sure that the ENG 1(2) BLEED pushbutton switch is released (OFF legend is on),
-
make sure that the APU BLEED pushbutton switch is released (ON legend is off),
-put a warning notice to tell persons not to operate the pneumatic system.
(3)
On the center pedestal, on the ENG panel 115VU:
-put a warning notice to tell persons not to start the engine 1(2).
(4)
On the HP ground connector:
-put a warning notice to tell persons not to pressurize the pneumatic system.
(5)
On the maintenance panel 50VU:
-make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off,
-put a warning notice to tell persons not to energize the FADEC 1(2).
Subtask 36-11-58-865-050
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 11HA1
49VU AIR BLEED/ENG 1/CTL 3HA1 D12 49VU AIR BLEED/ENG 1/MONG 2HA1 D11
FOR 11HA2 122VU AIR BLEED/ENG 2/CTL 3HA2 Z23 122VU AIR BLEED/ENG 2/MONG 2HA2 Z22
R 1EFF : 151-199, 401-499, 1 36-11-58Page 402 1 1 Aug 01/05 1 1 1CES 1
Subtask 36-11-58-010-050
D. Get Access
(1)
Open the access doors :
FOR 11HA1
415AL, 415AR
FOR 11HA2
425AL, 425AR
(2)
Put the access platform in position below the engine.
4. Procedure
_________
(Ref. Fig. 401/TASK 36-11-58-991-001) Subtask 36-11-58-020-050
A. Removal of the HP Bleed Override Solenoid
(1)
Disconnect the electrical connector (3) from the HP bleed override solenoid (4).
(2)
Disconnect the sense line (7) from the HP bleed override solenoid (4).
(3)
Remove the three screws (2) and the three washers (1) that attach the HP bleed override solenoid (4).
(4)
Remove the HP bleed override solenoid (4) from the support (6).
(5)
Remove the seal (5) and discard it.
(6)
Put blanking caps on the disconnected electrical connectors.
(7)
Put blanking plugs on the disconnected line ends.
R 1EFF : 151-199, 401-499, 1 36-11-58Page 403 1 1 Aug 01/05 1 1 1CES 1
HP Bleed Override Solenoid
Figure 401/TASK 36-11-58-991-001
R 1EFF : 151-199, 401-499, 1 36-11-58Page 404 1 1 Aug 01/05 1 1 1CES 1
TASK 36-11-58-400-001
Installation of the HP Bleed Override Solenoid (11HA1, 11HA2)
WARNING : MAKE SURE THAT THE PNEUMATIC SYSTEM IS DEPRESSURIZED BEFORE YOU START
_______ WORK ON THE PNEUMATIC SYSTEM.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notice No specific access platform 3.5 m (11 ft. 6 in.) No specific Torque Wrench : range 36.00 to 220.00 lbf.in
(0.40 to 2.60 m.daN)
B. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
5 seal 36-11-06 06C-240
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM PNEUMATIC 氣源 2(48)
