(1)
Disconnect the test set from the test port of the fan air valve.
(2)
Remove the blanking caps from the electrical connectors.
1EFF : ALL 1 36-11-54Page 508 1 1 Aug 01/05R 1 1 1CES 1
Subtask 36-11-54-420-052
B. Connect the Sense Line
(1)
Install the blanking plug on the test port of the fan air valve.
(2)
Remove the blanking plug from the union of the fan air valve.
(3)
Connect the sense line between the fan air valve and the control thermostat to the union of the fan air valve. TORQUE the nut to 141.6 lbf.in (1.60 m.daN).
R **ON A/C 004-049, 055-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 36-11-54-080-050-A
A. Disconnect the Test Set
(1) Disconnect the test set from the test intake of the fan air valve. Subtask 36-11-54-420-052-A
B. Connect the Sense Line
(1)
Install the blanking plug on the test intake of the fan air valve.
(2)
Remove the blanking plug from the union of the fan air valve.
(3)
Connect the sense line between the fan air valve and the control thermostat to the union of the fan air valve. TORQUE the nut to 141.6 lbf.in (1.60 m.daN).
**ON A/C ALL
Subtask 36-11-54-410-054
C. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Close the thrust reverser doors (Ref. TASK 78-36-00-410-040): FOR 1000EM1 451AL, 452AR FOR 1000EM2 461AL, 462AR
Subtask 36-11-54-440-051
D. Make the thrust reverser serviceable (Ref. TASK 78-30-00-081-041). Subtask 36-11-54-410-053
E. Close Access
(1)
Close the fan cowl doors (Ref. TASK 71-13-00-410-040):
FOR 1000EM1
437AL, 438AR
FOR 1000EM2
447AL, 448AR
(2)
Remove the access platform(s).
(3) Remove the warning notice(s). Subtask 36-11-54-862-051
F. De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
SOLENOID - BLEED PRESSURE REGULATOR VALVE CONTROL (10HA1,10HA2)
_______________________________________________________________ REMOVAL/INSTALLATION
____________________
TASK 36-11-55-000-001
Removal of the Bleed-Pressure-Regulator Valve Control-Solenoid (10HA1,10HA2)
WARNING : BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTER
_______ THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONE HOUR.
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific blanking caps
No specific blanking plugs
No specific circuit breaker(s) safety clip(s)
No specific warning notice
No specific access platform 1.5 m (4 ft. 11 in.)
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power R 36-11-55-991-001-A Fig. 401
3. Job Set-up
__________
Subtask 36-11-55-861-050
A. Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
Subtask 36-11-55-941-052
B. Safety Precautions
(1)
Make sure that the engine 1(2) shutdown occurred 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
(the OFF legend is on), R - make sure that the APU BLEED pushbutton switch is released (the OFF R legend is on),
-put a warning notice to tell persons not to operate the pneumatic system.
(3)
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. 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 2(42)
