(2)
Close the thrust reverser doors (Ref. TASK 78-36-00-410-040): FOR 1000EM1 451AL, 452AR FOR 1000EM2 461AL, 462AR
(3)
Remove the access platform(s).
Subtask 36-11-52-440-057
B. Make the thrust reverser serviceable (Ref. TASK 78-30-00-081-041).
Subtask 36-11-52-410-051
C. 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 warning notice(s).
1EFF : ALL 1 36-11-52Page 412 1 1 Aug 01/04R 1 1 1CES 1
Subtask 36-11-52-862-056
D. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
VALVE - BLEED PRESSURE REGULATOR (4001HA) - ADJUSTMENT/TEST
___________________________________________________________
TASK 36-11-52-790-001
Leak Test of the Bleed Pressure Regulator Valve (4001HA) with the Engine in Operation
1. Reason for the Job
__________________
Do this test after removal/installation of the bleed pressure regulator valve to make sure that:
-there are no leaks on the removed parts
-the electrical connectors are correctly installed.
You must start the engines to do this procedure.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform No specific warning notice R No specific FOIL-ALUMINUM (Local Purchase)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. CP3010 * developer, dry (Ref. 70-30-00) Material No. CP8004 * safetywire 0,024in. (0,6mm) (Ref. 70-30-00) R
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R R R R R R R R 24-41-00-861-002 24-41-00-862-002 31-60-00-860-001 31-60-00-860-002 71-00-00-710-003 71-00-00-710-004 71-00-00-710-028 71-13-00-010-040 71-13-00-410-040 78-30-00-081-041 78-30-00-481-041 78-36-00-010-040 78-36-00-410-040 Energize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External PowerEIS Start ProcedureEIS Stop ProcedureEngine Automatic StartEngine Manual StartEngine Shutdown Opening of the Fan Cowl Doors Closing of the Fan Cowl Doors Make the Thrust Reverser Serviceable after Maintenance Make the Thrust Reverser Unserviceable for Maintenance Opening of the Thrust Reverser Doors Closing of the Thrust Reverser Doors
3. Job Set-up__________
Subtask 36-11-52-861-062
A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
Subtask 36-11-52-860-068
B. Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).
Subtask 36-11-52-941-068
C. Safety Precautions
(1) Make sure that the engine 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 (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 HP ground connector: - put a warning notice to tell persons not to pressurize the pneumatic system.
R Subtask 36-11-52-010-081-A
R D. Get Access
R R R R R (1) Open the fan cowl doors (Ref. TASK 71-13-00-010-040): FOR 1000EM1 437AL, 438AR FOR 1000EM2 447AL, 448AR
R R (2) Put an access platform in position at the bleed pressure regulator valve.
R Subtask 36-11-52-040-082
R E. Make the thrust reverser unserviceable (Ref. TASK 78-30-00-481-041).
R Subtask 36-11-52-010-110
R R R R R F. Open the thrust reverser doors (Ref. TASK 78-36-00-010-040): FOR 1000EM1 451AL, 452AR FOR 1000EM2 461AL, 462AR
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