(4)
 Remove the access platform(s).

 1EFF : ALL 1 52-32-00Page 412 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL

 TASK 52-32-00-440-003 Reactivation of the Locking Hooks and Spools
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
52-30-00-860-001 Open the FWD or AFT Cargo-Compartment Door with the
 Yellow Electric Pump 52-32-21-400-007 Installation of the Locking Unit 52-32-32-400-001 Installation of the Lock Fitting Components
 3. Job Set-up
__________ Subtask 52-32-00-860-061
 A. Make sure that the AFT cargo-compartment door is fully opened and
 safetied with the support struts (Ref. TASK 52-30-00-860-001).

 4. Procedure
_________ Subtask 52-32-00-420-053
 A. Install the replacement spool (Ref. TASK 52-32-32-400-001) and/or
 replacement locking hook (Ref. TASK 52-32-21-400-007).

 1EFF : ALL 1 52-32-00Page 413 1 1 May 01/05 1 1 1CES 1 AFT CARGO COMPARTMENT DOOR - ADJUSTMENT/TEST

____________________________________________
 TASK 52-32-00-710-001
 Operational Test of the AFT Cargo-Compartment Door
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 2.0 m (6 ft. 7 in.)
 B. 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 29-14-00-614-002 Pressurization of the Hydraulic Reservoirs through
 the Ground Connector 29-24-00-864-001 Depressurize the Yellow Hydraulic System 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure 52-30-00-860-002 Close the FWD or AFT Cargo-Compartment Door with the
 Yellow Electric Pump
 1EFF : ALL 1 52-32-00Page 501 1 1 Feb 01/98 1 1 1CES 1

 3. Job Set-up
__________
 Subtask 52-32-00-010-050

 A. Get Access
 (1)
 Make sure that the AFT cargo compartment door (referred to as cargo door) is closed (Ref. TASK 52-30-00-860-002).

 (2)
 If necessary, put the access platform in position below the closed cargo door.

 (3)
 Open the access panel 154AR to get access to the selector of the control panel.

 Subtask 52-32-00-865-050
 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU HYDRAULIC/HYD POWER/Y 3803GX N30 122VU DOORS/CARGO 1MJ T12 123VU Y HYD/ELEC/PUMP 3802GX AB06
R 123VU Y HYD/ELEC/ELEC PUMP/NORM 3801GX AB03
 Subtask 52-32-00-860-050
 C. Aircraft Maintenance Configuration
 (1)
 Make sure that the aircraft electrical circuits are energized (Ref. TASK 24-41-00-861-002).

 (2)
 Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).

 (3)
 Make sure that the Yellow hydraulic system reservoir is pressurized (Ref. TASK 29-14-00-614-002).

 1EFF : ALL 1 52-32-00Page 502 1 1 Feb 01/99 1 1 1CES 1

 4. Procedure
_________ R **ON A/C 001-049, 053-061, 101-105, 201-203,
 Subtask 52-32-00-710-050-A
 A. Do this test:
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the AFT cargo door:  On the AFT cargo door:
 - push the handle flap in and pull the door handle away from the recess of the door structure.  - the vent door opens inboards,- the drift pins retract from thepockets of the fuselage,- you can see the red mark on each safety cam through the indication window.
　
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