5. Close-up
________ Subtask 24-21-00-410-080
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Make the thrust reverser serviceable (Ref. TASK 78-30-00-081-041).

 (3)
 Close the fan cowl doors (Ref. TASK 71-13-00-410-040):

 -
FOR 1000EM1
 437AL, 438AR,

 -
FOR 1000EM2
 438AL, 448AR.

 (4) Remove the warning notice(s). Subtask 24-21-00-862-062
 B. De-energize the ground service network
 (Ref. TASK 24-42-00-862-001).

 INTEGRATED DRIVE GENERATOR SYSTEM (IDG, GCU) - ADJUSTMENT/TEST______________________________________________________________
 TASK 24-21-00-710-040
 Operational Test of the IDG Disconnect and Reconnect (Reset) Function - Engine Static
 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__________________
 Refer to the MPD TASK: 242100-04 To do a check of the IDG disconnect system and reset system.
 2. Job Set-up Information______________________ 
R  A. Fixtures, Tools, Test and Support Equipment 
R R R  -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R R  No specific  Torque Wrench : range 5.00 to 35.00 lbf.in (0.05 to 0.40 m.daN) 
R  B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 24-41-00-862-002 31-60-00-860-001 31-60-00-860-002 71-13-00-010-040 71-13-00-410-040  Energize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External PowerEIS Start ProcedureEIS Stop ProcedureOpening of the Fan Cowl DoorsClosing of the Fan Cowl Doors 
R  **ON A/C 401-499, 
R  24-21-00-991-922  Fig. 501

R **ON A/C ALL
 3. Job Set-up
__________
 Subtask 24-21-00-861-050
 A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits
 (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)
 On the ECAM control panel, push the ELEC key to get the ELEC page.

 Subtask 24-21-00-010-050
 B. Open the right fan cowl door (Ref. TASK 71-13-00-010-040):
 -
FOR 1000EM1
 438AR

 -
FOR 1000EM2
 448AR

 Subtask 24-21-00-865-050
 C. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------122VU ELEC/IDG2/DISC 2XT T25 122VU ELEC/IDG1/DISC 1XT T24
 Subtask 24-21-00-865-051
 D. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------122VU ELEC/GCU/2 2XU2 T27 122VU ELEC/GCU/1 2XU1 T26

 4. Procedure
_________
 CAUTION : ENGAGE THE IDG DISCONNECT MECHANISM WITH THE DISCONNECT RESET RING
_______ BEFORE YOU START THE ENGINE. IF NOT YOU WILL CAUSE DAMAGE TO THE DOG TEETH, AT ENGINE START.
 CAUTION : DO NOT PUSH THE IDG DISCONNECT PUSHBUTTON SWITCH FOR MORE THAN 3
_______ SECONDS. THERE MUST BE AT LEAST 60 SECONDS BETWEEN TWO OPERATIONS OF THE SWITCH. THIS IS TO PREVENT DAMAGE TO THE DISCONNECT SOLENOID WHICH WILL BECOME TOO HOT.

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 Subtask 24-21-00-710-050
 A. Operational Test of the IDG Disconnect and Reconnect Function
 NOTE : This test is for the system 1. For the other system(s), use the
____
 indications between the parentheses.

 NOTE : Two persons are necessary to do the test: one person holds the
____ disconnect reset ring while the other person pushes the IDG pushbutton switch in the cockpit on the ELEC control panel 35VU.
　
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