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R 
R  d_  Look at the RAT and see if it turns.
R 
R  e_  On the overhead panel 40VU, push and release the BLUE ELEC
R  PUMP P/BSW. Make sure that the OFF light comes on. 
R 
R  f_  If the RAT turns, there is a fault in the GCM which you
R  must repair before dispatch of the aircraft. 
R 
R  g_  If the RAT does not turn, there is a defect in the wiring
R  associated with the connectors 2454GE-C or 2027GE-A. If 
R  necessary, deactivate the fault warning from them as 
R  follows: 
R  - Put blanking caps on the diconnected electrical 
R  connectors. 
R 
R  - Use tie-wraps and attach the two connectors and the 
R  cables to adjacent parts of the structure. 
R  5_ If it is installed, remove the PROTECTION EQUIPMENT - RAT
 (98D29207550001). 
R  6_ Retract the RAT (Ref. TASK 29-22-00-869-002).
 5. Close-up________
 Subtask 29-30-00-410-054
 A. Close Access
 (1) Make sure that the work area is clean and clear of tool(s) and other
 items.
 (2) Close the cover of the RAT control panel 2815GE.
 (3) Close the access panels 195BB and 197EB. 

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 B. Put the aircraft back to the serviceable condition.
 (1)
 Do the EIS stop procedure
 (Ref. TASK 31-60-00-860-002).

 (2)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

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 TASK 29-30-00-440-001 Reactivation of RAT Fault Warning on the ECAM Upper Display Unit
 1. Reason for the Job
__________________
 Refer to the MMEL TASK: 29-30-04-H)
 Indicating - Warning and Caution on ECAM
 RAT FAULT

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
 External Power TSM 290000500 (for corrective action) 29-30-00-991-003 Fig. 402
 3. Job Set-up
__________ Subtask 29-30-00-010-052
 A. Open the access door 195BB.
 4. Procedure
_________ (Ref. Fig. 402/TASK 29-30-00-991-003) Subtask 29-30-00-440-050
 A. Reactivation of the RAT Fault Warning
 (1)
 Find the electrical connector(s) which is/are disconnected (2455GE-A, 2454GE-C and/or 2027GE-A).

 (2)
 Cut and remove the tie-wrap which attaches it/them to the structure.

 (3)
 Remove the blanking caps from the electrical connector(s) and receptacle(s).

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 (4)
 Connect the electrical connector(s) to the correct receptacles:

 -2455GE-A to the jack control module,
 -2454GE-C to the ejection jack,
 -2027GE-A to the ground check module.

 (5)
 Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

 (6)
 Trouble-shoot the RAT system (Ref. TSM 290000500).

 (7)
 Do the necessary corrective actions.

 5. Close-up
________ Subtask 29-30-00-410-055
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Close the access panel 195BB.

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 TASK 29-30-00-040-002
 Deactivation of RAT Fault Warning on the ECAM Upper Display Unit

 1. Reason for the Job
__________________
 Refer to the MMEL TASK: 29-30-04-H)
 Indicating - Warning and Caution on ECAM
 RAT FAULT

 NOTE : Use this procedure together with the Master Minimum Equipment List
____ (MMEL). If the fault indication is because of a defect in the indication system, it is permitted to dispatch the aircraft. It is not permitted to dispatch the aircraft if the fault indication is because of a defect which could prevent operation of the RAT.
　
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