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R  30XN1 (30XN2). 
R  (13) TORQUE the screws (7) to between 0.17 and 0.19 m.daN (15.04 and 16.81 
R  lbf.in). 
R  Subtask 24-22-17-860-060 
R  C. Aircraft Maintenance Configuration 
R  FOR 41XU1, 41XU2 
R  (1) Energize the aircraft electrical circuits from the engine 1(2) 
R  (Ref. TASK 24-41-00-861-002). 
R  Subtask 24-22-17-860-061 
R  D. Aircraft Maintenance Configuration 
R  FOR 51XU1, 51XU2 
R  (1) Energize the aircraft electrical circuits from the external power 
R  (Ref. TASK 24-41-00-861-002). 
R  Subtask 24-22-17-865-051 
R  E. Make sure that this(these) circuit breaker(s) is(are) closed: 
R  -------------------------------------------------------------------------------
R  PANEL DESIGNATION IDENT. LOCATION 
R  -------------------------------------------------------------------------------
R  122VU ELEC/GALLEY/CNTOR 7MC S28 
R  122VU ELEC/GALY & CAB/CTL 1XA S26 
R  123VU FWD GALLEY/FEEDER F 16MC AC10 
R  123VU AFT GALLEY/FEEDER B 12MC AD09 
R  123VU FWD GALLEY/FEEDER D 2MC AD04 
R  123VU FWD GALLEY/FEEDER C 1MC AF09 
R  123VU AFT GALLEY/FEEDER E 14MC AF09 
R  123VU AFT GALLEY/FEEDER A 3MC AF04

 

R  Subtask 24-22-17-710-053 
R  F. Operational test 
R  (1) Do this test: 
R  -------------------------------------------------------------------------------
R  ACTION  RESULT 
R  -------------------------------------------------------------------------------

R  1. On the ECAM control panel:  On the lower ECAM display unit: 
R  - push the ELEC key to get the  - the ELEC page comes into view. 
R  ELEC page. 
R  2. On the ELEC panel 35VU:  On the panel 35VU: 
R  - push the GALY & CAB pushbutton  - the OFF legend of the GALY & CAB 
R  switch.  pushbutton switch goes off. 
R  On the lower ECAM display unit: 
R  - the white GALLEY SHED indication 
R  comes into view. 
R  3. In the FWD and/or AFT galleys:  On the lower ECAM display unit: 
R  - energize all the items of  - make sure that the electrical 
R  equipment.  parameters (load, voltage and 
R  frequency) of the GEN1(2) are 
R  correct. 
R  4. On the MCDU:  On the MCDU, on the AC GEN page: 
R  - do the operational test of the  - the TEST OK indication comes into 
R  Ground Auxiliary Power Control  view (after some seconds). 
R  Unit (GAPCU) (Ref. TASK 24-41-
R  00-740-002). 
R  Subtask 24-22-17-860-062 

R  G. Aircraft Maintenance Configuration 
R  FOR 41XU1, 41XU2 
R  (1) De-energize the aircraft electrical circuits supplied from the engine 
R  1(2) (Ref. TASK 24-41-00-862-002).

 

R  Subtask 24-22-17-860-063 
R  H. Aircraft Maintenance Configuration 
R  FOR 51XU1, 51XU2 
R  (1) De-energize the aircraft electrical circuits supplied from the 
R  external power (Ref. TASK 24-41-00-862-002). 
R  5. Close-up________ 
R  Subtask 24-22-17-410-052 
R  A. Close Access 
R  FOR 41XU1, 41XU2 
R  (1) Make sure that the work area is clean and clear of tool(s) and other 
R  items. 
R  (2) In the zone 130, install the ceiling panels 131MC 131PC and 131NC 
R  (Ref. TASK 25-54-12-400-002). 
R  (3) Remove the warning notice(s). 
R  (4) Close the cargo compartment door 825AR (Ref. TASK 52-30-00-860-002). 
R  (5) Remove the access platform. 
R  Subtask 24-22-17-410-053 
R  B. Close Access 
R  FOR 51XU1, 51XU2 
R  (1) Make sure that the work area is clean and clear of tool(s) and other 
R  items. 
R  (2) Remove the warning notice(s). 
R  (3) Close the access door 822. 
R  (4) Remove the access platform(s).

 

 SENSOR - TDC AC (50XU1,50XU2) - REMOVAL/INSTALLATION
____________________________________________________ TASK 24-22-18-000-001 Removal of the TDC AC Sensor 1(2) (50XU1, 50XU2)
 1.
　
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