pushbutton switch goes off. On the lower ECAM display unit:
-
the white GALLEY SHED indication comes into view.
On the lower ECAM display unit:
-make sure that the electricalparameters (load, voltage and frequency) of the GEN1(2) are correct.
On the MCDU, on the AC GEN page:
-the TEST OK message comes into view(after some seconds).
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-228, 301-302,
Subtask 24-22-17-860-052
K. Aircraft Maintenance Configuration
FOR 41XU1, 41XU2
(1) De-energize the aircraft electrical circuits supplied from the engine 1(2) (Ref. TASK 24-41-00-862-002).
Subtask 24-22-17-860-056
L. Aircraft Maintenance Configuration
FOR 42XU1, 42XU2, 42XU3, 42XU4
(1) De-energize the aircraft electrical circuits supplied from the external power (Ref. TASK 24-41-00-862-002).
5. Close-up
________ **ON A/C 001-049, 051-099, 101-105, 201-228, 301-302,
Subtask 24-22-17-410-050
A. Close Access
FOR 41XU1, 41XU2
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
In the zone 131, install the ceiling panels 131AC, 131BC, 131CC (Ref. TASK 25-54-12-400-002).
(3)
Remove the access platform(s).
(4)
Remove the warning notice(s).
(5) Close the access door 825AR (Ref. TASK 52-30-00-860-002). **ON A/C 151-199,
Subtask 24-22-17-410-050-A
A. Close Access
FOR 41XU1, 41XU2
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
In the zone 130, install the ceiling panels 131MC, 131NC, 131PC (Ref. TASK 25-54-12-400-002).
(3)
Remove the access platform(s).
(4)
Remove the warning notice(s).
(5) Close the access door 825AR (Ref. TASK 52-30-00-860-002). **ON A/C 001-049, 051-099, 101-105, 151-199, 201-228, 301-302,
Subtask 24-22-17-410-051
B. Close Access
FOR 42XU1, 42XU2, 42XU3, 42XU4
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
On the rear panel 120VU, close the panel which gives access to the AC power center 123VU.
(3)
Install the Third Occupant seat (Ref. TASK 25-11-41-400-001).
(4)
Remove the warning notice(s).
R **ON A/C 401-499,
R TASK 24-22-17-400-001-A
R Installation of the AC Current Transformers (41XU1, 41XU2, 51XU1, 51XU2)
R WARNING : MAKE SURE THAT NO AC OR DC POWER IS CONNECTED TO THE AIRCRAFT_______
R ELECTRICAL CIRCUITS.
R THERE IS A RISK OF ELECTROCUTION IF THE AC OR DC POWER STAYS
R CONNECTED.
R 1. Reason for the Job__________________
R Self Explanatory
R 2. Job Set-up Information______________________
R A. Fixtures, Tools, Test and Support Equipment
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R FOR FIN 41XU1, 41XU2
R No specific access platform 1.6 m (5 ft. 3 in.)
R FOR FIN 51XU1, 51XU2
R No specific cable ties
R No specific access platform 0.5 m (1 ft. 8 in.)
R No specific Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft)
R No specific Torque Wrench : range 0.20 to 3.60 m.daN
R (2.00 to 26.00 lbf.ft)
R FOR FIN 41XU1, 41XU2, 51XU1, 51XU2
R No specific warning notice(s)
R B. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R 24-41-00-740-002 R 24-22-17-991-001-A R FOR FIN 41XU1, 41XU2 R 24-41-00-861-002 R R 24-41-00-862-002 R R 25-54-12-400-002 R R 52-30-00-860-002 R R 24-22-17-991-002 R FOR FIN 51XU1, 51XU2 R 24-41-00-861-002 R R 24-41-00-862-002 R R 24-22-17-991-005
R 3. Job Set-up__________
R Subtask 24-22-17-010-056
R A. Get Access R FOR 41XU1, 41XU2 Operational Check of GAPCU via CFDS Fig. 401A
Energize the Aircraft Electrical Circuits from Engine 1(2) De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2) Installation of the Ceiling Panels in the FWD Cargo Compartment Close the FWD or AFT Cargo-Compartment Door with the Yellow Electric Pump Fig. 402
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