R 1EFF : ALL 1 30-11-00Page 503 1 1 Nov 01/04 1 1 1CES 11. On the panel 25VU:
R R R R (b) Do an operational test of the APU: - for the APS 3200 APU (Ref. TASK 49-00-00-710-008) - for the 131-9(A) APU (Ref. TASK 49-00-00-710-010).
4. Procedure_________
(Ref. Fig. 501/TASK 30-11-00-991-001)
Subtask 30-11-00-710-050
A. Operational Test of Wing Ice-Protection System
(1) Do this test:
NOTE : This test will only operate for 30 seconds. This is to protect____ the slat structure.
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
-
Put the ANN LT switch to the TEST position.
-
Put the ANN LT switch to the BRT or DIM position.
-Push (in) the ANTI ICE WING P/BSW.
-
the cockpit panel P/BSW lights comeon.
On the panel 25VU:
-
the ANTI ICE WING P/BSW FAULT and ON lights come on.
-
the ANTI ICE WING P/BSW FAULT and ONlights goes off.
-
the ANTI ICE WING P/BSW ON lightcomes on
-
the ANTI ICE WING P/BSW FAULT light comes on momentarily and then goes off.
On the ECAM lower DU:
-
the left and right ANTI ICE legends come on
-in less than 3 seconds, the left and right anti-ice symbols come on (green)
R 1EFF : ALL 1 30-11-00Page 504 1 1 Nov 01/04 1 1 1CES 1
Wing-Ice Protection - Indications Figure 501/TASK 30-11-00-991-001
1EFF : 1 1R 1CES ALL 1 11 1 30-11-00 Page 505 Nov 01/04
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
-Release (out) the ANTI ICE WING P/BSW.
5. Close-up
________
R
Subtask 30-11-00-860-060-B
-
after 10 seconds, the left and right anti-ice symbols become amber
-
after 31 seconds, the ANTI ICE legends and symbols go off.
On the panel 25VU:
-the ANTI ICE WING P/BSW ON light goes off.
A. Aircraft Maintenance Configuration
R (1) If the source of power is the Engine 1 or Engine 2:
R (a) On the AIR COND panel 30VU, put the X BLEED switch in the AUTO
R position.
R
(b) Stop Engine 1 or Engine 2 (Ref. TASK 71-00-00-710-003).
R (2) If the source of power is the APS 3200 APU or 131-9(A) APU:
R (a) Stop the APU:
R - for the APS 3200 APU (Ref. TASK 49-00-00-710-008)
R - for the 131-9(A) APU (Ref. TASK 49-00-00-710-010).
R (b) On the AIR COND panel 30VU:
R - push (in) the PACK 1 and PACK 2 P/BSW's
R - make sure that the OFF lights are off.
(3) If the source of power is the GAPC:
R (a) On the AIR COND panel 30VU, put the X BLEED switch in the AUTO
R position.
R
(b) Stop the GAPC.
(c) Disconnect the GAPC from the aircraft ground HP connection.
R (d) Close the access panel 191DB.
R (e) On the AIR COND panel 30VU: - push (in) the PACK 1 and PACK 2 P/BSW's - make sure that the OFF lights are off.
R R (4) On the ECAM control panel (CP), release (out) the BLEED P/BSW.
R (5) Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
R R (6) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
Subtask 30-11-00-942-065
B. Removal of Equipment
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Remove the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001).
(3) Remove the warning notice(s).
(4) Remove the safety barriers.
(5) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
TASK 30-11-00-790-001 Leak Test of the Wing Anti-Ice Ducts WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE. WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
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