(3)
Remove the warning notice(s).
(4)
Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
WING ICE PROTECTION - ADJUSTMENT/TEST
_____________________________________
TASK 30-11-00-710-001
Operational Test of the Wing Ice-Protection System
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
_______ GEAR.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers No specific warning notices No specific Ground Air Power Cart 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure 32-00-00-481-001 Installation of the Safety Devices on the Landing
Gears
1EFF : ALL 1 30-11-00Page 501 1 1 Nov 01/04R 1 1 1CES 1
-------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
49-00-00-710-008 Operational Test of the APU (APS 3200)
49-00-00-710-010 Operational Test of the APU (131-9(A))
71-00-00-710-003 Engine Automatic Start
TSM 21 PB 101
30-11-00-991-001 Fig. 501
3. Job Set-up__________
Subtask 30-11-00-941-067
A. Safety Precautions
(1) Put the safety barriers in position.
(2) Make sure that the ground safety locks are installed on the landing gear (Ref. TASK 32-00-00-481-001).
R (3) Put warning notices in the cockpit to tell persons not to operate the slats and the pneumatic systems.
Subtask 30-11-00-860-059-B
B. Aircraft Maintenance Configuration
R R (1) Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the slat/flap control lever.
(2) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
R R R R NOTE : You can do the Operational Test of the Wing Ice-Protection____ System with a bleed air supply from one of these sources: - one engine - the Ground Air Power Cart (GAPC) - the APS 3200 APU or 131-9(A) APU.
R R R NOTE : Do not use the GTCP 36-300 APU bleed air supply to do the____ test. The GTCP 36-300 APU bleed air system does not supply sufficient pressure for the test procedure.
NOTE : Access to the wing anti-ice system on the CFDS is through the____ TEMP CTL of the air-conditioning class 3 faults (Ref. TSM 21 PB 101).
(3) Do the EIS start procedure (ECAM only) (Ref. TASK 31-60-00-860-001).
R R (4) On the ECAM control panel (CP), push (in) the BLEED P/BSW.
(5) If the source of power is the aircraft engines:
(a) Operate Engine 1 or Engine 2 (Ref. TASK 71-00-00-710-003).
NOTE : The operational test does not continue satisfactorily with____ the two Engines in operation.
R R R (b) On the AIR COND panel 30VU, put the X BLEED switch in the OPEN position.
(c) Make sure that the bleed air pressure is between 2.8 bar (40.6105 psi) and 3.2 bar (46.4120 psi).
R (6) If the source of power is the Ground Air Power Cart (GAPC):
(a) On the AIR COND panel 30VU: - release (out) the PACK 1 and PACK 2 P/BSW's - make sure that the OFF lights are on.
R (b) Open the access panel 191DB.
R (c) Connect the GAPC to the HP connection.
R (d) Operate the GAPC to give a bleed air supply.
R R (e) On the AIR COND panel 30VU, put the X BLEED switch in the OPEN position.
R R R (f) Make sure that the bleed air pressure is between 2.8 bar (40.6105 psi) and 3.2 bar (46.4120 psi).
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