-------------------------------------------------------------------------------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 TSM 30 PB 101 (for corrective action)
3. Job Set-up
__________ Subtask 30-31-00-861-057
A. Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
Subtask 30-31-00-941-057
B. Aircraft Maintenance Configuration
(1) On the panel 25VU:
-push the PROBE/WINDOW HEAT pushbutton switch (the ON legend comes on).
4. Procedure
_________ Subtask 30-31-00-810-052
A. Reactivation of the Heating of the Static Probes
(1) Do the trouble-shooting of the system (Ref. TSM 30 PB 101) and do the applicable corrective steps.
1EFF : ALL 1 30-31-00Page 427 1 1 May 01/05R 1 1 1CES 1
5. Close-up
________ Subtask 30-31-00-942-054
A. Put the aircraft back to its initial configuration.
(1) On the panel 25VU:
-release the PROBE/WINDOW HEAT pushbutton switch (the ON legend goes off).
Subtask 30-31-00-862-056
B. De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
1EFF : ALL 1 30-31-00Page 428 1 1 May 01/05R 1 1 1CES 1
TASK 30-31-00-040-004
Deactivation of the Heating of the Angle of Attack Sensors
1. Reason for the Job__________________
Refer to the MMEL TASK: 30-31-04 Probe Ice Protection Angle-of-attack Probe Heating
2. Job Set-up Information______________________
R A. Fixtures, Tools, Test and Support Equipment
R R R -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R No specific circuit breaker(s) safety clip(s)
R B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R 30-31-00-710-001 32-69-00-860-001 34-13-00-740-002 34-13-00-740-003 Operational Test of the Probe Ice Protection Simulation of Flight, with the Aircraft on the GroundINTERFACE TEST of the ADRSYSTEM TEST of the ADR
3. Job Set-up__________
Subtask 30-31-00-941-058
A. Safety Precautions
(1) On the panel 25VU: - make sure that the PROBE/WINDOW HEAT pushbutton switch is released (the ON legend is off).
4. Procedure
_________ R **ON A/C 001-049, 101-105, 151-199, 201-210, 301-399, 401-499,
Subtask 30-31-00-710-059-A
A. Test
(1) Do an operational test of the available probe ice protection systems (Ref. TASK 30-31-00-710-001).
(2) Do a SYSTEM TEST of the ADR (Ref. TASK 34-13-00-740-003).
**ON A/C 051-099, 106-149, 211-299,
Subtask 30-31-00-710-059
A. Test
(1) Do an operational test of the available probe ice protection systems (Ref. TASK 30-31-00-710-001).
(2) Do an INTERFACE TEST of the ADR (Ref. TASK 34-13-00-740-002).
**ON A/C ALL
Subtask 30-31-00-750-053
B. Check of ECAM Warning Messages
(1) Do a check of the ECAM warning messages related to the systems that operate correctly.
Subtask 30-31-00-865-122
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 6DA1
49VU ANTI ICE/PROBES/AOA/1 4DA1 D04 49VU ANTI ICE/PROBES/PITOT/1 3DA1 D02
R Subtask 30-31-00-869-103
R D. Check
R (1) On the upper ECAM DU:
R - make sure that the
R ANTI ICE CAPT PITOT
R ANTI ICE CAPT AOA
R indications come into view.
R Subtask 30-31-00-865-123
R E. Remove the safety clip(s) and the tag(s) and close this(these) circuit
R breaker(s):
R FOR 6DA1
R 3DA1, 4DA1.
R Subtask 30-31-00-865-124
R F. Open, safety and tag this(these) circuit breaker(s):
R -------------------------------------------------------------------------------
R PANEL DESIGNATION IDENT. LOCATION
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