R Subtask 30-31-00-865-142
R R R R AL. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 2GA
5. Close-up________
Subtask 30-31-00-860-069
A. Make an entry in the logbook.
TASK 30-31-00-440-004 Reactivation 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
______________________
A. 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 TSM 30 PB 101 (for corrective action)
3. Job Set-up
__________ Subtask 30-31-00-861-058
A. Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
Subtask 30-31-00-941-059
B. Aircraft Maintenance Configuration
(1) On the panel 25VU:
-push the PROBE/WINDOW HEAT pushbutton switch (the ON legend comes on).
4. Procedure
_________ Subtask 30-31-00-810-053
A. Reactivation of the Heating of the Angle of Attack Sensors
(1) Do the trouble-shooting of the system (Ref. TSM 30 PB 101) and do the applicable corrective steps.
5. Close-up
________ Subtask 30-31-00-942-055
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 30-31-00-862-057
B. De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
TASK 30-31-00-040-005
Check of the ADR, CAPT (F/O, STBY) Probe Heaters and ECAM Warning Operation
1. Reason for the Job
__________________
Refer to the MMEL TASK: 30-31-01 b)c)
Probe Ice Protection
Probe Heat Computer
ADR, Heaters and Failure Warnings
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
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 30-31-00-710-001 Operational Test of the Probe Ice Protection 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure 32-69-00-860-001 Simulation of Flight, with the Aircraft on the Ground 34-13-00-740-003 SYSTEM TEST of the ADR
3. Job Set-up
__________
Subtask 30-31-00-861-059
A. Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
Subtask 30-31-00-860-070
B. Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).
4. Procedure_________
R R WARNING : DO NOT TOUCH THE PROBES IMMEDIATELY AFTER THE TEST._______ THEY ARE HOT AND CAN BURN YOU.
CAUTION : REMOVE THE PROTECTIVE COVERS FROM THE PROBES BEFORE YOU DO THE_______ TEST.
CAUTION : DO THE TEST AS QUICKLY AS POSSIBLE TO PREVENT DAMAGE TO THE_______ PROBES.
R
Subtask 30-31-00-710-060
A. Test.
(1) Do an operational test of the available probe ice-protection system (Ref. TASK 30-31-00-710-001).
(2) Do a SYSTEM TEST of the ADR (Ref. TASK 34-13-00-740-003).
R Subtask 30-31-00-750-050
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本文鏈接地址：A320飛機維護手冊 AMM ICE AND RAIN PROTECTION 防冰和排雨2(4)
