. discrete outputs . power outputs for CFDS test only.
-External circuits: . integrity of probe heaters (CFDS test only).
B. Memory deletion is ensured by the ground/flight transition.
R **ON A/C 001-049, 051-060, 101-101,
C. Power-up Test Initialization and Cockpit Repercussions
(1)
Conditions of power-up test initialization
-de-energization time of computer: 3 s.
-A/C configuration:
-whatever the A/C configuration on ground.
(2)
Progress of power-up tests
-Duration: 9 s.
NOTE : In case at least one engine is in operation, duration: 14 s.
____
-Cockpit repercussions (ECAM warning, audio warning, pushbutton switch flashing, if any):
-none
(3) Results of power-up tests (cockpit repercussions, if any, in case of tests passed/tests failed)
(a)
Tests passed:
-none.
(b)
Tests failed:
-ECAM warning: (XX: CAPT, F/O or STBY)
-
ANTI-ICE XX PITOT
-
ANTI-ICE XX TAT
-
ANTI-ICE XX AOA
-
ANTI-ICE XX L STATIC
-
ANTI-ICE XX R STATIC
-
ANTI-ICE XX PROBES.
NOTE : - The PHC 1 controls the Captain and left systems.
____
-
The PHC 2 controls the First Officer and right systems.
-
The PHC 3 controls the Standby systems.
R 1EFF : 001-049, 051-060, 101-101, 1 30-31-00Page 20 1 1 May 01/05 1 1 1CES 1 PROBE ICE PROTECTION - DEACTIVATION/REACTIVATION
________________________________________________
TASK 30-31-00-040-001
Check of the Operation of the Probe Heating Channel
CAUTION : REMOVE THE PROTECTIVE COVERS FROM THE PROBES BEFORE YOU DO THE TEST.
_______
CAUTION : DO NOT CONTINUE THE TEST FOR MORE THAN ONE MINUTE TO PREVENT DAMAGE
_______
TO THE PROBES.
1. Reason for the Job
__________________
Refer to the MMEL TASK: 30-31-01 a)
Probe Ice Protection
Probe Heat Computer
Check of the associated heating channel.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notice
FOR FIN 6DA3
No specific thermometer
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
R 32-00-00-860-002 Ground Configuration after Flight Configuration with R Electrical Power 32-69-00-860-001 Simulation of Flight, with the Aircraft on the Ground
3. Job Set-up__________
Subtask 30-31-00-941-052
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2) On the panel 25VU: - make sure that the PROBE/WINDOW HEAT pushbutton switch is released (the ON legend is off).
(3) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).
4. Procedure_________
WARNING : DO NOT TOUCH THE PROBES IMMEDIATELY AFTER THE TEST._______ THEY ARE HOT AND CAN BURN YOU.
R Subtask 30-31-00-860-072
R A. Aircraft Maintenance Configuration
R R (1) Do the simulation of flight, with the aircraft on the ground (Ref. TASK 32-69-00-860-001).
R (2) On the ENG panel 115VU:
R R (a) Put a warning notice to tell persons that a flight configuration is simulated.
Subtask 30-31-00-865-058
R B. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 6DA1
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