(9) Do the test in Para. 3.A.(1):
- if the fault continues, do the next step.
(10) Do a check of the aircraft wiring (Ref. ASM 30-11/01), and repair as necessary.
(11) Do the test in Para. 3.A.(1).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞30-11-00∞∞∞∞∞∞∞∞∞∞Page 206
Aug 01/05R
CES
Wing Anti-Ice High Pressure In Left (Right) System.
WARNING : DO NOT TOUCH THE ANTI-ICE DUCTS UNTIL THEY ARE COOL. THE TEMPERATURE
_______ OF THE DUCTS STAYS HIGH FOR SOME TIME AFTER THE ENGINE STOPS.
1. Possible Causes
_______________
- VALVE-WING ANTI ICE CONTROL, L (9DL)
- VALVE-WING ANTI ICE CONTROL, R (10DL)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 30-11-00-710-001 Operational Test of the Wing Ice-Protection System AMM 30-11-51-000-001 Removal of the Wing Anti-Ice Control Valve AMM 30-11-51-400-001 Installation of the Wing Anti-Ice Control Valve
3. Fault Confirmation
__________________
A. Procedure
(1) Do the operational test of the wing anti-ice system (Ref. AMM TASK 30-11-00-710-001).
4. Fault Isolation
_______________
A. Procedure
(1) If the ECAM shows the messages:
- WING A.ICE L(R) HI PR on the EWD
- WAI REGUL on the STATUS page.
(2) Replace the VALVE-WING ANTI ICE CONTROL, L (9DL) or VALVE-WING ANTI ICE CONTROL, R (10DL) (Ref. AMM TASK 30-11-51-000-001) and (Ref. AMM TASK 30-11-51-400-001).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞30-11-00∞∞∞∞∞∞∞∞∞∞Page 207
Aug 01/05R
CES Wing Anti-Ice Class 3 Faults.
1. Possible Causes_______________
- Wing Anti-Ice System
2. Job Set-up Information______________________ Not Applicable
3. Fault Confirmation__________________
A. Procedure
(1) Examine the ECAM for the Wing Anti-Ice System fault warning.
4. Fault Isolation_______________
A. Procedure
(1) If the ECAM shows the Wing Anti-Ice System warning, do the trouble shooting procedure related to the maintenance message.
(2) If the ECAM shows no Wing Anti-Ice System warning, the CFDS message can be regarded as spurious and requires no further action.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞30-11-00∞∞∞∞∞∞∞∞∞∞Page 208
Aug 01/05R
CES
Wing Anti-Ice Control-Valves Do Not Operate.
WARNING : DO NOT TOUCH THE ANTI-ICE DUCTS UNTIL THEY ARE COOL. THE TEMPERATURE
_______
OF THE DUCTS STAYS HIGH FOR SOME TIME AFTER THE ENGINE STOPS.
1. Possible Causes
_______________
- C/B-ANTI-ICE/WING/CTL 2DL
- P/BSW ANTI ICE/WING 3DL
- RELAY ANTI ICE VALVE CONTROL 5DL
- RELAY GROUND TEST (4DL)
- aircraft wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
30-11-00-810-809 Wing Anti-Ice (Wing) Circuit Breaker 2DL Tripped AMM 30-11-00-710-001 Operational Test of the Wing Ice-Protection System AMM 32-69-00-860-001 Simulation of Flight, with the Aircraft on the Ground ASM 30-11/01
3. Fault Confirmation
__________________
A. Procedure
(1) Do the operational test of the wing anti-ice system (Ref. AMM TASK 30-11-00-710-001).
4. Fault Isolation
_______________
A. Procedure
(1) If the test is not OK go to para (2).
If the test is OK:
(a) Do a check of the aircraft wiring from the relay anti-ice control 5DL to the LGCIU 1 and LGCIU 2. (Ref. ASM 30-11/01).
(b) Repair the unservicable wiring/connectors. CAUTION : MAKE SURE THAT YOU SET THE WING ANTI-ICE SYSTEM P/BSW
_______ TO OFF AFTER 30 SECONDS. THIS WILL PREVENT DAMAGE TO THE SLATS.
Aug 01/05R CES
