ASM 21-61/01 ASM 21-61/01 ASM 21-61/02 ASM 21-61/02
3. Fault Confirmation
__________________Installation of the Water Extractor 10HM8 (11HM8)Removal of the Air Cycle Machine 10HM1 (11HM1)Installation of the Air Cycle Machine 10HM1 (11HM1)Removal of the Water Injector 20HM (21HM)Installation of the Water Injector 20HM (21HM)Removal of the Water-Extractor Temperature Sensors 11HH and 31HHInstallation of the Water-Extractor Temperature Sensors 11HH and 31HHRemoval of the Pack-Inlet Pressure Sensor 16HH (36HH)Installation of the Pack-Inlet Pressure Sensor 16HH (36HH)Removal of the Pack-Outlet Pneumatic Sensor 10HM10 (11HM10)Installation of the Pack-Outlet Pneumatic Sensor 10HM10 (11HM10)Removal of the Pack Controller (7HH, 27HH)Removal of the Air-Conditioning System Controller (47HH, 57HH)Installation of the Pack Controller (7HH, 27HH)Installation of the Air-Conditioning System Controller (47HH, 57HH)Removal of the Anti-Ice Valve 17HH (37HH)Installation of the Anti-Ice Valve 17HH (37HH)Removal of the Air-Inlet Flap MechanismInstallation of the Air-Inlet Flap MechanismRemoval of the Ram-Air OutletInstallation of the Ram-Air OutletFunctional Test of the Cockpit and Cabin Temperature Control without CFDS/MCDU.BITE Check Landing Gear Control Interface Unit (LGCIU) using MCDU to Ensure that Continuous BITE is Operative
**ON A/C 001-003, 051-054,
A. Test NOTE : Do the steps (6) and (7) in less than 120 s, if not, the control
____
of the zone temperature stabilizes. 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : ALL ∞∞21-61-00∞∞∞∞∞∞∞∞∞∞Page A241
Aug 01/05 CES
(1) Do the check of the ram-air inlet door mechanism for excessive backlash and of the ram-air outlet door mechanism for damage.
(2) Do the pre-conditioning with the APU (Ref. AMM TASK 12-33-21-618-001).
(3) Make sure that the pack 2 inlet-pressure indication on the ECAM BLEED page is > 20 PSI.
(4) Set the selectors COCKPIT, FWD CABIN and AFT CABIN, which are installed on the panel 30VU, to HOT for 10 minutes.
(5) Check of ram-air outlet airflow
WARNING : THE AIRFLOW CAN BE HOT.
_______
-HOT AIR CAN CAUSE BURNS.
(a) Do a check to see that there is airflow at the pack 2 ram-air outlet.
(6) Set the selectors COCKPIT, FWD CABIN and AFT CABIN to COLD.
(7) On the ECAM BLEED page do a check of the pack 2 discharge temperature (referred to as PDT 2).
NOTE : The PDT 2 increases regularly (because of the pack de-icing
____
operation).
R **ON A/C 004-049, 055-099, 101-149, 151-199, 201-299, 401-499,
A. Test NOTE : Do the steps (6) and (7) in less than 120 s, if not, the control
____
of the zone temperature stabilizes.
(1) Do the check of the ram-air inlet door mechanism for excessive backlash.
(2) Do the pre-conditioning with the APU (Ref. AMM TASK 12-33-21-618-001).
(3) Make sure that the pack 2 inlet-pressure indication on the ECAM BLEED page is > 20 PSI.
(4) Set the selectors COCKPIT, FWD CABIN and AFT CABIN, which are installed on the panel 30VU, to HOT for 10 minutes.
(5) Check of ram-air outlet airflow
WARNING : THE AIRFLOW CAN BE HOT.
_______
-HOT AIR CAN CAUSE BURNS.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞21-61-00∞∞∞∞∞∞∞∞∞∞Page A242
201-299, 401-499, Aug 01/05 CES
(a) Do a check to see that there is airflow at the pack 2 ram-air outlet.
(6) Set the selectors COCKPIT, FWD CABIN and AFT CABIN to COLD.
(7) On the ECAM BLEED page do a check of the pack 2 discharge temperature (referred to as PDT 2).
NOTE : The PDT 2 increases regularly (because of the pack de-icing
____
operation).
**ON A/C 301-399,
A. Test NOTE : Do the steps (6) and (7) in less than 120 s, if not, the control
____
of the zone temperature stabilizes.
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) AIR CONDITIONING 空調(diào)2(64)
