(6) Do the pre-conditioning with the APU (Ref. AMM TASK 12-33-21-618-001) and make sure that you do not smell fumes in the cabin and/or there is no oil smoke at the APU exhaust.

 - if you smell smoke in the cabin, do the applicable trouble shooting procedure(Ref. TASK 49-00-81-810-874).

 (7) Do a leak check and make sure that there is no fuel leak and/or no oil leak on the APU and/or the APU generator.

 NOTE : Do the leak check with a black light lamp.
____
 「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, 101-105, 107-107, 151-199, ∞∞49-00-81∞∞∞∞∞∞∞∞∞∞Page B249
 201-210, Config-1 Aug 01/05 CES

 TASK 49-00-81-810-890

 APU Generator electrical-parameter indication(s) replaced by amber XX
 (131-9(A))

 1. Possible Causes
_______________
 - GCU-APU (1XS)

 - EGIU-2 (22XU2)

 - connection between the EGIU-2 (22XU2) and the SDAC 1 and 2 (1WV1(2)) and/or the APU GCU (1XS)

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-22-00-810-808 APU GEN Voltage, Frequency and Load Indication Lost
 or Incorrect
 AMM 24-22-33-000-001 Removal of the EGIU-1(2) (22XU1, 22XU2)
 AMM 24-22-33-400-002 Installation of the EGIU-1(2) (22XU1, 22XU2)
 AMM 24-23-34-000-001 Removal of the GCU-APU (1XS)
 AMM 24-23-34-400-001 Installation of the GCU-APU (1XS)
 AMM 49-00-00-710-010 Operational Test of the APU (131-9(A))

 3. Fault Confirmation
__________________
 A. Do the operational test of the APU (Ref. AMM TASK 49-00-00-710-010). Do a check of the APU GEN electrical-parameter indications on the lower ECAM DU (APU Page).
 4. Fault Isolation
_______________
 A. Maintenance Action
 (1) If all electrical parameter indications are replaced by amber XX:

 - do the trouble shooting of the connection between the EGIU-2 (22XU2) and the SDAC 1 and 2 (1WV1(2)) and/or the APU GCU (1XS) (Ref. TASK 24-22-00-810-808).

 (2) If one or two electrical parameter indications are replaced by amber

 XX:
 - replace the GCU-APU (1XS) (Ref. AMM TASK 24-23-34-000-001) and (Ref. AMM TASK 24-23-34-400-001).
 (a) If the fault continues:
R  - replace the EGIU-2 (22XU2) (Ref. AMM TASK 24-22-33-000-001) and (Ref. AMM TASK 24-22-33-400-002).
 「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, 101-105, 107-107, 151-199, ∞∞49-00-81∞∞∞∞∞∞∞∞∞∞Page B250
 201-210, Config-1 Aug 01/05 CES

 B. Do the test given in para. 3.

 「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, 101-105, 107-107, 151-199, ∞∞49-00-81∞∞∞∞∞∞∞∞∞∞Page B251
 201-210, Config-1 Aug 01/05 CES

R TASK 49-00-81-810-891
R No APU Bleed-Air Pressure, Low or Fluctuating APU Bleed-Air Pressure (with AIDS R Support) (131-9)(A))
R 1. Possible Causes
_______________
R - IGV ACTUATOR P21
R - APU
R - APU BLEED CHECK-VALVE (7260HM)
R - tube of the DIFFERENTIAL PRESSURE TRANSDUCER (P24)
R - tube of the TOTAL PRESSURE TRANSDUCER (P23)
R - DIFFERENTIAL PRESSURE TRANSDUCER (P24)
R - TOTAL PRESSURE TRANSDUCER (P23)
R - damage/leakage of the fuel supply and return lines of the SCV
R - SURGE CONTROL VALVE (P18)
R - ECB (59KD)
R - LOAD CONTROL VALVE P12
R - aircraft wiring
R - INLET TEMP SENSOR (P6)
R - IGV ACTUATOR 8014KM
R - tube of the DIFFERENTIAL PRESSURE TRANSDUCER (8043KM)
R - tube of the TOTAL PRESSURE TRANSDUCER (8044KM)
R - DIFFERENTIAL PRESSURE TRANSDUCER (8043KM)
R - TOTAL PRESSURE TRANSDUCER (8044KM)
R - SURGE CONTROL VALVE (8058KM)
R - LOAD CONTROL VALVE (8050KM)
R - INLET TEMP SENSOR (8010KM)
R - STARTER SHUTOFF VALVE (SAV)
R - aircraft bleed system
R - PACK-FLOW CONTROL VALVE (8HB)
R - PACK-FLOW CONTROL VALVE (11HB)
R - blockade of the Pack Heat Exchanger(s)

R 2. Job Set-up Information______________________
R A. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
　
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