- If the fault continues:
- . replace the FUEL CONTROL UNIT (P19) (Ref. AMM TASK 49-32-11-000-003) and (Ref. AMM TASK 49-32-11-400-003).
- If the fault continues:
- . replace the FLOW DIVIDER (P13) (Ref. AMM TASK 49-32-13-000-001) and (Ref. AMM TASK 49-32-13-400-001).
- If the fault continues:
- . do a check for damage of the IGV ACTUATOR linkage and the IGV assembly
- If the IGV ACTUATOR linkage/IGV assembly are damaged and/or do not move freely:
- . replace the APU (4005KM).
- If the IGV ACTUATOR linkage/IGV assembly are OK:
- . replace the APU INLET PRESSURE TRANSDUCER (P22) (Ref. AMM TASK 49-51-21-000-001) and (Ref. AMM TASK 49-51-21-400-001).
- If the fault continues:
- . replace the APU INLET TEMPERATURE SENSOR (P6) (Ref. AMM TASK 49-23-14-000-001) and (Ref. AMM TASK 49-23-14-400-001).
- If the fault continues:
- . replace the ECB (59KD) (Ref. AMM TASK 49-61-34-000-003) and (Ref. AMM TASK 49-61-34-400-003).
- If the fault continues:
- . replace the EGT 1 and/or 2 THERMOCOUPLE (Ref. AMM TASK 49-72-15-000-002) and (Ref. AMM TASK 49-72-15-400-003).
d If the APU does not rotate freely:
_
- replace the APU (4005KM) (Ref. AMM TASK 49-11-11-000-004) and (Ref. AMM TASK 49-11-11-400-004).
「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, 151-154, 201-207, ∞∞49-00-81∞∞∞∞∞∞∞∞∞∞Page A206
Config-1 May 01/05 CES
R **ON A/C 107-107,
R A. If an APU auto shutdown occurs during the APU operation and the APU
R SHUTDOWN report gives the maintenance message:
R
R NO ACCELERATION
R FCU P19 / APU FUEL SUPPLY / STARTER MOTOR 8KA
R
R associated with Fault Code Number (FCN) 215
R
R (1) do a check for a blockage of the APU inlet.
R - If the fault continues:
R - check the APU accumulated hours TSN/TSO (Ref. AMM TASK 31-36-00-R 740-015).
R (a) If the accumulated hours TSN/TSO are greater than 2000 hours:
R - make sure that the APU rotates freely.
R 1_ If the APU rotates freely:
R - get acces to the APU DMM report (Ref. AMM TASK 49-00-00-970-R 001)
R - compare the value of CT5ATP (corrected EGT during MES) from
R the DMM pade versus 663 deg.C (1225 deg.F).
R a_ If EGTA exceeds 663 deg.C (1225 deg.F) then continue in
R para. 2_ .
R b_ If EGTA does not exceed 663 deg.C (1225 deg.F) then
R continue in para (b).
R 2_ Get acces to the APU DMM report (Ref. AMM TASK 49-00-00-970-R 001)
R - compare the START_TIME (time of last APU start) from the DMM
R page versus 60 seconds.
R a_ If START_TIME exceeds 60 seconds (slow start time) then
R continue in para. 3_ .
R b_ If START_TIME does not exceed 60 seconds then continue in
R para (b).
R 3_ Get acces to the APU SHUTDOWN report 14 (Ref. AMM TASK 31-36-R 00-740-011):
R - scan down and ensure that IGV position is within the normal
R range for APU start (10 - 22 degrees).
R a_ If IGV position is not in the normal range:
R - do a check for damage of the IGV actuator linkage and IGV
R assy (Ref. TASK 49-00-81-810-811).
「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 : 107-107, ∞∞49-00-81∞∞∞∞∞∞∞∞∞∞Page A207
Config-1 Aug 01/05 CES
R b_ If IGV position is in the normal range:
R - scan down to lines labled "8N" and "9N", or to lines
R where EGTA is highest.
R - compare APU speed (NA) and EGTA versus LCIT on Fig. 201.
R - . If EGTA exeeds value on Fig. 201
R - .. high EGT is determined (HOT SECTION DISTRESS).
R - .. replace the APU (4005KM) (Ref. AMM TASK 49-11-11-000-R 004) and (Ref. AMM TASK 49-11-11-400-004).
R - . If EGTA does not exeed value on Fig. 201 then continue
R in Para. (b).
R 4_ If the APU does not rotate freely:
R - replace the APU (4005KM) (Ref. AMM TASK 49-11-11-000-004)
R and (Ref. AMM TASK 49-11-11-400-004).
R (b) If the accumulated hours TSN/TSO are lower than 2000 hours:
R - replace the STARTER MOTOR (8KA) (Ref. AMM TASK 49-42-51-000-R 004) (Ref. AMM TASK 49-42-51-400-004).
R 1_ If the fault continues:
R - do a check of the aircraft BATTERIES (Ref. AMM TASK 24-38-R 00-210-001).
R 2_ If the fault continues:
R - do a check for damage/leakage of the APU fuel system.
R a_ If there is damage/leakage in the APU fuel system: 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 機載輔助動力 2(74)
