3. Fault Confirmation
__________________
A. Read-out of ECB Trouble-Shooting Data
(1) Put the APU MASTER SW to the ON position.
(2) Get access to the APU SHUTDOWN report.
(3) Push the '>' adjacent to LRU DATA:
- the MCDU menu shows
OIL TEMP SENSOR SHOWS OUT OF RANGE HIGH
「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 A236
201-210, Config-1 Aug 01/05 CES
(4) Start the APU and apply Bleed Air for 20 seconds, minimum (Ref. AMM TASK 49-00-00-860-008).
4. Fault Isolation
_______________ R **ON A/C 001-049, 101-105, 107-107, 151-154, 201-207,
A. If an APU auto shutdown occurs during the APU operation and the APU SHUTDOWN report gives the maintenance message:
NO ACCELERATION
OIL TEMP SENSOR P11
associated with the Fault Code Number (FCN) 55
- do a check for damage/contamination of the electrical connector P11 of the OIL TEMP SENSOR (P11)
(1) If the electrical connector P11 is damaged/contaminated:
- do a repair/cleaning.
(2) If the electrical connector P11 is OK:
- use a multimeter to do a resistance check across pin A and pin B of the OIL TEMP SENSOR (P11).
(a) If the resistance value is > 200 Ohms:
- replace the OIL TEMP SENSOR (P11) (Ref. AMM TASK 49-94-15-000-001) and (Ref. AMM TASK 49-94-15-400-001).
(b) If the resistance value is in the specified limit:
- do a check and repair of the aircraft wiring from the ECB (59KD) AB/J5,B8 to the OIL TEMP SENSOR (P11) P11/A,B (Ref. ASM 49-61/01).
1 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).
**ON A/C 001-049, 101-105, 151-199, 201-210,
Post SB 49-1062 For A/C 001-049,101-105,151-154,201-207,
A. If an APU auto shutdown occurs during the APU operation and the APU SHUTDOWN report gives the maintenance message:
NOTE : With introduction of the ECB Software V2 the wording of the fault
____ message Oil Sump Temp Sensor (8084KM) is not correct. The functional item number of the Oil Temperature Sensor is (8092KM).
NO ACCELERATION
OIL SUMP TEMP SENSOR (8084KM)
「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 A237
201-210, Config-1 Aug 01/05 CES
associated with the Fault Code Number (FCN) 55
- do a check for damage/contamination of the electrical connector P11 of the OIL TEMP SENSOR (8092KM)
(1) If the electrical connector P11 is damaged/contaminated:
- do a repair/cleaning.
(2) If the electrical connector P11 is OK:
- use a multimeter to do a resistance check across pin A and pin B of the OIL TEMP SENSOR (8092KM)
(a) If the resistance value is > 200 Ohms:
- replace the OIL TEMP SENSOR (8092KM)
(Ref. AMM TASK 49-94-15-000-001) (Ref. AMM TASK 49-94-15-400-001).
(b) If the resistance value is in the specified limit:
- do a check and repair of the aircraft wiring from the ECB (59KD) AB/J5,B8 to the OIL SUMP TEMP SENSOR (8084KM) P11/A,B (Ref. ASM 49-61/01).
1 If the fault continues:
_
- replace the ECB (59KD)
(Ref. AMM TASK 49-61-34-000-003) (Ref. AMM TASK 49-61-34-400-003).
R **ON A/C 001-049, 101-105, 107-107, 151-199, 201-210,
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 A238
201-210, Config-1 Aug 01/05 CES
TASK 49-00-81-810-843
APU AUTO SHUTDOWN - INLET OVERHEAT, APU Inlet Temperature higher than Limit (131-9(A))
1. Possible Causes
_______________
- NO LRU FAULT DETECTED
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 機載輔助動力 2(86)
