B. If the APU GND SCANNING menu gives the maintenance message:
IGV ACTUATOR (8014KM)
associated with Fault Code Number (FCN) 82
- do a check for damage/contamination of electrical connector P21 of the IGV ACTUATOR (8014KM)
(1) If the electrical connector P21 is damaged/contaminated:
- do a repair/cleaning.
(2) If the electrical connector is OK:
- use a multimeter to do a resistance check across pin 2 and pin 5 of the IGV ACTUATOR (P21).
(a) If the resistance is not between 10 Ohms and 100 Ohms:
- replace the IGV ACTUATOR (8014KM) (Ref. AMM TASK 49-23-51-000-004) and (Ref. AMM TASK 49-23-51-400-004).
(b) If the resistance is between 10 Ohms and 100 Ohms:
- do a check and repair of the aircraft wiring from the ECB (59KD) AB/E11,E12 to the IGV ACTUATOR (8014KM) P21/2,5 (Ref. ASM 49-61/02).
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).
R **ON A/C 001-049, 101-105, 107-107, 151-199, 201-210,
C. Do a check of the APU GND SCANNING menu to verify the fault is not present.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 101-105, 107-107, 151-199, ∞∞49-00-81∞∞∞∞∞∞∞∞∞∞Page A291
201-210, Config-1 Aug 01/05 CES
TASK 49-00-81-810-859
Fuel-Control Unit (P19) Fault (131-9(A))
1. Possible Causes
_______________
- FUEL TEMP SENSOR SHOWS OUT OF RANGE LOW
- FUEL TEMP SENSOR SHOWS OUT OF RANGE HIGH
- damage/contamination of electrical connector P19
- FUEL CONTROL UNIT (P19)
- aircraft wiring
- ECB (59KD)
- FUEL CONTROL UNIT (8022KM)
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific multimeter
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 49-32-11-000-003 Removal of the Fuel Control Unit (FCU) (8022KM) (131-9(A)) AMM 49-32-11-400-003 Installation of the Fuel Control Unit (FCU) (8022KM) (131-9(A)) AMM 49-61-34-000-003 Removal of the Electronic Control Box (ECB) (131-9(A)) AMM 49-61-34-400-003 Installation of the Electronic Control Box (ECB) (131-9(A)) ASM 49-61/02
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 LAST LEG/PREVIOUS LEG report.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 101-105, 107-107, 151-199, ∞∞49-00-81∞∞∞∞∞∞∞∞∞∞Page A292
201-210, Config-1 Aug 01/05 CES
(3) Push the '>' adjacent to the related CFDS failure message:
- the MCDU menu shows:
FUEL TEMP SENSOR SHOWS OUT OF RANGE LOW
or
FUEL TEMP SENSOR SHOWS OUT OF RANGE HIGH
(4) Get access to the APU GND SCANNING menu.
4. Fault Isolation
_______________ R **ON A/C 001-049, 101-105, 107-107, 151-154, 201-207,
A. If the APU GND SCANNING menu gives the maintenance message:
FUEL CONTROL UNIT P19
associated with Fault Code Number (FCN) 51 or 52
- do a check for damage/contamination of electrical connector P19 of the FUEL CONTROL UNIT (P19)
(1) If the electrical connector P19 is damaged/contaminated:
- do a repair/cleaning.
(2) If the electrical connector is OK:
- use a multimeter to do a resistance check across pin 4 and pin 5 of the FUEL CONTROL UNIT (P19).
(a) If the resistance value is not between 72 Ohms to 200 Ohms:
- replace the FUEL CONTROL UNIT (P19) (Ref. AMM TASK 49-32-11-000-003) and (Ref. AMM TASK 49-32-11-400-003).
(b) If the resistance value is between 72 Ohms to 200 Ohms:
- do a check and repair of the aircraft wiring from the ECB (59KD) AB/C3,C4 to the FUEL CONTROL UNIT (P19) P19/4,5 (Ref. ASM 49-61/02).
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).
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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(107)
