TASK 49-70-00-810-817
EGT TCPLE Rake 1 Fault (131-9(A))
1. Possible Causes
_______________
- EGT1 SENSOR SHOWS OUT OF RANGE LOW
- EGT1 SENSOR DISAGREES WITH EGT2 SENSOR > 66C
- damage/contamination of the electrical connections
- EGT 1 THERMOCOUPLE
- aircraft wiring
- ECB (59KD)
- EGT 2 THERMOCOUPLE
- PRIMARY FUEL-NOZZLE and MANIFOLD
- SECONDARY FUEL-NOZZLE and MANIFOLD
- EGT TCPLE RAKE (8057KM1)
- EGT TCPLE RAKE (8057KM2)
- PRIMARY FUEL-NOZZLE and MANIFOLD (8020KM)
- SECONDARY FUEL-NOZZLE and MANIFOLD (8021KM)
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific multimeter
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
49-70-00-810-818 EGT TCPLE Rake 2 Fault (131-9(A))
AMM 49-00-00-860-008 APU Start by External Power (131-9(A))
AMM 49-31-41-000-003 Removal of the Primary and Secondary Fuel-Nozzle
(131-9(A)) AMM 49-31-41-400-003 Installation of the Primary and Secondary Fuel-Nozzle (131-9(A)) AMM 49-31-42-000-004 Removal of the Primary and Secondary Fuel-Manifold (8020KM) and (8021KM) (131-9(A)) AMM 49-31-42-400-006 Installation of the Primary and Secondary Fuel-Manifold (8020KM) and (8021KM) (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)) AMM 49-72-15-000-002 Removal of the Thermocouples (8057KM) (131-9(A)) AMM 49-72-15-400-003 Installation of the Thermocouples (8057KM) (131-9(A)) -------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
ASM 49-61/01
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.
(3) Push the '>'-key adjacent to the related CFDS failure message.
(4) If the MCDU menu shows:
EGT1 SENSOR SHOWS OUT OF RANGE LOW
- do the Fault Confirmation that follows:
(a) Get access to the APU GND SCANNING menu.
(5) If the MCDU menu shows:
EGT1 SENSOR DISAGREES WITH EGT2 SENSOR 66C
- do the Fault Confirmation that follows:
(a) Start the APU and apply Electrical Load and Bleed Air (Ref. AMM TASK 49-00-00-860-008).
(b) 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:
EGT TCPLE RAKE 1
associated with Fault Code Number (FCN) 42
- do a check for damage/contamination of the electrical connections of the EGT 1 THERMOCOUPLE.
(1) If the electrical connection of the EGT 1 THERMOCOUPLE is damaged/contaminated:
- do a repair/cleaning.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 101-105, 107-107, 151-199, ∞∞49-70-00∞∞∞∞∞∞∞∞∞∞Page 207
201-210, Config-2 Aug 01/05 CES
(2) If the electrical connections of the EGT 1 THERMOCOUPLE is OK:
- use a multimeter to do a resistance check across the terminals chromel and alumel of the EGT 1 THERMOCOUPLE.
(a) If the resistance is >20 Ohms:
- replace the EGT 1 THERMOCOUPLE (Ref. AMM TASK 49-72-15-000-002) and (Ref. AMM TASK 49-72-15-400-003).
(b) If the resistance is < 20 Ohms:
- do a check of the aircraft wiring from the ECB (59KD) AB/A6,A7 to the EGT 1 THERMOCOUPLE terminals chromel/alumel (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).
B. If the APU GND SCANNING menu gives the maintenance message:
EGT TCPLE RAKE 1
associated with Fault Code Number (FCN) 43
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(161)
