- EGT 1 and/or 2 THERMOCOUPLE
- FUEL FILTER (8028KM)
- FUEL CONTROL UNIT (8022KM)
- FLOW DIVIDER (8024KM)
- damage of the IGV ACTUATOR (8014KM) linkage and the IGV assembly
- APU INLET PRESSURE TRANSDUCER (8048KM)
- APU INLET TEMPERATURE SENSOR (8010KM)
- damage/contamination of electrical connector P19
- aircraft wiring
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific multimeter
No specific ratchet
No specific socket
「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 A201
201-210, Config-1 Aug 01/05 CES B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
49-00-81-810-811
AMM 24-38-00-210-001
AMM 31-36-00-740-006
AMM 31-36-00-740-011
AMM 31-36-00-740-015
AMM 49-00-00-860-008
AMM 49-00-00-970-001
AMM 49-11-11-000-004
AMM 49-11-11-000-804
AMM 49-11-11-400-004
AMM 49-11-11-400-804
AMM 49-23-14-000-001
AMM 49-23-14-400-001
AMM 49-32-11-000-003
AMM 49-32-11-400-003
AMM 49-32-13-000-001
AMM 49-32-13-400-001
AMM 49-32-41-920-001
AMM 49-42-51-000-004
AMM 49-42-51-400-004
AMM 49-51-21-000-001
AMM 49-51-21-400-001
AMM 49-61-34-000-003
AMM 49-61-34-400-003
AMM 49-72-15-000-002
AMM 49-72-15-400-003
AMM 49-91-42-200-004
ASM 49-61/01
49-00-81-991-002
APU AUTO SHUTDOWN - OVERTEMPERATURE (on speed), IGV
Position disagrees with Command (131-9(A))
Visual Inspection of the Batteries (2PB1, 2PB2)
Printout of the APU Hours and Cycles
Printout of Manually Requested Reports
Printout of the Engine / APU Hours and Cycles Stored
in the FDIMU (10TV)
APU Start by External Power (131-9(A))
Access to the Data Memory Module (DMM) Report
(131-9(A))
Removal of the Power Plant (APU) (131-9(A))
Installation of the Power Plant (APU) (131-9(A))
Removal of the Sensor-APU Inlet Temperature (8010KM)
(131-9(A))
Installation of the Sensor-APU Inlet Temperature
(8010KM) (131-9(A))
Removal of the Fuel Control Unit (FCU) (8022KM)
(131-9(A))
Installation of the Fuel Control Unit (FCU) (8022KM)
(131-9(A))
Removal of Flow Divider and Solenoid Valve (8024KM)
(131-9(A))
Installation of Flow Divider and Solenoid Valve
(8024KM) (131-9(A))
Replacement of the Fuel Filter (8028KM) (131-9(A))
Removal of the Starter Motor (131-9(A))
Installation of the Starter Motor (131-9(A))
Removal of the Transducer - APU Inlet Pressure
(8048KM) (131-9(A))
Installation of the Transducer - APU Inlet Pressure
(8048KM) (131-9(A))
Removal of the Electronic Control Box (ECB)
(131-9(A))
Installation of the Electronic Control Box (ECB)
(131-9(A))
Removal of the Thermocouples (8057KM) (131-9(A))
Installation of the Thermocouples (8057KM) (131-9(A))
Inspection of the Magnetic- Drain Plug (8077KM)
(131-9(A))
Fig. 201
「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 A202
201-210, Config-1 Aug 01/05 CES
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 NO LRU FAULT DETECTED or FUEL RESOLVER PRIMARY SHOWS OPEN CIRCUIT or FUEL RESOLVER SECONDARY SHOWS OPEN CIRCUIT or FUEL TORQUE MOTOR SHOWS OPEN CIRCUIT or FUEL TORQUE MOTOR SHOWS SHORT CIRCUIT 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320 Trouble Shooting Manual 排故手册 机载辅助动力 2(72)
