R **ON A/C 001-003, 051-099, 401-499,
B. Do the test given in para. 3.
TASK 49-00-00-810-817
APU AUTO SHUT DOWN - OVERTEMPERATURE, during APU Operation (GTCP 36-300)
1. Possible Causes
_______________
- damage and/or unwanted material in the air intake system and/or on the engine air-intake screen
- damage and/or unwanted material in the exhaust system and/or on the turbine exducer blades and stators
- INLET GUIDE-VANE ACTUATOR P21
- FLOW DIVIDER AND DRAIN VALVE ASSY
- ECB (59KD)
- PRIMARY FUEL NOZZLE AND MANIFOLD
- SECONDARY FUEL NOZZLE AND MANIFOLD
- AUXILIARY POWER UNIT (4005KM)
- INLET GUIDE-VANE ACTUATOR (8014KM)
- FUEL CONTROL UNIT (8022KM)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 49-00-00-710-004 Operational Test of the APU (4005KM) (GTCP 36-300) AMM 49-11-11-000-001 Removal of the Auxiliary Power Unit (APU) - 4005KM (GTCP 36-300) AMM 49-11-11-400-001 Installation of the Auxiliary Power Unit (APU) -4005KM (GTCP 36-300) AMM 49-16-00-210-001 Detailed Inspection of the Air Intake, Diffuser
Elbow, Seals and Felt Metal (GTCP 36-300) AMM 49-20-00-200-001 Inspection/Check of the Engine (4005KM) (GTCP 36-300) AMM 49-23-51-000-002 Removal of the Inlet Guide Vane-Actuator (8014KM)
(GTCP 36-300)
AMM 49-23-51-400-002 Installation of the Inlet Guide Vane-Actuator
(8014KM) (GTCP 36-300)
AMM 49-31-41-000-001 Removal of the Primary Fuel Nozzle and Manifold
(8020KM) (GTCP 36-300)
AMM 49-31-41-400-001 Installation of the Primary Fuel Nozzle and Manifold
(8020KM) (GTCP 36-300)
AMM 49-31-42-000-002 Removal of the Secondary Fuel Nozzle and Manifold
(8021KM) (GTCP 36-300)
AMM 49-31-42-400-004 Installation of the Secondary Fuel Nozzle and Manifold (8021KM) (GTCP 36-300) AMM 49-32-11-000-001 Removal of the Fuel Control Unit (FCU) (8022KM) (GTCP 36-300) AMM 49-32-11-400-001 Installation of the Fuel Control Unit (FCU) (8022KM) (GTCP 36-300)
-------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 49-32-12-000-001 Removal of the Flow Divider and Drain Valve Assembly (8023KM) (GTCP 36-300) AMM 49-32-12-400-001 Installation of the Flow Divider and Drain Valve Assembly (8023KM) (GTCP 36-300) AMM 49-61-34-000-001 Removal of the Electronic Control Box (ECB) (59KD) (GTCP 36-300) AMM 49-61-34-400-001 Installation of the Electronic Control Box (ECB) (59KD) (GTCP 36-300)
3. Fault Confirmation
__________________
A. Check/Test
(1) Before you start the APU for the operational test:
- do a visual inspection and make sure that you do not find damage and/or unwanted material in the air intake system and/or on the engine air-intake screen (Ref. AMM TASK 49-16-00-210-001).
- do a visual inspection and make sure that you do not find damage and/or unwanted material in the exhaust system and/or on the turbine exducer blades and stators (Ref. AMM TASK 49-20-00-200-001)
NOTE : THE TORQUE LIMIT IS 29 lbf.ft (3.9318 m.daN). DO NOT TURN THE
____ SHAFT WITH A TORQUE MORE THAN THE LIMIT. A TORQUE MORE THAN THE LIMIT WILL DAMAGE THE COMPONENT.
- turn the manual drive shaft of the starter motor (8KA) in a counterclockwise direction (in the direction of the arrow on the housing) and make sure that: . you can turn the manual drive shaft of the starter motor equally, . the APU rotors, bearings and gears do not rub, . the APU rotors, bearings and gears do not make unsual noise.
NOTE : Turn the manual drive shaft of the starter motor with a torque
____ wrench. Make sure that the drag is 15 to 45 lbf.in (0.17 to 0.51 m.daN).
(a) If you find that the drag of the APU rotors, bearings and gears is too much, they do rub or they make unsual noise, replace the AUXILIARY POWER UNIT (4005KM) (Ref. AMM TASK 49-11-11-000-001) and (Ref. AMM TASK 49-11-11-400-001).
(2) Do the operational test of the APU (Ref. AMM TASK 49-00-00-710-004).
「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 : 001-003, 051-099, 401-499, ∞∞49-00-00∞∞∞∞∞∞∞∞∞∞Page 247
Config-1 Aug 01/05 CES 4. Fault Isolation
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 1(16)
