「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 B252
201-210, Config-1 Aug 01/05 CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R 49-00-81-810-861 Load-Control Valve (P12) Fault (131-9(A))
R 49-00-81-810-871 Surge Control Valve (P18) Fault (131-9(A))
R 49-20-00-810-803 APU Inlet-Temperature (T2) Sensor Fault (131-9(A))
R AMM 21-51-51-000-001 Removal of the Pack Flow-Control Valve
R AMM 21-51-51-400-001 Installation of the Pack Flow-Control Valve
R AMM 21-52-24-000-001 Removal of the Heat Exchanger Unit 10HM4 (11HM4)
R (From the Aircraft)
R AMM 21-52-24-400-001 Installation of the Heat Exchanger Unit 10HM4 (11HM4)
R (Into the Aircraft)
R AMM 31-36-00-740-008 Access to the Parameter Call-Up Menus
R AMM 36-11-00-740-001 BITE Test of the BMC 1(2)
R AMM 36-12-51-000-001 Removal of the Check Valve
R AMM 36-12-51-200-001 Remove and Check Auxiliary Power Unit Bleed
R Check-Valve (7260HM) for Condition
R AMM 36-12-51-400-001 Installation of the Check Valve
R AMM 49-00-00-710-009 Self-Test of the ECB (131-9(A))
R AMM 49-00-00-860-008 APU Start by External Power (131-9(A))
R AMM 49-00-00-860-009 APU Shutdown by External Power (131-9(A))
R AMM 49-11-11-000-004 Removal of the Power Plant (APU) (131-9(A))
R AMM 49-11-11-400-004 Installation of the Power Plant (APU) (131-9(A))
R AMM 49-23-14-000-001 Removal of the Sensor-APU Inlet Temperature (8010KM)
R (131-9(A))
R AMM 49-23-14-400-001 Installation of the Sensor-APU Inlet Temperature
R (8010KM) (131-9(A))
R AMM 49-23-51-000-004 Removal of the Inlet Guide Vane - Actuator (8014KM)
R (131-9(A))
R AMM 49-23-51-400-004 Installation of the Inlet Guide Vane - Actuator
R (8014KM) (131-9(A))
R AMM 49-51-16-000-002 Removal of the Transducer - Differential Pressure
R (8043KM) (131-9(A))
R AMM 49-51-16-400-002 Installation of the Transducer - Differential
R Pressure (8043KM) (131-9(A))
R AMM 49-51-17-000-002 Removal of the Transducer - Total Pressure (8044KM)
R (131-9(A))
R AMM 49-51-17-400-002 Installation of the Transducer - Total Pressure
R (8044KM) (131-9(A))
R AMM 49-51-51-000-004 Removal of the Load Control Valve (8050KM) (131-9(A))
R AMM 49-51-51-400-004 Installation of the Load Control Valve (8050KM)
R (131-9(A))
R AMM 49-51-52-000-003 Removal of the Surge Control Valve (8058KM)
R (131-9(A))
R AMM 49-51-52-400-003 Installation of the Surge Control Valve (8058KM)
R (131-9(A))
R AMM 49-61-34-000-001 Removal of the Electronic Control Box (ECB) (59KD)
R (GTCP 36-300)
R AMM 49-61-34-000-003 Removal of the Electronic Control Box (ECB)
R (131-9(A))
「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 B253 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(130)