「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
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REFERENCE  DESIGNATION 
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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)