「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 A262
Config-1 Aug 01/05 CES -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 21-51-51-000-001
AMM 21-51-51-400-001
AMM 21-52-24-000-001
AMM 21-52-24-400-001
AMM 31-36-00-740-008
AMM 36-11-00-740-001
AMM 36-12-52-000-001
AMM 36-12-52-400-001
AMM 49-00-00-710-001
AMM 49-00-00-860-003
AMM 49-00-00-860-004
AMM 49-11-11-000-001
AMM 49-11-11-400-001
AMM 49-23-15-000-001
AMM 49-23-15-400-001
AMM 49-23-51-000-002
AMM 49-23-51-400-002
AMM 49-51-13-000-001
AMM 49-51-13-400-001
AMM 49-51-51-000-001
AMM 49-51-51-400-001
AMM 49-51-52-000-002
AMM 49-51-52-400-002
AMM 49-51-52-600-001
AMM 49-61-34-000-001
AMM 49-61-34-400-001
AMM 71-00-00-710-001
ASM 49-61/02
49-00-00-991-001
Removal of the Pack Flow-Control Valve
Installation of the Pack Flow-Control Valve
Removal of the Heat Exchanger Unit 10HM4 (11HM4)
(From the Aircraft)
Installation of the Heat Exchanger Unit 10HM4 (11HM4)
(Into the Aircraft)
Access to the Parameter Call-Up Menus
BITE Test of the BMC 1(2)
Removal of the Crossbleed Valve (6HV)
Installation of the Crossbleed Valve (6HV)
Self-Test of the ECB (59KD) (GTCP 36-300)
APU Start by External Power (GTCP 36-300)
APU Shutdown by External Power (GTCP 36-300)
Removal of the Auxiliary Power Unit (APU) - 4005KM
(GTCP 36-300)
Installation of the Auxiliary Power Unit (APU) -4005KM (GTCP 36-300)
Removal of the Load-Compressor Inlet
Temperature-Sensor (8011KM) ((GTCP 36-300))
Installation of the Load-Compressor Inlet
Temperature-Sensor (8011KM) ((GTCP 36-300))
Removal of the Inlet Guide Vane-Actuator (8014KM)
(GTCP 36-300)
Installation of the Inlet Guide Vane-Actuator
(8014KM) (GTCP 36-300)
Removal of the Pneumatic Sensor Assy (GTCP 36-300)
Installation of the Pneumatic Sensor Assy (GTCP
36-300)
Removal of the Bleed Load Control-Valve (8050KM)
(GTCP 36-300)
Installation of the Bleed Load Control-Valve (8050KM)
(GTCP 36-300)
Removal of the Surge Control Valve (8058KM) (GTCP
36-300)
Installation of the Surge Control Valve (8058KM)
(GTCP 36-300)
Clean Surge Valve Filter (GTCP 36-300)
Removal of the Electronic Control Box (ECB) (59KD)
(GTCP 36-300)
Installation of the Electronic Control Box (ECB)
(59KD) (GTCP 36-300)
Dry Motoring Check
Fig. 202
3. Fault Confirmation
__________________
A. Test
(1) Do the ECB self test (Ref. AMM TASK 49-00-00-710-001).
NOTE : If the self test of the ECB gives a maintenance message, do
____ the related trouble shooting first before you continue with this test.
(2) Get access to the AIDS parameters (ALPHA CALL UP) (Ref. AMM TASK 31-36-00-740-008).
(3) Start and operate the APU (Ref. AMM TASK 49-00-00-860-003).
(4) On overhead panel 35VU, make sure that the APU GEN p/bsw is released (APU GEN off).
(5) Examine and record the indications of the APU system page on the lower ECAM display unit and the AIDS parameters on the MCDU for the subsequent conditions. Record the trend of the EGT during change of APU running state.
NOTE : On the MCDU, you can read these AIDS parameters:
____
- IGV (APU Inlet Guide-Vane position),
- WB (APU Corrected Bleed-Air Flow),
- ADW1 (APU Discrete Word - Information regarding APU operating status), (Ref. Fig. 202/TASK 49-00-00-991-001) 中國航空網(wǎng) 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(jī)載輔助動力 1(59)
