AMM 27-92-17-400-001 Installation of the Flight Control Pressure Switch (10CE2) AMM 27-92-17-400-002 Installation of the Flight Control Pressure Switch (10CE3) AMM 27-92-17-400-003 Installation of the Flight Control Pressure Switch
(10CE1) AMM 27-93-34-000-001 Removal of the ELAC (2CE1,2CE2) AMM 27-93-34-400-001 Installation of the ELAC (2CE1,2CE2) AMM 27-94-34-000-001 Removal of the SEC (1CE1,1CE2,1CE3) AMM 27-94-34-400-001 Installation of the SEC (1CE1,1CE2,1CE3) AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning) AMM 29-10-00-864-001 Depressurize the Green Hydraulic System AMM 29-10-00-864-002 Depressurize the Yellow Hydraulic System AMM 29-10-00-864-003 Depressurize the Blue Hydraulic System AMM 29-32-12-000-001 Removal of the System Pressure Switch (1151GN) AMM 29-32-12-000-002 Removal of the System Pressure Switch (2151GN) AMM 29-32-12-000-003 Removal of the System Pressure Switch (3151GN) AMM 29-32-12-400-001 Installation of the System Pressure Switch (1151GN) AMM 29-32-12-400-002 Installation of the System Pressure Switch (2151GN) AMM 29-32-12-400-003 Installation of the System Pressure Switch (3151GN) ASM 24-38/02 ASM 27-92/01 ASM 27-92/02 ASM 27-92/27 TSM 27 PB 101
3. Fault Confirmation
__________________
A. In the cockpit, on the overhead ELEC panel 35VU, do a check of the battery voltage on the BAT2 voltmeter.
4. Fault Isolation
_______________
A. Table of the circuit breakers used in this procedure:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU ADIRS/ADIRU1/28VDC 6FP1 C02 105VU ELEC/HOT BUS/702PP SPLY 5PB2 D02 105VU ELEC/HOT BUS/702PP SPLY 12PB2 E02
R 105VU ELEC/BAT REF/BCL2 9PB2 F02 105VU ELEC/STAT INV/CNTOR/CTL 14XB G02 R 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞24-38-00∞∞∞∞∞∞∞∞∞∞Page 260
May 01/03 CES
R B. If the voltage is less than 25.5 V, do a check to find if the problem
R comes from the Spoiler Elevator Computers (SEC).
R (1) Make sure that the three hydraulic systems are not pressurized (Ref.
R AMM TASK 29-10-00-864-001), (Ref. AMM TASK 29-10-00-864-002) and
R (Ref. AMM TASK 29-10-00-864-003).
R (2) Make sure that the ELAC 1 (2CE1), ELAC 2 (2CE2), SEC 1 (1CE1), SEC 2
R (1CE2) and SEC 3 (1CE3) are correctly racked and powered.
R (3) Open the circuit breaker ELAC 2 NORM SPLY (15CE2).
R (4) After 30 seconds, on the FLT control panel 24VU, do a check of the
R FAULT legend of the FLT CTL/ELAC 2 pushbutton switch (6CE2).
R (a) If the FAULT legend is off:
R - remove the SEC 1 (1CE1)
R - after 30 seconds, on the FLT control panel 24VU, do a check of
R the FAULT legend of the FLT CTL/ELAC 2 pushbutton switch.
R 1_ If the FAULT legend comes on:
R - replace the SEC-1 (1CE1) (Ref. AMM TASK 27-94-34-000-001)
R and (Ref. AMM TASK 27-94-34-400-001).
R 2_ If the FAULT legend is off:
R - remove the SEC 2 (1CE2)
R - after 30 seconds, on the FLT control panel 24VU, do a check
R of the FAULT legend of the FLT CTL/ELAC 2 pushbutton switch.
R a_ If the FAULT legend comes on:
R - replace the SEC-2 (1CE2) (Ref. AMM TASK 27-94-34-000-001)
R and (Ref. AMM TASK 27-94-34-400-001)
R b_ If the FAULT legend is off:
R - remove the SEC 3 (1CE3)
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 电源 3(71)
