「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 : 301-399, ∞∞27-92-00∞∞∞∞∞∞∞∞∞∞Page 231
May 01/04 CES Failure of the Pedal Force Transducer Unit (74CE)
1. Possible Causes
_______________
- FTU-RUDDER PEDAL (74CE) R - C/B - RUDDER FTU (75CE)
- wiring of the +28VDC signal from the pedal force transducer unit to the circuit breaker
- wiring of the GND signal from the pedal force transducer unit to the ground
- ground wiring of the pedal force transducer unit
- wiring of the DGI 10 signal from the pedal force transducer unit to the first terminal block
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
31-32-00-810-934
R IPC 27920801 AMM 27-92-27-000-001 AMM 27-92-27-400-001
AMM 27-96-00-740-001 R ASM 27-92/00
3. Fault Confirmation
__________________
A. Test
Failure of the Digital Links
Removal of the Rudder Pedal Force Transducer (74CE)
Installation of the Rudder Pedal Force Transducer
(74CE)
BITE Test of the EFCS (Ground Scanning)
(1) Do the BITE test of the EFCS (ground scanning) (Ref. AMM TASK 27-96-00-740-001).
4. Fault Isolation
_______________
A. If the test confirm the fault:
- replace the FTU-RUDDER PEDAL (74CE) (Ref. AMM TASK 27-92-27-000-001) and (Ref. AMM TASK 27-92-27-400-001).
(1) If the fault continues: R - do the trouble shooting procedure (Ref. TASK 31-32-00-810-934) R related to the DGI 10 signal.
(2) If the fault continues: R - replace the C/B - RUDDER FTU (75CE) (Ref. IPC 27920801).
「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 : 301-399, ∞∞27-92-00∞∞∞∞∞∞∞∞∞∞Page 232
Aug 01/04 CES
(3) If the fault continues:
R - do a check of the wiring of the +28VDC signal from the pedal force
R transducer unit to the circuit breaker (Ref. ASM 27-92/00).
R - do a check of the wiring of the GND signal from the pedal force
R transducer unit to the ground (Ref. ASM 27-92/00).
R - do a check of the ground wiring of the pedal force transducer unit
R (Ref. ASM 27-92/00).
R - do a check and repair the wiring of the DGI 10 signal from the
R pedal force transducer unit to the first terminal block (Ref. ASM
R 27-92/00).
B. Do the test given in para. 3.
ELAC SYSTEM (ELEVATOR AILERON COMPUTER) - FAULT ISOLATION PROCEDURES
____________________________________________________________________
TASK 27-93-00-810-801
Loss of the Roll Signal on the CAPT Side Stick for the ELAC 1
1. Possible Causes
_______________
- ELAC-1 (2CE1)
- SSTU-ROLL CTL, CAPT (4CE1)
- wiring from the ELAC 1 (2CE1) to the SSTU (4CE1)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 27-92-41-000-002 Removal of the Transducer Units (4CE1,4CE2,4CE3,4CE4) AMM 27-92-41-400-002 Installation of the Transducer Units
(4CE1,4CE2,4CE3,4CE4)
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 27-96-00-710-020 Operational Test of the Side Stick Assembly
(Activation for the BITE Test) R AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning) ASM 27-92/12
3. Fault Confirmation
__________________
A. Test
(1) Do the operational test of the side stick assembly (activation for BITE test) (Ref. AMM TASK 27-96-00-710-020).
(2) Do the BITE test of the EFCS (Ground Scanning) (Ref. AMM TASK 27-96-00-740-001).
4. Fault Isolation
_______________
A. If the BITE test gives the maintenance message:
ELAC1 OR INPUT OF CAPT ROLL CTL SSTU 4CE1
- replace the ELAC-1 (2CE1), (Ref. AMM TASK 27-93-34-000-001) and (Ref. AMM TASK 27-93-34-400-001).
(1) If the fault continues: 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 飞行操纵 2(119)
