between 30 ohms and 500 ohms. The insulation must be more than 100
Mohms.
These values are given for information only. You can use these
values to do checks of the component electrical part or of the
wiring before you replace the component. But by this procedure,
the check of the component mechanical part is not done.
For primary winding (power supply):
- if you do the resistance check from the avionics compartment, you must disconnect the transducer of the Right Green Aileron Servo Control.
(1) If the fault continues:
(a) Do a check of the wiring of the POS XDCR signal from the servo control (33CE3) to the first terminal block, (Ref. ASM 27-93/02):
- if there is no continuity, repair the wiring
- if there is continuity, see Para. (b).
(b) Do a check and repair the wiring of the POS XDCR, V11, V12, V21, V22 signal from the servo control (33CE3) to the first terminal block, (Ref. ASM 27-93/02).
B. Do the test given in Para. 3.
「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 ∞∞27-10-00∞∞∞∞∞∞∞∞∞∞Page 208
May 01/05R
CES Loss of the Left Blue Aileron Position Transducer Signal for the ELAC 1
1. Possible Causes
_______________
- ELAC-1 (2CE1)
- wiring of the ANI 2-5, POS SV L AIL signal from the ELAC 1 (2CE1) to the first terminal block
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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)
AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning)
ASM 27-93/02
3. Fault Confirmation
__________________
A. Test
(1) Do the operational test of the side stick assembly (activation for the 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 test gives the maintenance message:
ELAC1 COM OR WIRING FROM L B AIL POS XDCR 33CE3
or
ELAC1 MON OR WIRING FROM L B AIL POS XDCR 33CE3
- 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:
(a) do a check and repair the wiring of the ANI 2-5, POS SV L AIL signal from the ELAC 1 (2CE1) to the first terminal block, COM or MON part as shown in the maintenance message (Ref. ASM 27-93/02).
B. Do the test given in Para. 3. R
「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 ∞∞27-10-00∞∞∞∞∞∞∞∞∞∞Page 209
May 01/05 CES Loss of the Servovalve Signal for the Left Blue Aileron Servo Control
1. Possible Causes
_______________
- ELAC-1 (2CE1)
- servovalve of the servo control (33CE3)
- wiring of the SV signal from the servo control (33CE3) to the ELAC1 (2CE1)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 27-14-51-000-003 Removal of the Aileron Servo-Control Servovalve AMM 27-14-51-400-003 Installation of the Aileron Servo-Control Servovalve 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 27-93/02
3. Fault Confirmation
__________________
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 飛行操縱 1(3)
