(Activation for the BITE Test)
AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning)
ASM 27-93/03
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).
(a) If the ground scanning gives the maintenance message: R B AIL MODE XDCR 33CE4 OR INPUT OF ELAC 2
- refer to the Para. Fault Isolation.
(b) If the ground scanning gives the maintenance messages: R B AIL MODE XDCR 33CE4 OR INPUT OF ELAC 2 L G AIL MODE XDCR 33CE1 OR INPUT OF ELAC 2
- refer to this procedure (Ref. TASK 27-90-00-810-810).
May 01/04R CES
4. Fault Isolation
_______________
A. If the test gives the maintenance message: R B AIL MODE XDCR 33CE4 OR INPUT OF ELAC 2
- replace the ELAC-2 (2CE2), (Ref. AMM TASK 27-93-34-000-001) and (Ref. AMM TASK 27-93-34-400-001).
(1) If the fault continues:
- replace the MODE XDCR of the servo control (33CE4), (Ref. AMM TASK 27-14-51-000-005) and (Ref. AMM TASK 27-14-51-400-005).
NOTE : The resistance of primary (pins A/K and A/L) and secondary
____ (pins A/J and A/U) windings of the transducer must be 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 Left Green Aileron Servo Control.
(2) If the fault continues:
(a) Do a check of the wiring of the MODE XDCR SPLY signal from the servo control (33CE4) to the first terminal block, (Ref. ASM 27-93/03):
- 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 MODE XDCR VS1, VS2 signal from the servo control (33CE4) to the ELAC 2 (2CE2), (Ref. ASM 27-93/03).
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 264
May 01/04R
CES Failure of the Right Blue Aileron Servo Control Servovalve
1. Possible Causes
_______________
- ELAC-2 (2CE2)
- SERVO CTL-R AILERON, OUTBD B (33CE4)
- servovalve of the servo control 33CE4
- wiring POS XDCR signal from the servocontrol (33CE4) to the ELAC 2 (2CE2) COM and MON side
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 27-14-51-000-001 Removal of the Aileron Servo Control AMM 27-14-51-000-003 Removal of the Aileron Servo-Control Servovalve AMM 27-14-51-400-001 Installation of the Aileron Servo Control 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)
AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning)
ASM 27-93/03
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:
R B AIL SERVO VLV 33CE4
- replace the servovalve of the servo control 33CE4, (Ref. AMM TASK 27-14-51-000-003) and (Ref. AMM TASK 27-14-51-400-003).
NOTE : The resistance must be 500 ohms +/- 10 %.
____
「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 265 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 飛行操縱 1(23)
