WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES
_______ ARE CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
「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 ∞∞22-63-00∞∞∞∞∞∞∞∞∞∞Page 213
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A. Job Set-Up
(1) Aircraft Maintenance Configuration
(a) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(b) Pressurize the aircraft hydraulic systems (Ref. AMM TASK 29-23-00-863-001) (Ref. AMM TASK 29-24-00-863-001) (Ref. AMM TASK 29-10-00-863-003).
B. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
49VU AUTO FLT/FAC1/28VDC 5CC1 B04
C. Test
(1) Open the circuit breaker 5CC1.
(2) After a minimum of 10 seconds, close the circuit breaker 5CC1.
(3) After 2 minutes, do the operational test of the AFS (Ref. AMM TASK 22-96-00-710-001) and read the result for the FAC 1.
4. Fault Isolation
_______________
A. If the test gives the maintenance message AFS : FAC1/YD RVDT BOX 2CC:
- replace the FAC-1 (1CC1), (Ref. AMM TASK 22-66-34-000-002) and (Ref. AMM TASK 22-66-34-400-002).
(1) If the fault continues:
- do a check of the wiring of the 26VAC signal at RVDT box (2CC) from pin A/A to the first terminal block (Ref. ASM 22-68/04).
(a) If there is no continuity:
- repair the above wiring.
(b) If there is continuity:
- do a check of the wiring of the ground signal at RVDT box (2CC) pin A/B (Ref. ASM 22-68/04).
1 If there is no continuity:
_
- repair the above wiring.
2 If there is continuity:
_
- replace the XDCR UNIT-YAW DAMPER POS (2CC), (Ref. AMM TASK 27-26-17-000-001) and (Ref. AMM TASK 27-26-17-400-001).
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Feb 01/03R CES
(2) If the fault continues:
- do a check and repair the wirings of the YAW V1 MON and YAW V2 MON discretes (from the RVDT box (2CC) to the FAC 1 (1CC1) (Ref. ASM 22-68/04).
B. Do the operational test of the yaw damper function (Ref. AMM TASK 22-63-00-710-001).
「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 ∞∞22-63-00∞∞∞∞∞∞∞∞∞∞Page 215
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CES Loss of the Signal from the Yaw-Damper Position Transducer-Unit (2CC) to the FAC 2
1. Possible Causes
_______________
- FAC-2 (1CC2)
- XDCR UNIT-YAW DAMPER POS (2CC)
- wiring of the 26VAC signal at RVDT box (2CC)
- wiring of the ground signal at RVDT box (2CC)
- wirings of the YAW V1 MON and YAW V2 MON discretes (from the RVDT box (2CC) to the FAC 2 (1CC2)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 22-63-00-710-001 Operational Test of the Yaw Damper Function AMM 22-66-34-000-002 Removal of the FAC (1CC1,1CC2) AMM 22-66-34-400-002 Installation of the FAC (1CC1,1CC2) AMM 22-96-00-710-001 Operational Test of the AFS AMM 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
External Power AMM 27-26-17-000-001 Removal of the Yaw Damper Position Transducer Unit 2CC AMM 27-26-17-400-001 Installation of the Yaw Damper Position Transducer Unit 2CC AMM 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground Power Supply
AMM 29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump
AMM 29-24-00-863-001 Pressurize the Yellow Hydraulic System with the
Electric Pump
ASM 22-68/04
3. Fault Confirmation
__________________
WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______
YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES 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 AUTO FLIGHT 自动飞行1(110)
