1. Possible Causes
_______________
- FAC1,2
- DMC 1,2
- FWC 1,2
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 22-60-00-710-004 Windshear Procedure
AMM 22-91-00-710-001 Ground Scanning of the AFS
AMM 31-50-00-710-001 Ground Scanning of the Central Warning System
AMM 31-60-00-740-004 EIS System Test
3. Fault Confirmation
__________________
A. Test
- Do the windshear test procedure (Ref. AMM TASK 22-60-00-710-004).
4. Fault Isolation
_______________
A. If the test not OK with: . WINDSHEAR not present on PFD and no aural warning . or/and WINDSHEAR DET FAULT/WINDSHEAR DET not present on ECAM.
- do the ground scanning of the AFS (FAC1,2) (Ref. AMM TASK 22-91-00-710-001).
(1) If there is one or several CFDS messages R - do the trouble shooting procedure related to the maintenance R message. R
(2) If there is no message:
(a) do the EIS system test (DMC1 for Capt PFD/EWD, DMC2 for the f/O PFD/SD) (DMC 1,2) (Ref. AMM TASK 31-60-00-740-004).
(b) do the ground scanning of the Central Warning system (FWC 1,2) (Ref. AMM TASK 31-50-00-710-001). Refer to the above Para. 4.A.(1).
「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 ∞∞22-66-00∞∞∞∞∞∞∞∞∞∞Page A220
Feb 01/05 CES
B. If the test not OK with: . WINDSHEAR not present on PFD but aural warning present:
- Refer to Para. 4.A.(2)(a) (DMC1 & 2).
. WINDSHEAR present on PFD but no aural warning:
- Refer to Para. 4.A.(2)(b).
C. 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 ∞∞22-66-00∞∞∞∞∞∞∞∞∞∞Page A221
May 01/04R
CES Wrong VLS, F, S or Green Dot displays (PFD)
1. Possible Causes
_______________
- Angle of attack value is different on the three ADIRUs
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
34-11-00-810-861 Different Angle of Attack Value on the three ADIRUs
3. Fault Confirmation
__________________
A. Test
(1) Not applicable.
4. Fault Isolation
_______________
A. If, on the PFD, the indications VLS, F, S or Green Dot are incorrect:
- if the Angle of attack value is different on the three ADIRUs, do the trouble shooting procedure (Ref. TASK 34-11-00-810-861).
「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 ∞∞22-66-00∞∞∞∞∞∞∞∞∞∞Page A222
May 01/04R
CES Loss of FAC 1 after 28VDC FAC 1 circuit breaker tripping
1. Possible Causes
_______________
- ACTUATOR-RUDDER TRIM (10CC)
- LIMITATION UNIT-RUDDER TRAVEL (4CC)
- FAC-1 (1CC1)
- SERVO ACTR-YAW DAMPER, 1 (3CC1)
- 28VDC FAC1 Power Supply wiring
- RTL SYS 1 - RELAY (13CC1)
- RUD TRIM 1 - RELAY (7CC1)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
22-63-00-810-801 Loss of the Yaw Damper Function on the FAC 1
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 27-22-51-000-001 Removal of the Rudder Trim Actuator (10CC)
AMM 27-22-51-400-001 Installation of the Rudder Trim Actuator (10CC)
AMM 27-23-51-000-001 Removal of the Rudder Travel Limitation Unit 4CC
R AMM 27-23-51-400-001 Installation of the Rudder Travel-Limitation Unit 4CC ASM 22-67/01 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 AUTO FLIGHT 自動飛行2(40)
