1. Possible Causes
_______________
- FAC-1 (1CC1)
- wiring of the HYD CIRC PRESS SW discrete (from the FAC 1 (1CC1) to the first terminal block)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
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 22-91-00-710-001 Ground Scanning of the AFS
AMM 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
Power Supply AMM 29-10-00-864-003 Depressurize the Blue Hydraulic System AMM 29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow
Hydraulic System through the PTU with the Electric Pump AMM 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU AMM 29-24-00-863-001 Pressurize the Yellow Hydraulic System with the
Electric Pump
AMM 29-24-00-864-001 Depressurize the Yellow Hydraulic System
ASM 22-68/04
3. Fault Confirmation
__________________
A. Job Set-up
(1) Aircraft Maintenance Configuration
(a) Pressurize the aircraft hydraulic systems (Ref. AMM TASK 29-10-00-863-003) (Ref. AMM TASK 29-23-00-863-001) (Ref. AMM TASK 29-24-00-863-001) .
B. Test
(1) Do the Ground Scanning of the AFS (Ref. AMM TASK 22-91-00-710-001).
「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 223
Feb 01/03R CES
4. Fault Isolation
_______________
A. If the test gives the maintenance message AFS : HYD G 1151GN:
- on the MCDU, get the AFS/TEST REPORT TROUBLE SHOOTING DATA page.
- make sure that the fourth number of the word W3 is equal to one of these values: . 8, 9, A, B, C, D, E or F.
(1) If the fourth number is not equal to one of the above values:
- replace the FAC-1 (1CC1) (Ref. AMM TASK 22-66-34-000-002) and (Ref. AMM TASK 22-66-34-400-002).
(a) If the fault continues:
- do a check and repair the wiring of the HYD CIRC PRESS SW discrete (from the FAC 1 (1CC1) to the first terminal block) (Ref. ASM 22-68/04).
B. Do the test given in Para. 3.
5. Close-up
________
A. Put the aircraft back to its initial configuration.
(1) Depressurize the aircraft hydraulic systems (Ref. AMM TASK 29-10-00-864-003) (Ref. AMM TASK 29-23-00-864-001) (Ref. AMM TASK 29-24-00-864-001).
「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 224
Feb 01/03R
CES Loss of the Reception of the HYD CIRC PRESS SW Discrete by the FAC 2
1. Possible Causes
_______________
- FAC-2 (1CC2)
- wiring of the HYD CIRC PRESS SW discrete (from the FAC 2 (1CC2) to the first terminal block)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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 22-91-00-710-001 Ground Scanning of the AFS
AMM 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
Power Supply AMM 29-10-00-864-003 Depressurize the Blue Hydraulic System AMM 29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow
Hydraulic System through the PTU with the Electric Pump AMM 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU AMM 29-24-00-863-001 Pressurize the Yellow Hydraulic System with the
Electric Pump
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 AUTO FLIGHT 自動飛行1(113)
