R (a) Do a check of the CSU and its wiring to the SFCC, which
R identified the out of detent condition (Ref. TASK 27-51-00-810-R 805).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 301-399, ∞∞27-81-00∞∞∞∞∞∞∞∞∞∞Page 232
May 01/04 CESR NOTE : When one system senses that the flap control lever is out
____ R of detent, but the other system senses a correct R condition, then the fault is usually in the CSU.
R (7) Make a record in the aircraft logbook to monitor the operation of the R slat system during the next flight.
R **ON A/C ALL
B. Procedure
(1) If the ECAM warning SLAT SYS 1 (2) FAULT is shown, but there is no related CFDS message on the PFR, or in the SFCC 1 (2) Slat LLR, do step (2).
(2) Interchange SFCC1 with SFCC 2, (Ref. AMM TASK 27-51-34-000-001) and (Ref. AMM TASK 27-51-34-400-001).
(a) Do a check of the upper ECAM DU for the ECAM Warning SLAT SYS 1(2) FAULT:
- if the fault moves to the opposite system, do step (3)
- if the fault stays in the intial system, do step (4).
(3) Replace the SFCC-1 (21CV) or SFCC-2 (22CV) identified in the ECAM Warning message shown in step (4)(a), (Ref. AMM TASK 27-51-34-000-001) and (Ref. AMM TASK 27-51-34-400-001):
(a) Do a check of the upper ECAM DU for the ECAM Warning SLAT SYS 1
(2) FAULT:
- if the message shows, do step (4)
- if the message does not show, no more maintenance is necessary.
(4) Remove the applicable slat fault relay 90CV or 92CV and use a multimeter to do a check at the base of the holder for a ground on pin Z and 28VDC on pin X:
- if there is a ground on pin Z and 28VDC on pin X, do step (5)
- if there is no ground on pin Z, do step (4)
- if there is no 28VDC on pin X, do step (6)
(5) Replace the applicable slat fault relay:
- for a SLAT SYS 1 FAULT message, replace RELAY-SLAT 1 FAULT (90CV)
- for a SLAT SYS 2 FAULT message, replace RELAY-SLAT 2 FAULT (92CV).
(a) Do a check of the upper ECAM DU for the ECAM Warning SLAT SYS 1
(2) FAULT:
- if the message is shows, do step (4)
- if the message does not show, no more maintenance work is necessary.
「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 ∞∞27-81-00∞∞∞∞∞∞∞∞∞∞Page 233
May 01/04 CES
(6) Do a check and repair as necessary the aircraft wiring between the applicable C/B and connector AA pin 2J of the SFCC mounting tray:
- for relay 90CV, do the check from C/B 5CV and SFCC 1 (Ref. ASM 27-81/02)
- for relay 92CV, do the check from C/B 7CV and SFCC 2 (Ref. ASM 27-81/03).
(a) Do the Operational Test of the Slat System (Ref. AMM TASK 27-84-00-710-001) and make sure that the ECAM Warning SLAT SYS 1(2) FAULT does not show on the upper ECAM DU.
5. Close-up
________
A. Put the aircraft back to its initial configuration.
(1) Do the EIS Stop Procedure, if not done before (Ref. AMM TASK 31-60-00-860-002).
(2) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
「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 ∞∞27-81-00∞∞∞∞∞∞∞∞∞∞Page 234
May 01/04R
CES Slat Menu Not Available On The CFDIU
1. Possible Causes
_______________
- SFCC-1 (21CV)
- SFCC-2 (22CV)
- RELAY-A/C ON GND (94CV)
- RELAY-A/C ON GND (96CV)
- PROX SNSR R L/G EXT 20GA
- PROX SNSR L L/G EXT 21GA
- PROX SNSR R L/G EXT 22GA
- PROX SNSR L L/G EXT 23GA
- aircraft wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 27-51-00-740-002 Bite Test of the Slat and Flap Control Computers
(Flap System)
AMM 27-51-34-000-001 Removal of the SFCC (21CV,22CV)
AMM 27-51-34-400-001 Installation of the SFCC (21CV,22CV)
ASM 27-81/02
ASM 27-81/03
3. Fault Confirmation
__________________
中國航空網 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 2(67)
