A. Aircraft Maintenance Configuration
(1)
Make sure that the access platform is in position at the access door 824 in zone 128.
(2)
Make sure that the access door 824 is open.
Subtask 27-95-34-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 3CE1
49VU FLIGHT CONTROLS/FCDC1/SPLY 20CE1 B10 FOR 3CE2 121VU FLIGHT CONTROLS/FCDC2/SPLY 20CE2 Q20
4. Procedure
_________
(Ref. Fig. 401/TASK 27-95-34-991-001)
Subtask 27-95-34-420-050
A. Installation of the FCDC
(1)
Remove the blanking caps from the electrical connectors (2).
(2)
Install the FCDC (1) on its rack (3).
(3)
Push the FCDC (1) on its rack (3) to connect electrical connectors (2).
(4)
Engage the nuts (4) on the lugs and tighten.
R CAUTION : MAKE SURE THAT THE OBRM(S) IS (ARE) CORRECTLY INSTALLED. IF
_______ R IT (THEY) IS(ARE) NOT INSTALLED CORRECTLY, PUSH THE OBRM(S) UNTIL THE LOCKING DEVICES ARE LOCKED.
Subtask 27-95-34-865-052
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): FOR 3CE1 20CE1 FOR 3CE2 20CE2
Subtask 27-95-34-710-050
C. Do the operational test of the FCDC (3CE1,3CE2) (Ref. TASK 27-96-00-710-001).
5. Close-up
________
Subtask 27-95-34-410-050
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other items.
R (2) Close the access door 824 (Ref. TASK 52-41-00-410-002).
(3)
Remove the access platform(s).
(1)
CFDS menu (Ref. Fig. 002)
(a) LAST LEG REPORT (Ref. Fig. 003) This function displays all the system failures which appeared during the last flight. The messages include:
-
the failed LRU with ATA reference number,
-
the time of occurrence,
-
the date
(b) PREVIOUS LEGS REPORT (Ref. Fig. 004) The messages related to failures which appeared during the previous 64 flights include:
-
the failed LRU with ATA reference number,
-
the time and date of occurrence,
-
the flight number.
(c) SYSTEM REPORT/TEST This is the access to various systems and particularly F/CTL (Ref. Fig. 005)
(2)
F/CTL menu This menu is mainly provided for main-base maintenance of flight controls. The 4 sub-menus below are displayed: (Ref. Fig. 005)
-
EFCS 1
-
EFCS 2
-
SFCC 1
-
SFCC 2
The EFCS maintenance messages are processed in the EFCS 1 or 2
sub-menus.
These two sub-menus have the same constitution:
(Ref. Fig. 006)
-LAST LEG REPORT
-PREVIOUS LEGS REPORT
-LRU IDENTIFICATION
-GROUND SCAN
-CLASS 3 FAULTS
-TEST
-MEMORY
(a) LAST LEG REPORT (7) (Ref. Fig. 007) Only the failures of the last flight, affecting flight controls are displayed. These messages include:
-
the date,
-
the aircraft identification,
-
the flight number,
-
the time,
-
the failed LRU with its ATA reference.
(b)
PREVIOUS LEGS REPORT (7) (Ref. Fig. 007) Only the failures of the last 64 flights, affecting flight controls are displayed. The display is identical with that of CFDS menu (Ref. Para. (1) (b)).
(c)
LRU IDENTIFICATION This page indicates the part numbers of the flight control computers (Ref. Fig. 008)
(d)
GROUND SCAN (Ref. Fig. 009) This function is used on the ground to display the failures which are present at the time of the request. Thus this function can confirm a troubleshooting.
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱9(111)
