(2)
On the overhead panel 24VU make sure that:
-The FLT CTL/ELAC 2, FLT CTL/SEC 2 and FLT CTL/SEC 3 pushbutton switches are pushed (on these pushbutton switches, the FAULT and OFF legends are off).
(3)
Do this test: .
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
On the center pedestal, on one MCDU, push the MCDU MENU mode key.
2.
Push the line key adjacent to the CFDS indication.
3.
Push the line key adjacent to the SYSTEM REPORT/TEST indication.
4.
Push the line key adjacent to the F/CTL indication.
5.
Push the line key adjacent to the EFCS 1 indication.
6.
Push the line key adjacent to the GROUND SCAN indication.
7.
Push the line key adjacent to the START GROUND SCAN indication and wait two minutes.
8.
Push the line key adjacent to the GROUND SCAN STOP indication.
9.
Push the line key adjacent to the GROUND REPORT indication.
10.
On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.
The MCDU shows the MCDU MENU page.
The MCDU shows the CFDS MENU page.
The MCDU shows the SYSTEM REPORT/TEST
page.
The MCDU shows the F/CTL page.
The MCDU shows the EFCS 1 page.
The MCDU shows the EFCS 1 GROUND SCANpage.
Make sure that the MCDU shows no faultof the transducer units (25CE1,25CE2).
The MCDU shows the MCDU MENU page.
(4) Do the operational test of the rudder hydraulic actuation (Ref. TASK 27-24-00-710-001).
1EFF : ALL 1 27-92-15Page 410 1 1 Feb 01/05R 1 1 1CES 1
5. Close-up
________ Subtask 27-92-15-410-050
A. Close Access
(1)
Remove the warning notice(s).
(2)
Make sure that the work area is clean and clear of tool(s) and other items.
(3)
Close the access door 811.
(4)
Remove the access platform(s).
(5)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
ACCELEROMETER - FLIGHT CONTROL (12CE1,12CE2,12CE3,12CE4) - REMOVAL/INSTALLATION
_______________________________________________________________________________ TASK 27-92-16-000-001 Removal of the Flight Control Accelerometer (12CE1,12CE2,12CE3,12CE4)
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking caps
No specific circuit breaker(s) safety clip(s)
No specific access platform 1.6 m (5 ft. 3 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
**ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
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本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵9(24)
