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.
The MCDU shows the MDCU MENU page.
The MCDU shows the CFDS MENU page.
The MCDU shows the SYSTEM REPORT/TEST
page.
The MCDU shows the F/CTL page.
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
5.
Push the line key adjacent to the EFCS1 indication.
6.
Push the line key adjacent to the GROUND SCAN indication.
7.
Push the line key adjacent to the START GROUND SCAN indication.
8.
After two minutes, 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 EFCS1 page.
The MCDU shows the EFCS1 GROUND SCANpage.
Make sure that the MCDU shows no faultindications related to:
-
the two accelerometers 3(12CE3) and 4(12CE4) associated with the ELAC 2.
-
the side stick transducers 1(4CE1), 2(4CE2), 3(4CE3) and 4(4CE4) associated with the ELAC 2 and the three SECs.
-
the servo valves, the solenoid valves, the mode selector valve transducers of the four elevator servo controls (34CE1), (34CE2), (34CE3), (34CE4), associated with the SEC2.
-
the pitch change-over of the SEC1 and SEC2.
The MCDU shows the MCDU MENU page.
1EFF : ALL 1 27-93-00Page 405 1 1 Feb 01/04R 1 1 1CES 1
Subtask 27-93-00-710-052
D. For the ELAC 1 PITCH FAULT warning:
(1) Do this test:
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the overhead panel 23VU:
-release the FLT CTL/SEC 1 pushbuton switch.
2. On the overhead panel 24VU:
-
release the FLT CTL/SEC 2 pushbutton switch
-
release the FLT CTL/ELAC 2 pushbutton switch.
3.
Pressurize the Green and Yellow hydraulic systems (Ref. TASK 29-23-00-863-001) (Ref. TASK 29-24-00-863-001).
4.
On the panel 114VU:
-make sure that the FLAPS control lever is in the 0 position.
5.
On the center pedestal:
-move the THS with the pitch-trim control wheels out of the neutral position.
6.
On the overhead panel 24VU:
-push the FLT CTL/SEC 2
pushbutton switch.
On the overhead panel 23VU:
-
the OFF legend of the FLT CTL/SEC 1pushbutton switch comes on.
On the overhead panel 24VU:
-
the OFF legend of the FLT CTL/SEC 2pushbutton switch comes on.
-
the OFF legend of the FLT CTL/ELAC 2pushbutton switch comes on.
The THS moves out of the neutralposition.
On the overhead panel 24VU:
-the OFF legend of the FLT CTL/SEC 2pushbutton switch goes off.
The THS must return to the neutral position (electric motor 3 in operation).
1EFF : ALL 1 27-93-00Page 406 1 1 Feb 01/04R 1 1 1CES 1
5. Close-up
________ Subtask 27-93-00-860-050
A. Put the aircraft back to its initial configuration.
(1)
For the ELAC 1 FAULT warning :
(a)
Put a warning notice on the FLT CTL/ELAC 1 pushbutton switch, to tell the crew that the ELAC 1 is deactivated.
中國航空網(wǎng) 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(74)
