(6)
On the center pedestal, on the ECAM control panel, set the F/CTL page.
(7)
Pressurize the aircraft hydraulic systems
(Ref. TASK 29-23-00-863-001)
(Ref. TASK 29-10-00-863-003).
Subtask 22-10-00-865-052
B. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AUTO FLT/FCU/1 9CA1 B05 49VU AUTO FLT/FMGC/1 10CA1 B02 121VU AUTO FLT/FCU/2 9CA2 M21 121VU AUTO FLT/FMGC/2 10CA2 M17 121VU AUTO FLT/RUDDER/ARTF/FEEL 14CA N17 121VU AUTO FLT/STICK/LOCK 13CA N16
4. Procedure
_________ Subtask 22-10-00-710-053
A. Do this test:
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. Make sure that the two FDs are engaged. On the upper section of the Captain'sand First Officer's PFDs: - The white 1FD2 indications are in
NOTE : If they are not engaged,____ push the FD pushbutton switches on the FCU (glareshield 13VU) view- The cyan ALT indications are in view- The cyan NAV indications are in view.On the FCU: - The dashes are in view in the SPD, HDG and V/S windows - A value is shown in the ALT window
- All the indicator lights are off, except LAT.
2. On the FCU: - Push the AP1 (AP2) pushbutton switch. This pushbutton switch comes on.On the PFDs:- The white AP1 (AP2) indication comes into view.
3. On the FCU: On the PFDs:
- Pull the V/S-FPA selector knob. - The green V/S indication with cyan value (+0) comes into view. - The cyan ALT indication goes out of view
- The pitch FD bar is shown centered. On the FCU, in the V/S window: - The dashes go out of view and are replaced by the zero value.
- Turn the V/S-FPA selector knob to UP. On the FCU:- The vertical speed shown in the V/S window increases positively. On the PFDs:
- The pitch FD bar moves up. - The cyan value increases. On the lower ECAM DU, on the F/CTL
page:
1EFF : ALL 1 22-10-00Page 515 1 1 Feb 01/98 1 1 1CES 1
-------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
-Turn the V/S-FPA knob to DN, to cancel the vertical speed.
-Pull the HDG-TRK selector knob.
-Turn the HDG-TRK selector knob to positively increase the heading value.
-
The elevators move up (nose-up command).
On the FCU:
-
The vertical speed shown goes back to
the zero value. On the PDFs:
-
The pitch FD bar is shown centered.
-
The cyan value goes back to the value
+0. On the lower ECAM DU, on the F/CTL page:
-
The elevators move back to zero.
On the PFDs:
-
The green HDG indication comes into view
-
The cyan NAV indication goes out of view
-
The roll FD bar is shown centered.
-cyan selected heading index comes into view in the center of the heading scale.
On the FCU, in the HDG window:
-
The dashes go out of view and the aircraft heading is shown
-
The LAT indicator light goes off.
On the FCU:
-
The heading shown in the HDG window
increases. On the PFDs:
-
The roll FD bar moves to the right. The selected heading index moves to the right (when the index is out of view, digits replace it on the right of the heading scale).
On the lower ECAM DU, on the F/CTL page:
-
The right aileron and the right spoilers move up
-
The left aileron moves down
-
The rudder moves to right
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-------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
-Turn the heading selector knob to get back to the aircraft heading.
4. On the Captain's or First Officer's side stick controller:
-Push the Captain's AP disconnect and priority pushbutton switch.
5. On the center pedestal, on the panel 110VU:
-Push the RUD TRIM/RESET pushbutton switch.
R R 6. On the FCU:
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本文鏈接地址：A320飛機維護手冊 AMM AUTO FLIGHT 自動飛行1(40)
