(2) Do this test:
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the center pedestal on the panel 114VU:
R R R R R R R R - move the slat and flap control lever to the position 1 and then to the position 2. Stop at each notch until the slats are in their new position.
2. On the panel 114VU:
R R - move the slat and flap control lever to the position 3.
R R R
3. On the panel 114VU:
R R - move the slat and flap control lever to the position FULL.
R R R R R
4. On the panel 114VU:
R R - move the slat and flap control lever back to the position 3.
R R
-
the slats move to the set position.
On the ECAM upper DU:
-
the slat position bar moves to the set position
-
the new position of the lever and the travel direction of the slats are shown.
-
the slats do not move.
On the ECAM upper DU:
-
the slat position bar does not move
-
the new position of the lever is shown as above.
-
the slats move to the set position.
On the ECAM upper DU:
-
the slat position bar moves to the set position
-
the new position of the lever and the travel direction of the slats are shown.
-
the slats move to the set position.
On the ECAM upper DU:
-
the slat position bar moves to the set position
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
R R R R R
5. On the panel 114VU:
R R - move the slat and flap control lever back to the position 2.
R R R
6. On the panel 114VU:
R R R R R R R R R R - move the slat and flap control lever back to the positions 1 and 0. Stop at each notch until the slats are in their new position.
5. Close-Up________
Subtask 27-84-00-860-053
-the new position of the lever and the travel direction of the slats are shown
-no warnings related to the slat system are shown.
-
the slats do not move.
On the ECAM upper DU:
-
the slat position bar does not move
-
the new position of the lever is shown.
-
the slats move to the set position.
On the ECAM upper DU:
-
the slat position bar moves to the set position
-
the new position of the lever and the travel direction of the slats are shown
-no warnings related to the slat system are shown.
A. Aircraft Maintenance Configuration
(1)
Depressurize the Blue hydraulic system
(Ref. TASK 29-10-00-864-003).
(2)
On the ECAM control panel, set the control/brightness controls to OFF.
(3)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
Subtask 27-84-00-865-051
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV, 14CC1, 14CC2.
Subtask 27-84-00-942-050
C. Removal of Equipment
(1)
Remove the safety barriers.
(2)
Remove the warning notice(s).
(3)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
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本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM FLIGHT CONTROLS 飛行操縱7(92)
