-
The selected heading index returns to
the center of the heading scale. On the lower ECAM DU, on the F/CTL page:
-
The ailerons and spoilers move back to zero.
-
The rudder and the rudder trim stay
turned to the right and are aligned. On the rudder trim indicator:
-
The trim value is still shown.
The AP1 (AP2) disengages.
The warnings related to AP
disengagement occur momentarily.
On the lower ECAM DU, on the F/CTL
page:
-The rudder and the rudder trim move
back to zero. On the rudder trim indicator:
-L or R 00.0. (plus or minus 0.3.) is shown.
On the FCU:
-
The TRK-FPA indication replaces the
HDG-V/S indication. On the PFDs:
-
The roll and pitch FD bars are replaced by the Flight Path Director and Flight Path Vector symbols.
-
The green V/S indication with cyan value reverts to the green FPA indication with cyan value.
1EFF : ALL 1 22-10-00Page 517 1 1 Feb 01/01 1 1 1CES 1
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
-The green HDG indication reverts to the green TRACK indication.
5. Close-up
________
Subtask 22-10-00-860-055
A. Aircraft Maintenance Configuration
(1)
Depressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-864-001) (Ref. TASK 29-10-00-864-003).
(2)
On the overhead panel, on the ADIRS CDU, set the OFF/NAV/ATT selector switches to OFF.
(3)
Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
(4)
De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
1EFF : ALL 1 22-10-00Page 518 1 1 Feb 01/98 1 1 1CES 1
TASK 22-10-00-710-004
Operational Test of the FCU Lighting WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______
YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
1.
Reason for the Job
__________________
To do a check of the integral lighting and the windows lighting of the FCU.
2.
Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power
3. Job Set-up
__________
Subtask 22-10-00-861-053
A. Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002).
Subtask 22-10-00-865-053
B. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
49VU AUTO FLT/FCU/1 9CA1 B05 121VU AUTO FLT/FCU/2 9CA2 M21 R 122VU LIGHTING/INSTL LT/GLARE/SHLD 5LF Y05
1EFF : ALL 1 22-10-00Page 519 1 1 Feb 01/99 1 1 1CES 1
4. Procedure
_________
Subtask 22-10-00-710-054
A. Do this test:
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the glareshield, below the On the FCU:
FCU:
Set the two linear potentiometers - The indications on the front face are
to their left stop. off.
- The windows lighting is off.
2. Set the left linear potentiometer - All the indications on the front face
to the right stop. get brighter.
3. Set the right linear - The windows lighting increases.
potentiometer to the right stop.
4. Set the two linear potentiometers - Same result as in step 1.
to the left stop.
5. Close-up________
Subtask 22-10-00-862-053
A. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002). 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM AUTO FLIGHT 自动飞行1(41)
