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时间:2011-03-20 20:47来源:蓝天飞行翻译 作者:admin
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 WARN lights flash for approximately 3
 seconds.
 - On the upper ECAM DU, the red AP OFF
 indication is shown for approximately
 9 seconds.
 4. On the FCU:  This pushbutton switch comes on.
 - Push the AP1(2) pushbutton  On the upper section of the PFDs:
 switch to engage the AP1(2).  - The white AP1(2) indication comes
 into view.
 5. On the First Officer's side stick  The AP1(2) disengages.
 controller:  On the FCU:
 - Push then release the First  - The AP1(2) pushbutton switch goes
 Officer's takeover and priority  off.
 pushbutton switch.  The warnings related to AP
 disengagement occur as follows:
 - You can hear the cavalry charge
 warning for approximately 1.5
 seconds.
 - On the glareshield, the red MASTER
 WARN lights flash for approximately 3
 seconds.
 - On the upper ECAM DU, the red AP OFF
 indication is shown for approximately
 9 seconds.
 6. Open the circuit breakers  On the overhead panel, on the FLT CTL
 15CE1(15CE2) and 16CE1(16CE2).  panel 23VU:
 - The FAULT legend on the ELAC 1(2)
 pushbutton switch comes on.
 7. On the FCU:  This pushbutton switch comes on.
 - Push the AP1(2) pushbutton  On the upper section of the PFDs:
 switch to engage the AP1(2).  - The white AP1(2) indication comes
 into view.
 8. On the Captain's side stick  The AP1(2) disengages.
 controller:  On the FCU:

 

 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
-Push then release the Captain's takeover and priority pushbutton switch.
9.
 Close the circuit breakers 15CE1(15CE2) and 16CE1(16CE2).

10.
 Do the tests again from step 2 to step 9 with information between parentheses.


 5. Close-up
________
 Subtask 22-10-00-860-051-The AP1(2) pushbutton switch goes
off.The warnings related to AP disengagement occur as follows:
 -You can hear the cavalry charge warning for approximately 1.5 seconds.
 -
On the glareshield, the red MASTER WARN lights flash for approximately 3 seconds.

 -
On the upper ECAM DU, the red AP OFF indication is shown for approximately 9 seconds.


On the overhead panel, on the FLT CTLpanel 23VU:
 -The FAULT legend of the ELAC 1(2) pushbutton switch goes off after some seconds.
You must get the same results (step bystep).
 A. Aircraft Maintenance Configuration
 (1)
 On the overhead panel, on the ADIRS CDU, set the OFF/NAV/ATT selector switches to OFF.

 (2)
 Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).

 (3)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).


 1EFF : ALL 1 22-10-00Page 505 1 1 Feb 01/98 1 1 1CES 1 Subtask 22-10-00-410-050


 B. Close Access
 (1)
 Install the protective cover on the battery power center 105VU.

 (2)
 Tighten the two screws.

 (3)
 Close the access door 822.

 (4)
 Remove the access platform(s).


 1EFF : ALL 1 22-10-00Page 506 1 1 Feb 01/98 1 1 1CES 1 TASK 22-10-00-710-002


 Operational Test of Autopilot Disengagement and Locking Devices of the Side
 Stick Controller and Rudder Pedals
 WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______
 YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.

 1. Reason for the Job
__________________
 Refer to the MPD TASK: 221000-01
 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
R 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
R Power Supply 29-10-00-864-003 Depressurize the Blue Hydraulic System 29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure 34-10-00-860-004 IR Alignment Procedure
 
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