AUTOPILOT/FLIGHT DIRECTOR (AP/FD) - ADJUSTMENT/TEST
___________________________________________________
 TASK 22-10-00-710-001 Operational Test of the Takeover and Priority Pushbutton Switches 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 AP disengagement by the Takeover and Priority
 Pushbutton Switches and related warning.

 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 1.6 m (5 ft. 3 in.)
 B. 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 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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 3. Job Set-up
__________

 Subtask 22-10-00-860-050
 A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002).

 (2)
 Align the ADIRS (two ADIRS are necessary in this test)
 (Ref. TASK 34-10-00-860-004).

 (3)
 On the overhead panel, on the FLT CTL panels 23VU and 24VU:

 -make sure that the ELAC 1 and 2, SEC 1, 2 and 3, and FAC 1 and 2 pushbutton switches are pushed (the FAULT and OFF legends must be off).
 NOTE : The two ELACs, one SEC and one FAC are necessary for this
____
 test.

 (4) Do the EIS start procedure
 (Ref. TASK 31-60-00-860-001).

 Subtask 22-10-00-010-050
 B. Get Access
 (1) Put the access platform in position at the access door 822.
 (a)
 Open the access door 822.

 (b)
 On the battery power center 105VU:

 -loosen the two screws and remove the protective cover.
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 Subtask 22-10-00-865-050

 C. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU AUTO FLT/FCU/1 9CA1 B05 49VU AUTO FLT/FMGC/1 10CA1 B02
R 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 R 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 R
 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 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
 4. Procedure
_________
 Subtask 22-10-00-710-050
 A. Do this test:
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. Make sure that the two FDs are  On the upper section of the Captain's engaged. and First Officer's PFDs:
 -The white 1FD2 indications are in NOTE : If they are not engaged, view.
____
 push the FD pushbutton
 switches on the FCU
 (glareshield: 13VU).

 2. 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.
 3. On the Captain's side stick  The AP1(2) disengages.
 controller: On the FCU:

 -Push then release the Captain's  - The AP1(2) pushbutton switch goes 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.
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 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
- On the glareshield, the red MASTER
　
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