A320飞机维护手册 AMM NAVIGATION 导航1(162)

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4. On the ADIRS CDU:  On the ADIRS CDU:
 - push the ADR1 and ADR2 pushbutton switches.  - the OFF legend of the ADR1 pushbuttonswitch comes on - the OFF legend of the ADR2 pushbutton switch goes off.
 5. Do the ADR2 test as specified in step 3. Same results on the F/O side.
 6. On the ADIRS CDU:  On the ADIRS CDU:
 - push the ADR2 and ADR3 pushbutton switches.  - the OFF legend of the ADR2 pushbuttonswitch comes on - the OFF legend of the ADR3 pushbutton switch goes off.
 7. On the SWITCHING panel 8VU: - set the AIR DATA selector switch to CAPT/3.  On the CAPT PFD, the speed and altitudeindications from the ADR3 come intoview.
 8. Do the ADR3 test as specified in the step 3. Same results on the CAPT side.
 9. On the ADIRS CDU:
R  - push the ADR1 and ADR2 pushbutton switches again  On the ADIRS CDU, the OFF legend of theADR1 and ADR2 pushbutton switches goes off.
 5. Close-up________
 Subtask 34-13-00-410-060
 A. 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).

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 Subtask 34-13-00-865-083
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CC1, 5CC2, 7XE
 **ON A/C ALL
 Subtask 34-13-00-860-051
 C. Put the aircraft back to its initial configuration.
 (1)
 Do the EIS STOP procedure (Ref. TASK 31-60-00-860-002).

 (2)
 Do the ADIRS stop procedure (Ref. TASK 34-10-00-860-005).

 (3)
 On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.

 (4)
 De-energize the aircraft electrical circuit
 (Ref. TASK 24-41-00-862-002).

 (5)
 Close the nose landing gear doors (Ref. TASK 32-22-00-410-001).

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 TASK 34-13-00-720-009
 Functional Test of the Altitude and Airspeed Data
 CAUTION : OBEY THESE PRECAUTIONS WHEN YOU DO THE TEST TO PREVENT DAMAGE TO
_______
 INSTRUMENTS:

 -PRESSURE SET MUST NOT BE MORE THAN 1050 hPa (31 in Hg) OR LESS THAN 115 hPa (3.39 in Hg)
 -CHANGES IN PRESSURE MUST NOT BE MORE THAN 6000 FEET/MINUTE
 -DO NOT SUDDENLY OPEN LINES TO AMBIENT AIR WHILE THE PRESSURE GENERATOR IS CONNECTED.
 CAUTION : THE TOTAL PRESSURE IN THE PITOT SYSTEM MUST NEVER BE LESS THAN THE
_______ STATIC PRESSURE. THE DIFFERENCE BETWEEN THE PITOT AND THE STATIC PRESSURE CIRCUITS MUST NEVER BE MORE THAN 368 hPa (10.86 in Hg).
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
 No specific colored adhesive tape R No specific 1 GENERATOR - GROUND PRESSURE MINI. 100 MB (1.45 PSI) R TO 1400 MB (20.3 PSI)
 36122 1 ADAPTOR-CHARGING,PITOT PROBE R 98D34003500000 1 ADAPTER COVER-STATIC PORT
 1EFF : 001-049, 051-099, 101-105, 151-158, 1 34-13-00Page 544 1201-209, 1Aug 01/05 1 1 1CES 1

 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 27-50-00-866-009 Retraction of the Flaps on the Ground 31-60-00-860-001 EIS Start Procedure 34-10-00-860-002 ADIRS Start Procedure 34-10-00-860-005 ADIRS Stop Procedure 34-11-15-200-001 Inspection/Check of the Pitot Probe (9DA1,9DA2,9DA3)
 3. Job Set-up
__________
 Subtask 34-13-00-860-054
 A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002).

 (2)
 Do the EIS start procedure (PFD DUs only) (Ref. TASK 31-60-00-860-001).

 (3)
 Do the ADIRS start procedure (Ref. TASK 34-10-00-860-002).
　
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