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时间:2011-03-26 00:13来源:蓝天飞行翻译 作者:admin
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 - on the upper ECAM display unit, this indication is shown: OVERSPEED VMO/MMO 350/.82
The test procedure stops:
- on the upper ECAM display unit, the OVERSPEED warning indication goes out of view,
 - on the CAPT (F/O) PFD, the speed and altitude indications go back to their initial value,
 - on the lower ECAM display unit, the TAT and SAT values show the local temperature (only with ADR1 and/or ADR3 is set).
On the ADIRS CDU, the OFF legend of theADR2 pushbutton switch goes off
Same results on the F/O side.
- on the lower ECAM display unit, the TAT and SAT values are not shown (only with ADR1 and/or ADR3 is set).
On the ADIRS CDU, the OFF legend of the ADR3 pushbutton switch goes off
R 1EFF : 106-149, 303-399, 401-499, 1 34-13-00Page 596 1 1 Aug 01/05 1 1 1CES 1


 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
R  - push the ADR1 pushbutton 
R  switch. 


R  6. On the SWITCHING panel 8VU: 
R  - set the AIR DATA selector 
R  switch to CAPT/3. 
R  7. Do the ADR3 test as specified in 
R  the para. 1 and 2. 
R  8. On the ADIRS CDU, push the ADR1 
R  pushbutton switch. 
R  9. On the SWITCHING panel 8VU: 
R  - set the AIR DATA selector 
R  switch to NORM. 
R  10. On the ADIRS CDU, set the three 
R  OFF/NAV/ATT selector switches to 
R  OFF. 
R  After the ADR3 test, set the AIR 
R  DATA selector switch 15FP to 
R  NORMAL. 
R  **ON A/C ALL
 5. Close-up________
 Subtask 34-13-00-860-078

On the ADIRS CDU, the OFF legend of the ADR1 pushbutton switch comes on On the CAPT PFD, the speed and altitude indications go out of view.
On the CAPT PFD, the speed and altitude indications from the ADR3 are shown.
Same results on the CAPT side.
On the ADIRS CDU, the OFF legend of the ADR1 pushbutton switch goes off
On the CAPT PFD, the speed and altitude indications stay in view.
A. Put the aircraft back to its initial configuration.
 (1)
 On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.

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

 (3)
 On the FLT CTL panels 23VU and 24VU, push the FAC, ELAC and SEC pushbutton switches. The related OFF legend goes off.


R 1EFF : ALL 1 34-13-00Page 597 1 1 May 01/05 1 1 1CES 1


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

 Subtask 34-13-00-410-055
 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). Subtask 34-13-00-865-092
 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 7XE, 5CC1, 5CC2
R 1EFF : ALL 1 34-13-00Page 598 1 1 May 01/05 1 1 1CES 1


 TASK 34-13-00-740-003 SYSTEM TEST of the ADR
 1.
 Reason for the Job

__________________
 Self Explanatory


 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 31-32-00-860-010 Procedure to Get Access to the SYSTEM REPORT/TEST NAV
 Page 34-10-00-860-002 ADIRS Start Procedure 34-10-00-860-005 ADIRS Stop Procedure
 3. Job Set-up
__________ Subtask 34-13-00-860-079
 A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002).


 (2)
 Do the ADIRS start procedure (Ref. TASK 34-10-00-860-002).

 (3)
 
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