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时间:2011-03-25 23:58来源:蓝天飞行翻译 作者:admin
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 Subtask 32-46-00-860-051
 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 AIDR stop procedure (Ref. TASK 34-10-00-860-005).

 (3)
 Remove the warning notice(s).

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

 

R **ON A/C 106-149, 221-299, 401-499,
 Subtask 32-46-00-860-051-A
 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 AIDR stop procedure (Ref. TASK 34-10-00-860-005).

 (3)
 Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).

 (4)
 Remove the warning notice(s).

 (5)
 De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002).

 

 1EFF : ALL 1 32-46-00Page 506 1 1 Aug 01/05 1 1 1CES 1R **ON A/C ALL


 TASK 32-46-00-740-002
 BITE Test of the BSCU - Ground Scanning

 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific  warning notice
 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 31-32-00-860-009 Procedure to Get Access to the SYSTEM REPORT/TEST/L/G Page
 3. Job Set-up
__________
 Subtask 32-46-00-860-054

 A. Aircraft Maintenance Configuration
 (1)
 On the panel 400VU, make sure that the L/G normal control-lever is set to DOWN.

 (2)
 On the panel 402VU, make sure that the A/SKID & NOSE WHEEL switch is at ON.


 1EFF : ALL 1 32-46-00Page 507 1 1 Feb 01/04 1 1 1CES 1


 (3)
 Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002).


 (4)
 On one MCDU, get the SYSTEM REPORT/TEST/L/G Page (Ref. TASK 31-32-00-860-009).


 Subtask 32-46-00-941-055
 B. Safety Precautions
 (1) Put a warning notice on the L/G normal control-lever to tell persons not to move it.
 Subtask 32-46-00-865-051
 C. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU HYDRAULIC/BRAKING AND STEERING/SYS2/SPLY 4GG M36 121VU HYDRAULIC/BRAKING AND STEERING/SYS2/CTL 3GG M35 121VU HYDRAULIC/BRAKING AND STEERING/SYS1/CTL 1GG M34 121VU HYDRAULIC/BRAKING AND STEERING/SYS1/IND AND/SPLY 2GG M33
 4. Procedure
_________
R  **ON A/C 001-049, 051-099, 101-105, 151-199, 201-220, 301-399,
 Subtask 32-46-00-740-051
 A. Do this test:
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
 On the MCDU, push the line key  - the BSCU SYS 1 page comes into view. adjacent to the BSCU 1 indication.

 2.
 Push the line key adjacent to the - the BSCU SYS 1/GROUND SCANNING page


 GND SCAN indication.  comes into view. If the test finds no faults:
 -the NO FAILURE indication comes into view.
 1EFF : ALL 1 32-46-00Page 508 1 1 May 01/05 1 1 1CES 1


 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------If the test results are incorrect:
 -a list of fault messages comes into view.
 3.
 Push the line key adjacent to the
 RETURN indication to get the
 SYSTEM REPORT/TEST/L/G page.


 4.
 Push the line key adjacent to the
 
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