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时间:2011-03-25 18:01来源:蓝天飞行翻译 作者:admin
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 Subtask 32-42-00-865-066
 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 32-42-00-740-053
 A. Do this test:
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
 On the MCDU, push the line key  The BSCU SYS1 page comes into view. adjacent to the BSCU1 indication

 2.
 Push the line key adjacent to the The BSCU SYS1/LAST LEG REPORT page


 LAST LEG REPORT indication.  comes into view. Make sure that none of these messages is shown for the non affected wheels: TACHOMETER 19(20)(21)(22) GG or BSCU.
 1EFF : ALL 1 32-42-00Page 427 1 1 May 01/05 1 1 1CES 1


 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
NOTE : TACHOMETER 19 is for wheel
____ N..1, 20 for wheel N..3, 21 for wheel N..2 and 22 for wheel N..4.
 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 BSCU2 indication.

 5.
 Do the same actions as in Para.


2.
R **ON A/C 106-149, 221-299, 401-499,
 Subtask 32-42-00-740-053-A
 A. Do this test:
The SYSTEM REPORT/TEST/L/G page comes
into view.
The BSCU SYS2 page comes into view.
Same results as for the BSCU SYS1.

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
 On the MCDU, push the line key adjacent to the BSCU1 indication

 2.
 Push the line key adjacent to the LAST LEG REPORT indication.

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 BSCU2 indication.


The BSCU CHAN 1 page comes into view.

The BSCU CHAN 1/LAST LEG REPORT page
comes into view.
 Make sure that none of these messages
 is shown for the non affected wheels:
 TACHOMETER1(19GG)/BSCU(10GG)
 TACHOMETER2(21GG)/BSCU(10GG)
 TACHOMETER3(20GG)/BSCU(10GG)
 TACHOMETER4(22GG)/BSCU(10GG)

The SYSTEM REPORT/TEST/L/G page comes
into view.

The BSCU CHAN 2 page comes into view.

 1EFF : ALL 1 32-42-00Page 428 1 1 Aug 01/05 1 1 1CES 1


 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
5. Do the same actions as in Para. Same results as for the BSCU CHAN 1.
 2. **ON A/C ALL
 5. Close-up
________ Subtask 32-42-00-860-082
 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)
 De-energize the aircraft electrical circuits

 (3)
 Remove the warning notice(s).

 (4)
 In the cockpit, install a temporary placard to tell the crew that the autobrake function is inoperative.

 (5)
 Make an entry in the log book.


 1EFF : ALL 1 32-42-00Page 429 1 1 May 01/04 1 1 1CES 1 NORMAL BRAKING - ADJUSTMENT/TEST


________________________________
 TASK 32-42-00-710-001
 Operational Check of the Normal Braking System
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
 WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
 WARNING : MAKE SURE THAT THE CONTROLS AGREE WITH THE POSITION OF THE ITEMS THEY
_______ OPERATE BEFORE YOU PRESSURIZE A HYDRAULIC SYSTEM.
 WARNING : PRESSURIZE ONLY THE HYDRAULIC SYSTEM(S) THAT IS (ARE) NECESSARY FOR
_______ THE TASK. ISOLATE THE OTHER HYDRAULIC SYSTEM(S) BEFORE YOU SUPPLY HYDRAULIC POWER TO THE AIRCRAFT.
 
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