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时间:2011-03-21 14:12来源:蓝天飞行翻译 作者:admin
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R  Subtask 27-51-00-860-052-A 
R  E. Aircraft Maintenance Configuration 
R R  (1) Pressurize the Blue hydraulic system with the electric pump (Ref. TASK 29-10-00-863-003). 
R R R  (2) Pressurize the Green hydraulic system from the Yellow hydraulic system through the Power Transfer Unit (PTU) with the electric pump (Ref. TASK 29-23-00-863-001).

 

 4. Procedure
_________
 Subtask 27-51-00-710-052 R A. Operational Test of the Wing Tip Brake and the Pressure-Off Brake R WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ R CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS R AND/OR DAMAGE.
R NOTE : When you do this test the flap surfaces will move automatically.
____ R NOTE : Make sure that the CFDS is not in the SFCC menu mode before you
____ R start the test. The test will not operate, if a BITE test was R completed before. Subsequently Pin Prog Fault will be shown.
R -------------------------------------------------------------------------------R ACTION RESULT
R -------------------------------------------------------------------------------
R 1. Set the Slat and Flap control The Slats and Flaps move to the
R lever to the position 3. position 3.

R 2. On the MCDU: ON the MCDU:
R - push the line key < SFCC 1 (2). - the MCDU shows the SFCC 1 (2) menu.

R NOTE : Use the SFCC 2 to do this test again for the WTB 33CV-B and 34CV-B.

____
R 3. Push the NEXT PAGE button. R
R 4. Push the line key TEST/RESET FLP R >.
R 5. Push the line key < WTB/POB TEST. R
R 6. Push the line key < CONTINUE. R R
R 7. Push the line key < START TEST. R R NOTE : If the line key < START
____ R TEST is not shown, do the R instructions that the MCDU R shows.
-
the MCDU shows the next page of the SFCC 1 (2) menu.

-
the MCDU shows the SFCC 1 (2) FLAP TEST/RESET menu.

-
the MCDU shows the SFCC 1 (2) FLAP WTB/POB TEST instructions.

-
the MCDU shows the next page of the SFCC 1 (2) FLAP WTB/POB TEST instructions.

-
the MCDU shows that the FLAP WTB/POB TEST is IN PROGRESS

 


 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
R  - the MCDU shows in less than 2 minutes 
R  SFCC 1 (2) 
R  PERFORMED 
R  NO FAULTS 
R  RESULT NOT STORED 
R  - if the MCDU shows: 
R  PERFORMED UNSUCCESSFULLY 
R  do the steps 1 thru 7 again a maximum 
R  of three times 

R  - if the MCDU still shows 
R  PERFORMED UNSUCCESSFULLY 
R  do the full test procedure with a 
R  Ground Power Cart (Ref. TASK 27-51-
R  00-710-003) or 
R  the Engine Driven Pumps 
R  (Ref. TASK 27-51-00-710-004). 

R  NOTE : When the test of the Wing Tip____ 
R  Brake and the Pressure Off Brake 
R  will not operate, the subsequent 
R  message is shown: 
R  Pin Prog Fault. 
R  Push the <RETURN key frequently 
R  to show the CFDS menu page. Then 
R  do the test again after the menu 
R  mode is shown. 
R  8. Push the line key < RETURN 
R  frequently until the SYSTEM 
R  REPORT/TEST - F/CTL menu is 
R  shown. 
R  9. Make sure that the WTBs are not 
R  set. 
R  10. Open the circuit breakers 5CV 
R  and 6CV (flap and slat system 
R  1).

 

 -------------------------------------------------------------------------------
ACTION RESULT
 -------------------------------------------------------------------------------R 11. Close the circuit breakers 7CV R and 8CV (flap and slat system R 2).
R 12. Use the SFCC 2 to do this test R again.
R 13. Push the line key < RETURN R frequently until the CFDS menu R page is shown.
R 14. Close the circuit breakers 5CV R and 6CV.
R 15. Set the Slat and Flap control R lever to the position 0.
 5. Close-up
________
 Subtask 27-51-00-865-056

 A. Make sure that this(these) circuit breaker(s) is(are) closed: 7CV, 8CV. R Subtask 27-51-00-860-053-A
R B. Aircraft Configuration R (1) De-pressurize the Green and Yellow hydraulic systems (Ref. TASK 29-R 23-00-864-001).
R (2) De-pressurize the Blue hydraulic system (Ref. TASK 29-10-00-864-003). R (3) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-R 002). Subtask 27-51-00-942-051
 
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