(2)
 Pressurize the Yellow hydraulic system from the Green hydraulic system through the Power Transfer Unit (PTU) (Ref. TASK 29-23-00-863-002).

 4. Procedure
_________

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 Subtask 27-51-00-710-067
 A. Operational Test of the Wing Tip Brake and the Pressure-Off Brake
 WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.

 NOTE : Use the Multipurpose Control Display Unit (MCDU) 3 on panel 1VU
____ for the test. If the MCDU 3 is defective, use the MCDU 2 on panel 11VU.
 NOTE : When you do this test the flap surfaces will move automatically.
____
 NOTE : Make sure that the CFDS is not in the SFCC menu mode before you
____ start the test. The test will not operate, if a BITE test was completed before. Subsequently Corrupted RAM - Return On Line - or Pin Prog Fault will be displayed.
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
 Set the Slat and Flap control  The Slats and Flaps move to the lever to the position 3. position 3.

 2.
 On the MCDU:  On the MCDU:

 -push the line key < SFCC 1 (2). - the MCDU shows the SFCC 1 (2) menu.
 NOTE : Use the SFCC 2 to do this test again for the WTB 33CV-B and 34CV-B.
____
 3. Push the NEXT PAGE button.  - the MCDU shows the next page of the SFCC 1 (2) menu.
 4. Push the line key TEST/RESET FLP >.  - the MCDU shows the SFCC 1 (2) FLAPTEST/RESET menu.
 5. Push the line key < WTB/POB TEST.  - the MCDU shows the SFCC 1 (2) FLAP WTB/POB TEST instructions.
 6. Push the line key < CONTINUE  - the MCDU shows the next page of the SFCC 1 (2) FLAP WTB/POB TEST instructions.
 7. Push the line key < START TEST.  - the MCDU shows that the FLAP WTB/POB TEST is IN PROGRESS.
 NOTE : If the line key < START____ TEST is not shown, do the instructions the MCDU
 shows.
 - the MCDU shows in less than 2 minutes
 SFCC 1 (2) PERFORMED
 NO FAULTS 

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-51-00Page 517 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1

 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------RESULT NOT STORED
 NOTE : When the test of the Wing Tip____
 Brake and the Pressure Off Brake
 will not operate, the subsequent
 message(s) is (are) displayed:
 Corrupted RAM - Return On Line ,
 or Pin Prog Fault.
 Then push the <RETURN key
 frequently to show the CFDS menu
 page. Then do the test again
 after the menu mode is
 displayed.
 8. Push the line key < RETURN
 frequently until the SYSTEM
 REPORT/TEST - F/CTL menu is
 shown.
 9. Make sure that the WTBs are not
 set.
 10. Open the circuit breakers 5CV
 and 6CV (flap and slat system
 1).
 11. Close the circuit breakers 7CV
 and 8CV (flap and slat system
 2).
 12. Use the SFCC 2 to do this test
 again.
 13. Push the line key <RETURN
 frequently until the CFDS menu
 page is shown.
 14. Close the circuit breakers 5CV
 and 6CV.
 15. Set the Slat and Flap control
 lever to the position 0. 

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-51-00Page 518 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1R **ON A/C 301-399,

R Subtask 27-51-00-710-067-A
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 : Use the Multipurpose Control Display Unit (MCDU) 3 on panel 1VU
____ R for the test. If the MCDU 3 is defective, use the MCDU 2 on panel R 11VU.
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 displayed.
R -------------------------------------------------------------------------------R ACTION RESULT R -------------------------------------------------------------------------------
　
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