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MAINTENANCE MANUAL

 (b)  
Set the rudder pedal to the position as shown in the table that follows:

 (c)  
Make sure the tester display shows the correct value as listed in the table.

 ~..................................................... | TEST | POSITION | TESTER DISPLAY | ....................................................... | RUDDER | LEFT FULLY FORWARD | 0367 to 0655 | | PEDAL .......................................... | | RIGHT FULLY FORWARD | 7140 to 7401 | 2............….....................…..................1

 (d)
Set the rudder position back to the neutral position.

 Z. Flap Handle Position Test
 S 735-755-002
 (1)  Do the flap handle test that follows:
 (a)  
Make sure these circuit breakers on the overhead circuit breaker panel, P11, are close: 1) 11G12, FLAP/SLAT ELEC UNIT-1 PWR 2) 11G13, FLAP/SLAT ELEC UNIT-1 CONT 3) 11G14, FLAP/SLAT ELEC UNIT-1 SENSOR

 (b)  
On the tester, set the SUBFRAME to 3 and the WORD to 14.

 (c)  
Set the flap handle position, and make sure the tester display shows the value as shown in the table that follows:

 ~............................................. | FLAP HANDLE POSITION | TESTER DISPLAY | ............................................... | UP | 0000 to 2211 | ............................................... | 15 | 4426 to 5156 | 2........................…....................1
 
 GUN 001-008, 010, 101 POST-EO B531006;  ú 31-31-00
 GUN 051, 102-999  ú CONFIG 2 ú 06 Page 523 ú May 28/02

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MAINTENANCE MANUAL

 (d)  Set the flap handle to the UP position.
 S 735-746-002
 (2)  Leading Edge Slat Position Test
 (a)  
Make sure the leading edge slat system is operational
 (AMM 27-81-00).

 (b)  
Set the SUBFRAME and WORD for each parameter condition as shown in the table that follows.

 (c)  
Make sure the tester display shows the correct data for each postion.

 ~................................................................ | | TESTER SETUP | TESTER DISPLAY | | L.E. SLATS/CONDITION ........................................... | | SUBFRAME | WORD |BIT (DISCRETE)| VALUE | .................................................................. | FULL EXTEND | 0 | 03 | 1 | 1 | .................................................................. | NOT FULLY EXTEND | | | | 0 | .................................................................. | PART EXTEND | 0 | 11 | 1 | 1 | .................................................................. | NOT PART EXTEND | | | | 0 | .................................................................. | RETRACTED | 0 | 19 | 1 | 1 | .................................................................. | NOT RETRACTED | | | | 0 | .................................................................. | FAIL *[1] | 0 | 27 | 1 | 1 | .................................................................. | NOT FAIL | | | | 0 | 2......................…..........….......…..............….......1 *[1] Uncommanded motion (UCM) or Asymmetry. Refer to 27-81-00 to make the slat condition of the UCM. To created the UCM
　
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