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 (c)  Set the elevator system back to the usual condition (AMM 27-31-00/501).
 S 735-718-002
 (3)  Aileron Position Test
 (a)  
Make sure the aileron and aileron trim control system are operational (AMM 27-11-00/501).

 (b)  
Set the SUBFRAME and WORD for each signal and set the aileron position as shown in the table that follows:

 ~...................................................................... | SIGNAL | TESTER SETUP | | ................................................... TESTER | | AILERON | POSITION | SUBFRAME | WORD | DISPLAY | ........................................................................ | LEFT | NEUTRAL | 2 | 44 | 7514 to 0264 | | ........................................................... | | FULL UP | 2 | 44 | 3010 to 3564 | 2............…............…............…..........…....................1
 (c)  Set the aileron back to the usual condition (AMM 27-11-00).
 S 735-719-002
 (4)  Control Column Position (Syncro) Test
 (a)  Set the SUBFRAME to 0 and the WORD to 13.
 
 GUN 001-008, 010, 101 POST-EO B531006;  ú 31-31-00
 GUN 051, 102-999  ú CONFIG 2 ú 06 Page 521 ú Sep 28/01

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MAINTENANCE MANUAL

 (b)  
Set the control column to the position as shown in the table that follows:

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

 ~.................................................. | TEST | POSITION | TESTER DISPLAY | .................................................... | CONTROL | FULLY FORWARD | 7253 to 7616 | | COLUMN ....................................... | | FULLY AFT | 0315 to 0661 | 2............…..................…..................1

 (d)  
Set the control column to the neutral position.

 S 735-720-002
 (5)  Control Wheel Position (Syncro) Test
 (a)  
Set the SUBFRAME to 0 and the WORD to 12.

 (b)  
Set the control wheel 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 | .................................................... | CONTROL | FULLY CLOCKWISE | 6700 to 6760 | | WHEEL ....................................... | | FULLY | 1020 to 1100 | | | COUNTERCLOCKWISE | | 2............…..................…..................1

 (d)  
Set the control wheel back to the neutral position.

 S 735-721-002
 (6)  Rudder Pedal Position (Syncro) Test
 (a)  Set the SUBFRAME to 0 and the WORD to 49.
　
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本文鏈接地址：757 AMM 飛機(jī)維護(hù)手冊(cè) 儀表 CHAPTER 31 - INSTRUMENTS 1(91)