A
757 
MAINTENANCE MANUAL
 S 865-710
 (34)
 Release the CONFIG switch.
S 865-711
 (35)
 Put the ALTN FLAPS control in the 25-unit position.
S 865-712
 (36)
 Put the TE switch in the ALTN position to activate the TE flaps electric drive.
 NOTE: Permit time for the flaps to get to the 25-unit position.
____
 S 865-713
 (37) Hold the CONFIG switch on the TEST panel in the T/O position.
 (a)  Make sure the red EICAS message, FLAPS, shows on the top display when the EICAS COMPUTER switch is in the L and R positions.
 S 865-714
 (38)
 Release the CONFIG switch.
S 865-715
 (39)
 Put the TE switch in the NORM position to deactivate the TE flaps electric drive.
 NOTE:____The flaps will move to the 20-unit position. The slats will start to move to the fully extended position then reverse direction and stop at the intermediate position.
 S 865-716
 (40) Put the LE switch in the ALTN position to activate the LE slats electric drive.
 NOTE: Permit time for the slats to get to the fully extended
____
 position.
 S 865-717
 (41) Hold the CONFIG switch on the TEST panel in the T/O position.
 (a)  Make sure the red EICAS message, FLAPS, shows on the top display.
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MAINTENANCE MANUAL
 S 865-718
 (42)
 Release the CONFIG switch.
S 865-719
 (43)
 Put the FLAP lever in the 5-unit position.
S 865-720
 (44)
 Make sure that the flaps and slats do not move.
S 865-721
 (45)
 Put the LE switch in the NORM position to deactivate the LE slats electric drive.
 NOTE:____The flaps will move to the 5-unit position. The slats will move to the intermediate position.
 S 865-824
 (46) Open these P11 panel circuit breakers:
 (a)  
11C14, FLAP/SLAT ELEC UNIT 2 POWER
 (b)  
11C15, FLAP/SLAT ELEC UNIT 2 CONT
 (c)  
11C16, FLAP/SLAT ELEC UNIT 2 SENSOR
 S 865-825
 (47) Close these P11 panel circuit breakers:
 (a)  
11G12, FLAP/SLAT ELEC UNIT 1 POWER
 (b)  
11G13, FLAP/SLAT ELEC UNIT 1 CONT
 (c)  
11G14, FLAP/SLAT ELEC UNIT 1 SENSOR
 S 865-827
 (48)
 Put the LE and TE switches in the NORM position.
S 865-805
 (49)
 Set the FLAP control to the UP position.
S 865-806 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址:757 AMM 飞机维护手册 仪表 CHAPTER 31 - INSTRUMENTS 2(119)