NOTE: You can do the test for each phase independently.
____
 (e)  
Push the ALT FLAPS ARM switch to put the flap system in alternate control.

 (f)  
Turn the ALT FLAPS EXT/RET switch to extend the inboard flaps. 1) Measure the current in each of the three phases with the multimeter and current probe.

 2)  The difference in the current between the three phases must be less than 2.4 amps.

 (g)  
Turn the ALT FLAPS EXT/RET switch to retract the inboard flaps.

 (h)  
Push the ALT FLAPS ARM switch.

 S 865-009
 (3)  
Open these circuit breakers and attach DO-NOT-CLOSE tags:

 (a)  
P6, Main Power Distribution Panel
 1) 6L20, TE FLAP ELEC CONT INBD

 (b)  
P415, Power Distribution Center - Right
 1) 415A32, TE FLAP ELEC INBD

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-51-17
 ALL  ú ú 01 Page 502 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 085-010
 (4)  
Remove the test box:

 (a)  
Disconnect the test box cable from the motor and the connector.

 (b)  
Attach the electrical connector D625 to the inboard motor.

 S 725-011
 (5)  
Do the outboard drive motor test:

 (a)  
Remove the electrical connector D622 from the outboard drive motor.

 (b)  
Connect the test box to the outboard drive motor: 1) Connect the test box cable G27025-3 connector P2 to the motor. 2) Connect the test box cable connector J2 to the connector DM622.

 3)  Connect the cable connector P1 to the test box connector J1.

 (c)  
Remove the DO-NOT-CLOSE tags and close these circuit breakers: 1) P6, Main Power Distribution Panel a) 6L19, TE FLAP ELEC CONT OTBD

 2)  P415, Power Distribution Center - Right a) 415M38, TE FLAP ELEC OTBD

 (d)  
Put the multimeters and current probes on the cables A, B and C in the test box.

 NOTE: You can do the test for each phase independently.
____
 (e)  
Push the ALT FLAPS ARM switch to put the system in alternate control.

 (f)  
Turn the ALT FLAPS EXT/RET switch to extend the outboard flaps. 1) Measure the current in each of the three phases. 2) The difference in the current between the three phases must

 be less than 2.4 amps.

 (g)  
Turn the ALT FLAPS EXT/RET switch to retract the outboard flaps.

 (h)  
Push the ALT FLAPS ARM switch.

 S 865-012
 (6)  
Open these circuit breakers and attach DO-NOT-CLOSE tags:

 (a)  
P6, Main Power Distribution Panel
 1) 6L19, TE FLAP ELEC CONT OTBD

 (b)  
P415, Power Distribution Center - Right
 1) 415M38, TE FLAP ELEC OTBD

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-51-17
 ALL  ú ú 01 Page 503 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 085-013
 (7)  
Remove the test box:

 (a)  
Disconnect the test box cable from the motor and the connector.

 (b)  
Attach the electrical connector D622 to the outboard motor.

 G.
Put the Airplane Back to its Usual Condition

 S 865-014
 (1)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:

 (a)  
P6, Main Power Distribution Panel
 1) 6L19, TE FLAP ELEC CONT OTBD
 2) 6L20, TE FLAP ELEC CONT INBD

 (b)  
P415, Power Distribution Center - Right
 1) 415A32, TE FLAP ELEC INBD
 2) 415M38, TE FLAP ELEC OTBD

 S 865-015
 (2)  Do this task: "Remove Electrical Power" (AMM 24-22-00/201).
 S 495-016
 WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASK BELOW TO REMOVE THE
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機(jī)維護(hù)手冊 飛行操縱 FLIGHT CONTROLS 4(163)