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 WARNING:  BE CAREFUL WHEN YOU REMOVE THE CLAMP-ON AC CURRENT PROBE FROM THE POWER PANEL. THE VOLTAGES IN THE POWER PANEL CAN KILL AND/OR CAUSE DAMAGE TO EQUIPMENT.
 2)  Remove the clamp-on ac current probe from the wire at the ACMP ELCU in the P31 panel.
 I.  Put the Airplane Back to Its Usual Condition
 S 866-366
 (1)  Remove hydraulic power (AMM 29-11-00/201).
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 29-11-00
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 S 026-517
 (2)  
Remove the Yaw Damper Module Simulators and put the Yaw Damper Modules into place (Fig. 207).

 S 416-370

 (3)  
Close the access panels, 434AL and 444AL, for the hydraulic bay in the aft strut (AMM 06-43-00/201).

 S 416-371

 (4)  
Close the access door for the central hydraulic service center (AMM 06-41-00/201).

 S 416-372

 (5)  
Install the access panel, 561AB, for the aileron quadrant (AMM 06-44-00/201).

 S 416-373

 (6)  
Install the access panel, 345DB, for the right elevator PCA and the access panel, 335DB, for the left elevator PCA (AMM 06-42-00/201).

 S 416-374
 WARNING:_______USE THE PROCEDURE AMM 32-00-15 TO REMOVE THE DOOR LOCKS. THE DOORS OPEN AND CLOSE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (7)  
Remove the door locks from the landing gear doors and close the doors (AMM 32-00-15/201).

 (8)  
Remove electrical power if it is not necessary (AMM 24-22-00/201).

 S 866-369
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 29-11-00
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FULL CHECK
Component Check for the Left Hydraulic System
Figure 610 (Sheet 1)

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