(b)  
Open these circuit breakers and attach DO-NOT-CLOSE tags:

 1)  P180 DC Power Distribution Panel a) 180E7, ELEV/RUD VLV SYS 2 b) 180E22, ELEV/RUD VLV SYS 4 c) 180H8, ELEV/RUD VLV SYS 1 d) 180H23, ELEV/RUD VLV SYS 3
 WARNING:_______DO NOT TOUCH THE PNEUMATIC DUCTS WHEN THEY ARE HOT. WHEN THE DUCTS ARE HOT THEY CAN CAUSE INJURY TO PERSONS.
 (c)  Visually examine the EAS and make sure there is no hydraulic leakage.
 L.  Restore the Airplane to Normal
 S 864-139
 (1)  Remove DO-NOT-CLOSE tags and close these circuit breakers:
 (a)  P180 DC Power Distribution Panel
 1) 180E7, ELEV/RUD VLV SYS 2
 2) 180E22, ELEV/RUD VLV SYS 4
 3) 180H8, ELEV/RUD VLV SYS 1

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 4)  180H23, ELEV/RUD VLV SYS 3
 (2)  S 864-140Put the FLT CONT HYD POWER TAIL 1, 2, and 3 switches in the NORM position. You can find these switches on the Pilots' Overhead Maintenance Panel (P461).
 (3)  S 414-141Close access panel 315A (AMM 06-09-05/201).
 (4)  S 414-190Close the ceiling panel in the area below the control columns (AMM 25-59-01/401).
 (5)  S 864-145Remove hydraulic power if it is not necessary (AMM 29-11-00/201).
 (6)  S 864-146Remove electrical power if it is not necessary (AMM 24-22-00/201).

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747-400 MAINTENANCE MANUAL
 ELEVATOR AUTOPILOT SERVO MECHANICAL LINKAGE - INSPECTION/CHECK
______________________________________________________________
 1.  General_______
 A.  There are two tasks in this procedure. The first task is for the visual inspection of the elevator autopilot servo (EAS) mechanical linkage. The second task is for the full inspection of the EAS mechanical linkage.
 B.  In the first task, you do not have to remove the EAS mechanical linkage. In the second task, you have to remove the EAS mechanical linkage for a full inspection of the worn areas. Usually you use the second task when you do the overhaul of the EAS mechanical linkage.
 TASK 22-12-01-206-007
 2.  EAS Mechanical Linkage Visual Inspection (Fig. 601)________________________________________
 A.  General
_______
 (1)  This procedure is for a visual inspection of the EAS mechanical linkage for bends, cracks, corrosion, or worn areas. In this procedure, you do not have to remove the mechanical linkage if it is not necessary.
 B.  References
 (1)  
AMM 06-09-05/201, Body Section 48 Access Doors and Panels

 (2)  
AMM 24-22-00/201, Manual Control

 (3)  
AMM 29-11-00/201, Main Hydraulic Supply System

 C.  Access
 (1)  
Location Zones 315 Area Aft of Stabilizer Box Compartment, LH 316 Area Aft of Stabilizer Box Compartment, RH

 (2)  
Access Panel
 315A Access Door

 D.  Procedure
 S 866-008
 (1)  
Supply electrical power (AMM 24-22-00/201).

 S 866-009

 (2)  
Remove the hydraulic pressure from the correct hydraulic system given below (AMM 29-11-00/201):

 (a)  
Center EAS - hydraulic system No. 1

 (b)  
Right EAS - hydraulic system No. 2

 (c)  
Left EAS - hydraulic system No. 3

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