CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (2)  
Do this task to pressurize the hydraulic systems No. 2 and No. 3: "Supply Hydraulic Power" (AMM 29-11-00/201).

 S 864-004

 (3)  
Use the STAB TRIM ALTN switch to move the stabilizer to the 3 units of trim (Fig. 401).

 S 864-005

 (4)  
Do this task to release the pressure in the hydraulic systems No. 2 and No. 3: "Remove Hydraulic Power" (AMM 29-11-00/201).

 S 864-006

 (5)  
Set the STAB TRIM 2 and 3 switches on control stand to CUTOUT.

 S 864-007

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

 (a)  
P7, Overhead Circuit Breaker Panel 1) 7E7, L STAB TRIM S/O VLV 2) 7E20, R STAB TRIM S/O VLV

 S 864-008
 (7)  
If the electrical power is not necessary, do this task: "Remove Electrical Power" (AMM 24-22-00/201).

 S 014-009

 (8)  
Open the access door 312A (AMM 06-09-05/201).

 S 014-010

 (9)  
Remove the removal door of the safety rod.

 S 874-011

 (10)
 Drain the oil from the primary brake housing (Section A-A, Sheet 2, Fig. 401).

 S 434-024

 (11)
 Install the drain plug:

 (a)  
Tighten the drain plug.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-41-13
 ALL  ú ú 01 Page 404 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (b)  
Install a lockwire on the drain plug.

 F.  
Remove the Lip Seal

 S 494-012
 (1)  
Install the safety rod adapter to the higher end of the safety rod:

 (a)  
Remove the lockbolt of the safety rod nut.

 (b)  
Remove the safety rod nut.

 (c)  
Attach the safety rod adapter to the top of the safety rod.

 1)  Tighten the adapter lanyard to the structure to hold the safety rod.
 S 014-013
 (2)
Remove the safety rod from the horizontal stabilizer actuator:

 (a)  
Remove the safety shaft retaining bolt from the lower gimbal retaining pin.

 (b)  
Remove the safety shaft.

 (c)  
Remove the safety rod through the removal door.

 NOTE: The safety rod weight is approximately 35 pounds.
____
 S 024-014
 (3)  
Remove the lip seal:

 (a)  
Remove the lip seal housing: 1) Remove the attachment screws. 2) Remove the lip seal housing through the space between the

 lower gimbal and the bottom of the primary brake housing.

 (b)  
Remove the lip seal and the O-ring from the lip seal housing.

 TASK 27-41-13-404-015
 3.  Stabilizer Trim Drive Mechanism Lip Seal Installation_____________________________________________________
 A.  Special Tools and Equipment
 (1)
3MIT65B03670 Horizontal Stabilizer Actuator Safety Rod Adapter

 B.  
Consumable Materials

 (1)  
D00270 Hydraulic Fluid - MIL-H-5606

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-41-13
 ALL  ú ú 01 Page 405 ú Feb 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 (2)  
D00633 Grease - BMS 3-33 (Preferred)

 (3)  
D00013 Grease - MIL-G-23827 (Optional)

 C.
Access

 (1)  
Location Zone
 311 Area Aft of Pressure Bulkhead, LH
 312 Area Aft of Pressure Bulkhead, RH

 (2)  
Access Panel
 312A Horizontal Stabilizer Jackscrew Access Door

 D.
Procedure

 S 424-016
 (1)  
Install the lip seal in the lip seal housing:

 (a)  
Apply a thin layer of grease (BMS 3-33 to MIL-G-23827) to the inside of the lip seal housing.
　
中國(guó)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(cè) 飛行操縱 FLIGHT CONTROLS 4(8)