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时间:2011-04-10 10:01来源:蓝天飞行翻译 作者:航空
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_______________________________________________________________
 1.  General_______
 A.  This procedure has three tasks. There is one task each for the removal, the installation, and the operational test of the stabilizer trim drive mechanism lip seal (which is referred to as the "lip seal"). The procedure has these parts:
 (1)
The removal of the lip seal

 (2)
The installation of the replacement lip seal

 (3)
An operational test of the lip seal.

 B.  
The lip seal is at the bottom of the primary brake housing of the stabilizer trim drive mechanism.

 C.  
If there are leaks from the joint, you can replace the lip seal without removing the stabilizer trim drive mechanism.


 TASK 27-41-13-004-001
 2.  Stabilizer Trim Drive Mechanism Lip Seal Removal________________________________________________
 A.  Special Tools and Equipment
 (1)
3MIT65B03670 Horizontal Stabilizer Actuator Safety Rod Adapter

 B.  
Consumable Materials

 (1)
D00633 Grease - BMS 3-33 (Preferred)

 (2)
D00013 Grease - MIL-G-23827 (Optional)

 C.  
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

 D.  
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

 E.  
Prepare for Removal

 (1)
Do this task: "Supply Electrical Power" (AMM 24-22-00/201).


 S 864-002
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

SEE  B 
STABILIZER 
TRIM 
NEUTRAL 
POSITION 
SEE  C 

SEE  A 
SEE  D 
SAFETY ROD 
SAFETY 
ROD NUT 
SAFETY ROD 
NUT LOCKBOLT  A 

1 THE STABILIZER IS IN THE NEUTRAL POSITION WHEN THE DIMENSION BETWEEN THE NORMAL SURFACES OF THE BALL NUT AND THE BALL SCREW STOPS IS
7.42 |0.05 INCHES
B
(188.5 |1.3 MILLIMETERS)
Stabilizer Trim Drive Mechanism Lip Seal Installation Figure 401 (Sheet 1)
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 ALL  ú ú 01 Page 402 ú Feb 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 747-400 MAINTENANCE MANUAL 
LANYARD 
OIL DRAIN PLUG 
OIL FILLER PLUG 
LIP SEAL HOUSING 
SAFETY ROD TOOL 
SAFETY ROD 
LIP SEAL  O-RING  A-A 

A  RETAINING BOLT (2 LOCATIONS) SAFETY SHAFT (3 LOCATIONS) LIP SEAL HOUSING ATTACHMENT SCREW 
A  SAFETY SHAFT 
LOWER GIMBAL RETAINING PIN 
D  SAFETY SLEEVE SAFETY SLEEVE RETAINING RING 
Figure 401 (Sheet 2) Stabilizer Trim Drive Mechanism Lip Seal Installation

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 27-41-13
 ALL  ú ú 01 Page 403 ú Oct 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 S 864-003

 WARNING:_______ MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
 SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER.  AILERONS, RUDDERS,
 ELEVATORS, FLAPS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS
 CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER.  THIS CAN
 
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