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时间:2011-04-21 08:08来源:蓝天飞行翻译 作者:航空
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 27-48-01
 úLEVERS ON THE CONTROL STAND  ú ú 02.1 Page 402 ú Sep 28/02
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A
757
MAINTENANCE MANUAL


AFT VIEW
B-B

Limit Switch and Position Transmitter Module Installation
Figure 401 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH ALTERNATE STAB TRIM ú

 27-48-01
 SWITCHES ON THE CONTROL STAND  ú ú 02 Page 403 ú Dec 20/91
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A

757 MAINTENANCE MANUAL
 (g)  
11H10, STAB TRIM POS IND L
 or STAB TRIM LEFT POS IND


 (h)  
11H11 or 11C05, STAB TRIM CONT L

 (i)  
11H19, STAB TRIM POS IND RIGHT

 (j)  
11H20, STAB TRIM CONT R


 S 864-004
 (3)  
Put the RIGHT and CENTER STAB TRIM SHUTOFF valve switches on the control stand panel, P10, to the CUTOUT position.

 S 864-005

 (4)  
Remove the power from the right and center hydraulic systems (Ref 29-11-00).


 S 014-006
 WARNING: STAY OFF THE SERVICE ACCESS DOOR, 311AL AND THE ELEVATOR
_______ CONTROL ACCESS DOOR, 313AL. YOUR WEIGHT CAN RELEASE THE SPRING-LOADED LATCHES ON THE DOOR. IF YOU FALL THROUGH THE DOOR, INJURIES CAN OCCUR.
 (5)  
Open the access door for the forward stabilizer compartment, 311AL (Ref 06-42-00).

 D.
Remove the LSTM (Fig. 401)


 S 034-007
 (1)  
Disconnect the electrical connector.

 S 034-008

 (2)  
Remove the bolts from the mounting flange on the LSTM.

 S 024-009

 (3)  
Carefully disengage the LSTM input shaft from the drive assembly.

 (4)  
Remove the LSTM.


 S 024-010
 TASK 27-48-01-424-011
 3.  Install the Limit Switch and Position Transmitter Module (LSTM)_______________________________________________________________
 A. Consumable Materials
 (1)  C00271 Conversion Coating - Iridite 14-2
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-48-01
 ALL  ú ú 04 Page 404 ú Jan 20/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

 B. References
 (1)  
06-42-00/201, Empennage Access Doors and Panels.

 (2)  
20-10-21/601, Electrical Bonding

 (3)  
20-10-22/701, Metal Surfaces Cleaning/Painting

 (4)  
20-30-03/201, Finishing Materials

 (5)  
24-22-00/201, Electrical Power - Control

 (6)  
27-41-00/501, Horizontal Stabilizer Trim Control System

 (7)  
27-48-00/501, Stabilizer Trim Position Indicating System

 C.
Access

 (1)  
Location Zones 211/212 Control Cabin 311/312 Area Aft of Pressure Bulkhead to BS 1787.45

 (2)  
Access Panel
 311AL Forward Stabilizer Compartment


 D.
Install the LSTM (Fig. 401)


 S 124-012
 (1)  
Clean the mating surfaces with abrasives (Ref 20-10-22).

 S 624-013

 (2)  
Apply a layer of Iridite 14-2 to the bare aluminum surfaces (Ref 20-30-03).

 S 424-014

 (3)
Carefully engage the LSTM input shaft to the drive assembly.


 NOTE: Make sure the tooth that is gone aligns with the splines on
____
 the mating part.

 S 434-015
 (4)  Turn the LSTM to align the mounting holes in the mounting flange with the holes in the drive assembly bracket.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-48-01
 ALL  ú ú 02 Page 405 ú Dec 20/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
 
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