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时间:2011-04-01 19:20来源:蓝天飞行翻译 作者:航空
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 27-41-81
 ALL  ú ú 02 Page 603 ú Mar 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
4.  BUSHING/SLEEVE (2 LOCATIONS)
FWD
(2 LOCATIONS)

 

NO. INDEX  PART NAME  DIM.  DESIGN LIMITS  WEAR LIMITS  PART WORN REPLACE  PART WORN REPAIR  INSTR REPAIR 
DIAMETER  DIM. WEAR MITTED PER- ANCE CLEAR-MAX DIA 
MIN  MAX 
4 BUSHING  ID  1.100  1.101  1.104  0.005  X 
SLEEVE  OD  1.098  1.099  1.097  X 
5 BUSHING  ID  1.000  1.001  1.004  0.005  X 
PIN  OD  0.998  0.999  0.997  X 
6 BUSHING  ID  0.750  0.751  0.754  0.005  X 
PIN  OD  0.748  0.749  0.747  X 
7  BUSHING  ID  1.000  1.001  1.004  0.005  X 
PIN  OD  0.998  0.999  0.997  X 

Gimbal Wear Limits
Figure 601 (Sheet 3)

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 27-41-81
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (c)  
Replace the parts that are not in the tolerance.

 (d)  
Install the parts.


 S 426-003
 (3)  Do this task: "Stabilizer Ball Nut and Jackscrew Gearbox Installation" (AMM 27-41-81/401).
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 27-41-81
 ALL  ú ú 01 Page 605 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 STABILIZER TRIM CUTOUT SWITCHES - REMOVAL/INSTALLATION
______________________________________________________
 1.  General_______
 A.  This procedure has two tasks, one for the removal and one for the installation of the stabilizer trim cutout switch (which is referred to as the cutout switch). The procedure has these parts:
 (1)  
The removal of the cutout switch

 (2)  
The installation of the cutout switch.

 B.  
This procedure can be used for the removal and installation of the main cutout switch S272 or the autopilot cutout switch S149.


 TASK 27-41-91-004-001
 2.  Stabilizer Trim Cutout Switches Removal (Fig. 401)_______________________________________
 A.  Special Tools and Equipment
 (1)  
AIRPLANES WITH THE TOGGLE SWITCHES;
 M81969/14-03 - Contact Installation/Removal Tool


 B.  
Access

 (1)  
Location Zones
 101 Control Cabin, LH
 102 Control Cabin, RH


 C.  
Procedure


 S 864-002
 (1)
Open these circuit breakers and attach DO-NOT-CLOSE tags:

 (a)  
P6 Circuit Breaker Panel
 1) STABILIZER TRIM CONT
 2) STABILIZER TRIM ACTUATOR

 

 S 014-006
 (2)  
AIRPLANES WITH THE CABLE ACTUATED SWITCHES; Remove the lower right access panel from the control stand.

 S 014-007

 (3)  
AIRPLANES WITH THE TOGGLE SWITCHES; Remove the access panel on the right side of the control stand.


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 27-41-91
 ALL  ú ú 02 Page 401 ú Jul 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

737-300/400/500MAINTENANCE MANUAL
CONTROL STAND
SEE A
BRACKET SCREWS
COTTER PIN
SWITCH MOUNTING BOOT
SCREWS (EXAMPLE)
CABLES
MAIN CUTOUT SWITCH, S272
ELECTRICAL CONNECTORBRACKET SCREWS
 
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