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 1.  General_______
 A.  This procedure has one task. The task is an inspection of the horizontal stabilizer. The procedure has these parts:
 (1)  
The removal of the horizontal stabilizer

 (2)  
An inspection of the horizontal stabilizer

 (3)  
The installation of the horizontal stabilizer.

 TASK 27-41-11-206-001
 2.  Horizontal Stabilizer Inspection (Fig. 601)________________________________
 A.  Standard Tools and Equipment
 (1)  
Micrometer - 0-1 inch

 (2)  
Vernier Caliper

 B.  
References

 (1)  
27-41-11/401, Horizontal Stabilizer

 C.  
Access

 (1)  
Access Panels
 3801 Tail Cone Access Door, LH
 3802 Tail Cone Access Door, RH

 D.  
Procedure

 S 026-002
 (1)  
Do this task: "Horizontal Stabilizer Removal" (Ref 27-41-11/401).

 S 216-003

 (2)  
Examine the parts for worn areas:

 (a)  
Use a micrometer or a vernier caliper to measure the parts for the worn areas.

 (b)  
Compare the dimensions you measured with the permitted dimensions shown in Fig. 601.

 (c)  
Replace the parts that are not in the tolerance.

 (d)  
Install the parts.

 S 426-004
 (3)  Do this task: "Horizontal Stabilizer Installation"
 (Ref 27-41-11/401).

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
REAR SPAR FITTINGS
SEE B
HINGE SUPPORT
FWD
A 737-300/400/500MAINTENANCE MANUAL
FRONT SPAR FITTINGS
SEE A
JACKSCREW SUPPORT
1. BUSHING/BOLT 
3. BUSHING/BOLT 
UPPER FITTING 
4. BUSHING/BOLT 
CENTER FITTING 
5. BUSHING/BOLT 
2. BUSHING/BOLT 

LOWER FITTING
B
A
Horizontal Stabilizer Wear Limits Figure 601 (Sheet 1)
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 ALL  ú ú 01 Page 602 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
NO. INDEX  PART NAME  DIM.  DESIGN LIMITS  WEAR LIMITS  PARTWORN REPLACE  PART WORN REPAIR  INSTR REPAIR 
DIAMETER  PER-MITTED WEAR DIM.  ANCE CLEAR-MAX DIA 
MIN  MAX 
1  BUSHING  ID  1.0030 1.0045 1.0090  .010  1 
BOLT  OD  .9985  .9990  .9930  1 
2  BUSHING  ID  .8780  .8795  .8840  .010 1 
BOLT  OD  .8735  .8740  .8680 1 
3 BUSHING  ID  1.3781  1.3791  1.3840  .010 1 
BOLT  OD  1.3725  1.3740  1.3681  1 
4 BUSHING  ID  1.3781  1.3791 1.3840  .010  1 
BOLT  OD  1.3725  1.3740  1.3681  1 
5 BUSHING  ID  1.5031  1.5041  1.5090  .010 1 
BOLT  OD  1.4975  1.4990  1.4931 1 

REPLACE WITH NEW PART HAVING SAME PART NUMBER
Horizontal Stabilizer Wear Limits
Figure 601 (Sheet 2)

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 ALL  ú ú 01 Page 603 ú Mar 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 HORIZONTAL STABILIZER LEADING EDGE - REMOVAL/INSTALLATION
_________________________________________________________
 1.  General
_______
 A.  This procedure has two tasks, one for the removal and one for the installation of the horizontal stabilizer leading edge (which is referred to as the leading edge). The procedure has these parts:
　
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