27-62-82
 ALL  ú ú 01 Page 601 ú Nov 15/91 
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. 
A 737-300/400/500MAINTENANCE MANUAL 
SEE A 
BEARING/BOLT  2  
BEARING/BOLT  2  
BEARING/BOLT  2  
(2 LOCATIONS)  
1. BEARING/BOLT  
BEARING/BOLT  2  
(2 LOCATIONS)  
1. BEARING/BOLT  
IDLER CRANK  
FWD  
A 
DESIGN LIMITS 
WEAR LIMITS MAXDIAMETER REPLACE REPAIRMAX DIAM 
INDEX WORN WORN REPAIRWEAR CLEAR-
NO.
PART NAME DIM. 
MIN 
MAX 
PART PART INSTR.
DIM. 
ANCE 
BEARING 
ID 0.5000 
0.5015 
0.5040 
X 
1
0.0045 
BOLT
OD 0.4985 
0.4995 
0.4970 
X 1 
1  CHROME PLATE THICKNESS 0.0030 INCH 
2  THE WEAR LIMITS SHOWN APPLY TO ALL BEARINGS AND BOLTS. ALL BEARINGS AND BOLTS ARE THE SAME DIAMETER WITH LENGTHS AS NECESSARY FOR THE INSTALLATION 
No. 4 and 5 Ground Spoiler Actuator Linkage Wear Limits
Figure 601
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. 
A 
737-300/400/500MAINTENANCE MANUAL
 NO. 0, 1, 8 AND 9 GROUND SPOILERS - REMOVAL/INSTALLATION
________________________________________________________
 1.  General_______
 A.  There are two tasks in this procedure. There is a task for the removal and a task for the installation of the No. 0, 1, 8 and 9 ground spoilers.
 B.  The graphite/composite ground spoilers and the aluminum/fiberglass ground spoilers are interchangeable.
 TASK 27-62-91-004-001
 2.  No. 0, 1, 8 and 9 Ground Spoiler Removal________________________________________
 A.  Special Tools and Equipment
 (1)  
C27001-34 Spoiler Ground Lock Set
 B.  
References
 (1)  
24-22-00/201, Manual Control
 (2)  
27-62-00/201, Speed Brake Control System
 C.  
Access
 (1)  
Location Zone 307, 407 Wing Trailing Edge Outboard Flaps and Spoilers
 D.  
Procedure
 S 864-002
 (1)  
Supply the electrical power (Ref 24-22-00/201).
S 864-003
 (2) 
Supply the systems A and B hydraulic power (Ref 27-62-00/201).
S 864-004
 (3)  
Move the flap control lever in the 40-unit detent to extend the trailing edge flaps.
S 864-005
 (4)  
Move the FLT CONTROL SPOILER system A and B switches to the OFF position.
 (5)  
Move the speed brake lever to the UP position to lift the spoilers.
 (6)  
Install the ground locks on the ground spoilers.
 (7) 
Remove the systems A and B hydraulic power (Ref 27-62-00/201).
S 024-009
 (8)  
Remove the ground spoiler (Fig. 401):
 (a)  
Remove the bolt that attaches the actuator rod end to the ground spoiler.
 S 864-006
 S 494-007
 S 864-008
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 27-62-91
 ALL  ú ú 01 Page 401 ú Nov 12/00 
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. 
A 737-300/400/500MAINTENANCE MANUAL 
SPOILER NO. 1  SPOILER NO. 8  
SPOILER NO. 0  SPOILER NO. 9  
SEE  A 
SPOILER ACTUATOR  
ROD END  
PHENOLIC  
SEE  B  RUB STRIP  
ADJUSTABLE SEAL 
GROUND SPOILER  
BONDING JUMPER  
FWD  INBD  SPOILER BOLTS 1 HINGE  A (EXAMPLE)  SPOILER HINGE BEARING SPOILER WASHER  SPOILER ATTACH 1 BOLT NUT ACTUATOR  
 
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