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 A.  There are two tasks in this procedure. There is a task for the adjustment and a task for the functional test of the ground spoiler interlock valve.
 B.  The airplane must be on jacks during the adjustment and the functional test of the cable. The shock strut for the right main gear must be in the fully extended position.
 TASK 27-62-61-825-001
 2.  Ground Spoiler Interlock Valve Adjustment (Fig. 501)_________________________________________
 A.  Special Tools and Equipment
 (1)  Rig Pin (S/B-3) - 0.311 +0.000/-0.002 inch diameter, 6.70 +/-0.25 inches long (MS70207-11)
 NOTE: The rig pin is a part of the kit F70207-69, -78, or -83.
____
 B.  References
 (1)  
07-11-11/201, Jack Airplane

 (2)  
27-62-51/501, Ground Spoiler Interlock Valve Cable

 C.  
Access

 (1)  
Location Zone
 217 Right Main Wheel Well

 D.  
Procedure

 S 585-002
 (1)  
Lift the airplane with the jacks until the right main gear shock strut is fully extended (Ref 07-11-11/201).

 S 485-003

 (2)  
Make sure you can easily install the rig pin S/B-3 through the yoke of the interlock valve.

 S 825-004

 (3)  
If you cannot easily install the rig pin, adjust the speed brake interlock valve cable (Ref 27-62-51/501).

 (4)  
Remove the rig pin S/B-3.

 (5)
Do the functional test of the ground spoiler interlock valve.

 S 585-007

 (6)  
Lower the airplane and remove the jacks from the airplane (Ref 07-11-11/201).

 S 085-005
 S 725-006
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-62-61
 ALL  ú ú 01 Page 501 ú Jul 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SEE A
FWD
VALVE CABLE INTERLOCK  RIG PIN S/B-3 
INTERLOCK VALVE GROUND SPOILER  FWD 
A 
Figure 501 Ground Spoiler Interlock Valve Adjustment 

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-62-61
 ALL  ú ú 01 Page 502 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 TASK 27-62-61-725-008
 3.  Ground Spoiler Interlock Valve Functional Test______________________________________________
 A. References
 (1)  
07-11-11/201, Jack Airplane

 (2)  
07-11-31/201, Jack Airplane Axles

 (3)  
12-15-31/301, Main Landing Gear Shock Strut

 (4)  
24-22-00/201, Manual Control

 (5)  
27-62-00/201, Speed Brake Control System

 B.
Access

 (1)  
Location Zone
 217 Right Main Wheel Well

 C.
Prepare for the Functional Test

 S 585-009
 (1)  
Lift the airplane with the jacks until the right main gear shock strut is fully extended (Ref 07-11-11/201).

 S 865-010

 (2)  
Supply the electrical power (Ref 24-22-00/201).

 S 865-011

 (3)
Supply the system A hydraulic power (Ref 27-62-00/201).

 D.
Do the Functional Test

 S 865-012
 (1)  
Move the speed brake lever to the UP position.

 (a)  
Make sure the ground spoilers do not move.

 S 865-013
 (2)  Release the air pressure in the shock strut for the right main landing gear.
 S 485-014
 CAUTION:_______LIFT THE AXLE AT THE JACK PAD ON THE AXLE ONLY. IF NOT, YOU WILL CAUSE DAMAGE TO THE AXLE.
 (3)  
Install the jack below the jack pad on the right main gear axle (Ref 07-11-31/201).

 S 725-015

 (4)  
Slowly lift the axle to compress the shock strut until the ground spoiler interlock valve opens.

 (a)  
Make sure the ground spoilers move to the fully extended position.

 (b)  
　
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