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 jumper, drill a hole in the lower part of the spoiler panel near the hinge fittings. a) Drill the hole 3.5 inches from the end of the spoiler
 panel, 0.5 inch aft of the leading edge. 3) Use the milliohmmeter to make sure the resistance of the bonding jumper connection is less than 0.010 ohms.
 S 714-014
 (5)  
Move the spoiler through its full travel.

 (a)  
Make sure the spoiler panel moves freely.

 S 034-015
 (6)  
Connect the adjustable rod for the spoiler position transmitter to the spoiler (Ref 22-11-27/401).

 S 034-016

 (7)  
Install the bolt that attaches the rod end for the spoiler actuator to the spoiler panel:

 (a)  
Apply a layer of BMS 3-24 grease to the bolt.

 (b)  
Install the bolt with its head left.

 (c)  
Install the washers and the nut on the bolt.

 (d)  
Tighten the nut to 350-400 pound-inches.

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 (e) (f)  Install the cotter pin.Apply BMS 3-24 grease to the bolt, washer, nut and cotter pin.
 (8)  S 864-017Make sure the hydraulic power is not on.
 (9)  S 094-018Remove the spoiler ground locks.
 S 864-019

 (10)
 Supply the systems A and B hydraulic power (Ref 27-61-00/201).

 S 864-020

 (11)
 Move the speed brake lever to the DOWN position to lower the spoilers.

 S 864-021

 (12)
 Remove the systems A and B hydraulic power (Ref 27-61-00/201).

 S 224-022

 (13)
 Make sure the clearance between the spoiler panel and the wing structure is 0.40 |0.05 inch at the aft end of the spoiler panel.

 NOTE: The clearance is specified as the distance between the metal
____ surfaces.
 S 224-024
 (14) Make sure the clearance between the adjacent spoilers is
 0.70 |0.10 inch.
 S 224-025
 (15) Make sure the clearance between the seals on the adjacent spoiler is
 0.000 to 0.020 inch.
 S 214-026
 (16)
 Make sure the seals between the spoiler and the wing structure touch tightly.

 (17)
 Do the flight spoiler adjustment (Ref 27-61-11/501).

 S 824-027
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 S 724-028
 (18)
 Do the functional test of the flight spoiler (Ref 27-61-11/501).

 S 864-029

 (19)
 Remove the electrical power (Ref 24-22-00/201)

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 FLIGHT SPOILER - ADJUSTMENT/TEST
________________________________
 1.  General_______
 A.  There are two tasks in this procedure. There are tasks for the
 adjustment and functional test of the flight spoilers.

 TASK 27-61-11-825-001
 2.  Flight Spoiler Adjustment (Fig. 501)_________________________
 A.  Consumable Materials
 (1)  
A00247 Sealant BMS 5-95

 (2)  
B00365 Solvent - Methyl-Ethyl-Ketone TT-M-261

 (3)  
C00308 Compound - Corrosion Preventive, MIL-C-11796, Class 3

 B.  
References

 (1)  
24-22-00/201, Manual Control

 (2)  
27-61-00/201, Spoiler Control System
　
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