(2)  
Place washer and nut on bolt. Tighten nut 240 to 350 pound-inches.

(3)  
Install cotter pin.

D.  Install inboard and outboard hinge bolts.
(1)  
Position spacer on both sides of bearing.

NOTE: Ensure that flanged bushings are installed in structure.

(2)  
Position bearing to align with clevis and install bolts with heads as shown in Fig. 401.

(3)  
Place washer and nut on bolt. Tighten nut 100 to 140 pound-inches.

(4)  
Install cotter pin.

E.  Connect bonding jumpers to spoiler. Jumpers are attached at lower leg of leading channel adjacent to inboard and outboard hinges.
(1)  If hole is not provided for bonding jumper fastener, drill hole 3.5 inches in from end of panel and 0.5 inch aft of panel leading edge.
F.  Rotate spoiler through full travel and check for binding or interference.
501 
Jun 20/86  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  27-61-11 Page 403 

G.  Install bolt attaching spoiler actuator rod end to spoiler.
(1)  
Install bolt with head to the left.

(2)  
Secure bolt with washer and nut.

(3)  
Tighten nut to 240-350 pound-inches.

(4)  
Install cotter pin.

H.  Ensure that hydraulic systems A and B are not pressurized. Remove spoiler actuator lock.
I.  Provide system A and B hydraulic power (Ref 27-61-0).
J.  Place speed brake control lever in DOWN position to lower spoilers.
K.  Remove system A and B hydraulic power (Ref 27-61-0).
L.  Check that gap between spoiler and fixed wing structure is 0.40 +0.05 inch at end of spoiler panel. Gap is defined as metal-to-metal clearance.
M.  Check that gap between adjacent spoilers is 0.70 +0.10 inch.
N.  Adjust seals on adjacent spoiler to 0.000 +0.020/-0.000-inch gap.
O.  Ensure that seals between spoiler and fixed wing structure contact firmly.
P.  Adjust and test flight spoiler (Ref 27-61-11, Flight Spoilers - Adjustment/Test).
Q.  Remove electrical power if no longer required.
500 
27-61-11 Page 404  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  Aug 01/96 

FLIGHT SPOILERS - ADJUSTMENT/TEST
1.  Flight Spoiler Adjustment
A.  Equipment and Materials
(1)  
Corrosion Preventive Compound - MIL-C-11796, Class 3

(2)  
Sealant - BMS 5-95 (Ref 20-30-11)

B.  Prepare for Adjustment
(1)  
Provide electrical power.

(2)  
Provide system A and B hydraulic power (Ref 27-61-0 MP).

(3)  
Place speed brake control in UP position to raise spoilers.

(4)  
Place FLT CONTROLS A switch on forward overhead panel to ON to pressurize trailing edge flaps.

(5)  
Retract trailing edge flaps to full up position with jackscrew stops in contact.

(a)  
Place flap control lever in FLAP UP detent.

(b)  
Pull inboard on WFFA cable in wheel well until jackscrew stops contact.

(6)  
Place speed brake control lever in DOWN position to lower spoilers.

C.  Adjust Flight Spoiler
(1)  
Check that spoiler to flap clearance is 0.03 (+ 0.10/-0.00) inch measured at point of minimum clearance. Rotate captain's control wheel clockwise to ensure that flight spoilers No. 2 and 3 are full down, or counterclockwise to ensure that flight spoilers No. 6 and 7 are full down (Fig. 501).

(2)  
If spoiler to flap clearance is not within limits:

(a)  
Provide access to spoiler actuator by either lowering flaps or opening applicable hinged trailing edge panel or by placing speed brake control lever in UP position to raise spoilers. Depressurize hydraulic systems A and B (Ref 27-61-0 MP).

WARNING:  DO NOT PUT ANY PART OF BODY BETWEEN SPOILER AND WING UNLESS HYDRAULIC POWER IS REMOVED. SERIOUS INJURY CAN RESULT.

(b)  
Break lockwire and loosen checknut on actuator rod end.

(c)  
Disengage locking key from piston rod.

500 
Feb 01/95  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  27-61-11 Page 501 

A89648
Flight Spoiler Panel Adjustment  500 
27-61-11  Figure 501  Oct 20/92 
Page 502 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 
　
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