737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 5(91)

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 the rod end to the torsion link. 8) Install the cotter pin on the nut. 9) Make sure the two rod ends align correctly. 10) Tighten the checknut on the lower rod end. 11) Attach the protective boot to the spacer with the clamp. 12) Remove the rig pin S/B-3. 13) Lower the airplane and remove the jacks (AMM 07-11-11/201).
 S 825-013
 (5)  
Adjust the clearance between the ground spoiler panels and the flap:

 (a)  
Supply the electrical power (AMM 24-22-00/201).

 (b)  
Supply the systems A and B hydraulic power (AMM 27-62-00/201).

 (c)  
Move the speed brake lever to the UP position to lift the spoilers.

 (d)  
Move the flap control lever to the UP position to fully retract the trailing edge flaps.

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

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SEE  A 
SEE  B  RIG PIN S/B-3 
FWD  INBD  CONTROL CABLE INTERLOCK VALVE  SEE  C 
INTERLOCK VALVE GROUND SPOILER 
VALVE CABLE INTERLOCK  A 
CLAMP  DIMENSION "B" 1.62 INCHES MINIMUM 
BOOT PROTECTIVE 
BOLT HOLE TO TORSION LINK) (LOWER ROD END SPACER CLAMP CHECKNUT  B  ROD END LOWER ADAPTER ROD END  INBD  MAIN GEAR OLEO PARTIALLY COMPRESSED INTERLOCK VALVE GROUND SPOILER C 
Figure 505 Ground Spoiler Interlock Valve 

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 (f)  Measure the clearance between the trailing edge of the spoiler
 panels and the flaps near the centerline of the spoiler
 actuators.
 (g)  Make sure the clearance between the spoilers No. 4 and 5 and
 the flaps is in the limits shown in Fig. 506.
 (h)  Make sure the clearance between the spoilers No. 0, 1, 8 and 9
 and the flaps is 0.03 +0.10/-0.00 inch
 (i)  Make sure there is a clearance between the trailing edge of the
 spoiler panels and the flaps for the full span of the spoiler.
 (j)  If the clearances between the spoiler panels and the flaps are
 not in the limits, adjust clearance:
 1) Make a record of the clearance.
 WARNING: DO NOT PUT A PART OF YOUR BODY BETWEEN THE SPOILER_______
 AND THE WING UNLESS YOU REMOVE THE HYDRAULIC POWER.
 THE SPOILERS CAN CAUSE INJURY TO PERSONS.
 2) Lift the spoiler or extend the flaps to get access to the
 spoiler actuator:
 a) Move the speed brake lever to the UP position to lift
 the spoilers.
 b) Move the flap control lever to the 40-unit detent to
 extend the flaps.
 c) Remove the system A and B hydraulic power
 (AMM 27-62-00/201).
 3) Loosen the checknut on the rod end of the actuator.
 4) Remove the locking key from the piston rod.

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500
MAINTENANCE MANUAL

ACTUATOR PISTON SPOILER TO GROUND
ROD END  FLAP CLEARANCE

AIRPLANE CONFIGURATION  CLEARANCE MEASURED AT OUTBOARD ACTUATOR CL (INCHES)  CLEARANCE MEASURED ACTUATOR CL AT INBOARD (INCHES) 
ON JACKS 3NO FUEL  0.03 +0.10/-0.00  0.03 +0.10/-0.00 
ON GEAR 4NO FUEL  0.03 +0.10/-0.00  0.08 +0.10/-0.00 
ON GEAR FULL FUEL 4  0.03 +0.10/-0.00  0.13 +0.10/-0.00 
　
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