S 434-016

 (6)  
Attach the cables to the quadrant assembly and hold them with a cotter pin.

 S 434-015
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 (7)  S 434-017Tighten the cables.
 (8)  S 714-022Adjust and do a test of the control system (Ref 32-31-00/501).
 (9)  S 414-018Replace the left inboard panel on the floor.
 S 414-019

 (10) Install the seats.

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737-300/400/500MAINTENANCE MANUAL
 LANDING GEAR SELECTOR VALVE QUADRANT ASSEMBLY - INSPECTION/CHECK
________________________________________________________________
 1.  General_______
 A.  This data contains illustrations and wear limit charts. There is not a procedure in this data which tells you where the components are. You must go to the removal/installation procedure to find where the components are (AMM 32-31-61/401).
 TASK 32-31-61-226-001
 2.  Landing Gear Selector Valve Quadrant Assembly Wear Limits (Fig. 601)_________________________________________________________
 A.  General
 (1)  This data contains illustrations and wear limit charts. There is not a procedure in this data which tells you where the components are. You must go to the removal/installation procedure to find where the components are (AMM 32-31-61/401).
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A 737-300/400/500MAINTENANCE MANUAL
QUADRANT ASSEMBLY
SEE A
LGVA LGVB
CABLE 
RETAINING  QUADRANT 
COTTER  ASSEMBLY 
PIN  A  CONTROL 
SEALANT  CABLE 
WHEEL WELL CEILING  SUPPORT 

(EXAMPLE) BOLT MOUNTING 
A  CRANK 
SELECTOR VALVE  ACTUATING LINK  INBD 
A  FWD 
Landing Gear Selector Valve Control Quadrant Assembly Wear Limits Figure 601 (Sheet 1) 

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A-A

Landing Gear Selector Valve Control Quadrant Assembly Wear Limits
Figure 601 (Sheet 2)

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INDEX NO.  PART NAME  DIM.  DESIGN LIMITS  WEAR LIMITS  REPLACE PART WORN  REPAIR WORN PART  REPAIR INSTR. 
DIAMETER  MAX WEAR DIM.  DIAM CLEAR-ANCE MAX 
MIN  MAX 
1  BEARING  ID  0.9995  1.0000  1.0005  0.0005  X 
SHAFT  OD  1.0001  1.0004  0.9999  X 
2  BEARING  ID  0.9995  1.0000  1.0015  0.002  X 
　
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