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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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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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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本文链接地址：737-300 400 500 AMM 飞机维护手册 起落架 LANDING GEAR 2(58)
