5
0.0050
0.0070
6
(0.178)
7
0.0030 (0.0762)
0.0050
8
(0.127)
0.0150
9
(0.381)
0.0395
10
(1.003)
PART WORN REPLACE PART WORN REPAIR INSTR REPAIR
X
X X 3
4
X
X
X
X X 5
X X 4
X X 6
X X 4
X X 4
X X 4
X
Inboard Flight Spoiler Quadrant Installation
Figure 201 (Sheet 4)
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A
747-400
MAINTENANCE MANUAL
RIG PIN HOLE
PLATE
BACR15BB6B RIG PIN SHEAR RIVET
QUADRANT
ALUMINUM FOIL MARKER ALUMINUM FOIL MARKER
Inboard Flight Spoiler Quadrant Installation
Figure 201 (Sheet 5)
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A
747-400 MAINTENANCE MANUAL
TASK 27-61-06-402-011
3. Inboard Flight Spoiler Quadrant Installation (Fig. 201)____________________________________________
A. Special Tools and Equipment
(1)
G12001-50 Rig Pin Kit
B.
References
(1)
24-22-00/201, Manual Control
(2)
29-11-00/201, Main Hydraulic Supply System
C.
Access
(1)
Location Zone
135 Left Wing Landing Gear Wheel Well
136 Right Wing Landing Gear Wheel Well
575 Spoiler No. 5
675 Spoiler No. 8
(2)
Access Panel
572FB Access Panel - Trailing Edge Lower, LH
672FB Access Panel - Trailing Edge Lower, RH
D.
Procedure
S 422-012
(1)
Attach the quadrant to the mounting bracket:
(a)
Install the bolt, spacer, washer and nut.
(b)
Install the cotter pin.
S 432-013
(2)
Connect the cables to the quadrant and install the cotter pins to hold the cables.
S 432-014
(3)
Connect the input arm rod to the quadrant lever.
(a)
Install the cotter pin.
S 432-015
(4)
Connect the ratio changer linkage to the mounting bracket and the actuator.
(a)
Install the cotter pins.
S 862-016
(5)
Do this task to pressurize hydraulic system No. 4: "Hydraulic System Pressurization" (Ref 29-11-00/201).
(6)
Do this task: "Supply Electrical Power" (Ref 24-22-00/201).
S 832-018
(7)
Adjust the control cables:
(a)
Turn the captain's control wheel to manually adjust the aileron system until you can install rig pin A/S-4 (A/S-5, right).
S 862-017
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(b)
Install the rig pin A/S-19 (A/S-21, right) in the inboard flight spoiler quadrant.
(c)
Tighten the control cables to the tension shown in Fig. 201. 1) Make sure the rig pins move freely.
(d)
Install the lock clips on the turnbuckle.
(e)
Remove the rig pins.
S 712-019
(8)
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