(b)  
Tighten the bolt to 95-110 pound-inches.

 (c)  
Install the cotter pin.

 (d)  
Connect the input control rod to the quadrant with the nut, bolt and washer.

 (e)  
Install the cotter pin.

 (f)  
Attach the cables to the quadrant.

 (g)  
Install the cotter pins.

 S 864-009
 WARNING:  MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
_______ SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS, ELEVATORS, FLAPS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (2)  Do this task: "Hydraulic System Pressurization" (Ref 29-11-00/201).
 NOTE: No. 1 or 3 hydraulic systems supply the left control package.
____ No. 2 or 4 hydraulic systems supply the right control package.
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 (3)  S 864-010Do this task:  "Supply Electrical Power" (Ref 24-22-00/201).
 (4)  S 834-011Adjust the aileron control and trim system: (a) Manually move the captain's and the first officer's control wheels to the neutral position. (b) Operate the trim system switches and move the control wheel until you can easily install rig pin A/S-2 (Fig. 401).
 NOTE:____ Rig pin A/S-2 must stay in its hole to keep the trim system at the center for the subsequent adjustment.
 (c) (d) (e) (f) (g) (h) (i) (j)  With a clamp, attach the control wheel straightedge across the thumbrests on the captain's and first officer's control wheels.Make sure you can easily install rig pin A/S-6 (A/S-7 right).Tighten the cables to the specified tension range (Fig. 401).Make sure you can easily install rig pin A/S-8 (A/S-9 right).Install the clip locks on the turnbuckles.Remove all the rig pins.Align the inboard aileron rigging straightedge to the centerline of the inboard primary hinge.Make sure the inboard aileron aligns with the trailing edge.
 NOTE:____ The permitted tolerance is less than 0.25 inch.
 (k)  1) If the inboard aileron does not align with the trailing edge, adjust the input control rod.Remove the straightedges from the wing and the control wheels.
 (5)  S 714-018Turn the captain's control wheel full left and then full right. (a) Make sure the aileron moves through full travel in each direction.
 (6)  S 224-013Make sure the inboard aileron is not out of tolerance.

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747-400 MAINTENANCE MANUAL
 E. Put the Airplane Back to its Usual Condition
 S 094-014
 WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASK BELOW TO REMOVE THE
_______ DOOR LOCKS FROM THE LANDING GEAR DOORS. THE DOORS CAN CLOSE QUICKLY IF YOU DO NOT REMOVE THE DOOR LOCKS CORRECTLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (1)  
Do this task: "Removal of the Door Locks from the Wing Landing Gear" (Ref 32-00-30/201).

 S 864-015

 (2)  
Do this task: "Hydraulic System Depressurization"
 (Ref 29-11-00/201).

 S 864-016

 (3)  
Do this task: "Electrical Power Removal" (Ref 24-22-00/201).

 (4)  
Close all the access panels.

 S 414-017
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747-400 MAINTENANCE MANUAL
 INBOARD AILERON POWER CONTROL PACKAGE -
_____________________________________ MAINTENANCE PRACTICES
　
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