FORCE
ROD END
LIMITER ROD SLEEVE
1.58 INCHES
1.68 INCHES MAXIMUM DIMENSIONS
FORCE LIMITER ROD VERNIER ADJUSTMENT
1
INSTALLED IN THE LEFT WHEEL WELL A 2
INSTALLED IN THE RIGHT WHEEL WELL
Wheel Well Control Linkage Figure 503
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MAINTENANCE MANUAL
OUTBOARD
AILERON OUTBOARD AILER0N
POWER CONTROL PACKAGE
AND LOCKOUT MECHANISM INBOARD
SEE A AILERON
INBOARD AILERON
POWER CONTROL PACKAGE
SEE B
POWER CONTROL OUTBOARD AILERON TORQUE LEFT WING SHOWN
PACKAGE ACTUATOR DRIVE (RIGHT WING OPPOSITE)
LINKAGE (REF)
LEFT OR RIGHT OUTBOARD AILERON LOCKOUT ACTUATOR
OUTBOARD AILERON QUADRANT
OUTBOARD OUTPUTAILERON LINKAGE (REF) RIG PIN A/S-8POWER CONTROL PACKAGE INPUT OUTBOARD INBOARD AILERON
LINKAGE (REF) AILERON
QUADRANT LOCKOUT MECHANISM INPUT ROD
OUTBOARD AILERON CONTROL PACKAGE VERTICAL
AND LOCKOUT MECHANISM
REACTION LINK
A
INBOARD POWER CONTROL PACKAGE ACTUATOR
INBOARD AILERON
WING STRUCTURE (REF)
HORIZONTAL REACTION LINK
INBOARD AILERON POWER CONTROL PACKAGE
B
Aileron Power Control Package Figure 504
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MEASURED FROM INBOARD TRAILING EDGE OF OUTBOARD AILERON TO TRAILING EDGE OF ADJACENT FIXED STRUCTURE
MEASURED FROM INBOARD TRAILING EDGE ON INBOARD AILERON TO OUTBOARD TRAILING EDGE OF INBOARD FLAP ADD OR SUBTRACT NEUTRAL READING, AS APPLICABLE, TO GET TOTAL AILERON TRAVEL FROM NEUTRAL
|0.05 INCH FOR RIGGING ADJUSTMENT AT NEUTRAL, |0.25 INCH FOR SYSTEM TEST AT NEUTRAL
Aileron Deflection and Rigged Neutral Position
Figure 505
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(b)
Turn the control wheel manually to make sure the system is in the center of the trim detent (when the control wheels turn, to get 44-50 degrees).
(c)
Move the trim switches to RIGHT WING DOWN and hold the switches until the movement of the control wheels stops. 1) Make sure the control wheels turn clockwise 44 to 50
degrees. 2) Make sure the right inboard aileron moves up and the left inboard aileron moves down.
(d)
Turn the control wheel manually to make sure the system is in the center of the trim detent (when the control wheels turn, to get 44-50 degrees).
(e)
Put the aileron trim system back to the neutral position.
S 715-013
(2)
Do a test of the inboard aileron operation:
