FLIGHT CONTROLS / PITCH CONTROLS 9-51
CHANGE C3 ICON A5 / MAINTENANCE MANUAL
22. Check the FWD and AFT pitch secondary stop:
a. Apply 16±2 lb at the center of the control stick grip. Force should be applied FWD and AFT.
b. Verify that contact is made with the secondary pitch stops (located in the vertical tail) at
the specified force.
c. Verifying that the primary pitch stops (located in vertical tail) contacts prior to the
secondary stops. See Figure 9-38.
23. Adjust the bolt on the secondary stops as needed to achieve contact when specified force is
applied. See Figure 9-38. If the secondary stops get contacted before the primary stops, not
achieving the elevator travel limits, it is acceptable to remove the bolt on the bottom secondary
stop.
FIGURE 9-38
SECONDARY STOPS LOCATION
24. Once the requirements for the upward and downward deflections have been met, install the
hardware to connect the pushrod to the elevator control horn. Torque the pushrod jam nut to 60
inlbs. Torque the bolt to 20 inlbs.
25. Ensure that there is no rubbing, binding, or any signs of interference while the elevator is moved
throughout its entire range of motion.
26. Install Horizontal Tail. (See “Horizontal Tail Installation” on page 12-13.)
27. Install center console bucket and throttle bezel. (See “Center Console Bucket Installation” on
page 8-8.)(See “Throttle Handle and Bezel Installation” on page 8-13.)
28. Install fuel tank. (See “Install Fuel Bladder (MY17 Only)” on page 10-12.)
29. Install baggage floor boards. (See “Baggage Floor Installation” on page 3-42.)
30. Install seat back and seat pan. (See “Seat Back Installation” on page 3-51.) (See “Seat Pan Instal-
lation” on page 3-53.)
31. Install left hand and right hand forward and main cockpit floor boards. (See “Cockpit Floor Board
Installation” on page 3-47.)
VERIFICATION METHOD:
Conduct the Check Elevator Rigging Procedure to verify proper rigging. (See “Inspect Pitch Rigging”
on page 9-44.)
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