9-90 FLIGHT CONTROLS / YAW CONTROLS
ICON A5 / MAINTENANCE MANUAL CHANGE C3
Aircraft System
06—Flight Controls
Consumables
LOCTITE
®
243™
1. Remove AFT Tail Access Panel, Water Rudder Access Panel, and AFT Bulkhead Baggage
Panel.(See “Removal and Installation of Inspection Panels and Fairings” on page 3-34.) (See
“Baggage Floor Removal” on page 3-41.)
2. Check cable tension. (See “Inspect Yaw Cable Tension” on page 9-80.)
3. Remove left hand and right hand FWD and Main Cockpit Floor Bards. (See “Cockpit Floor Board
Removal” on page 3-46.)
4. Remove Seat Back and Seat Pan. (See “Seat Back Removal” on page 3-50.)(See “Seat Pan
Removal” on page 3-52.) Retain all fastening hardware.
5. Remove Baggage Floor Boards. (See “Baggage Floor Removal” on page 3-41.) Retain all
fastening hardware.
6. Remove Seatbelt Reel Cover, left hand and right hand baggage sidewalls, and baggage head-
liner. (See “Seat Belt Inertia Reel Removal” on page 3-39.)(See “Baggage Sidewall Panel
Removal” on page 3-43.)(See “Headliner Removal” on page 3-37.)
7. (Optional) Remove fuel tank if needed. (See “Remove Fuel Bladder (MY17 Only)” on page 10-11.
or See “Remove Fuel Tank (MY18+)” on page 10-15.) Retain all fastening hardware.
8. Remove Center Console Bucket and Throttle Bezel. (See “Center Console Bucket Removal” on
page 8-5.)(See “Throttle Handle and Bezel Removal” on page 8-10.) Retain all fastening hard-
ware.
9. Inspect all components within the rudder circuit for excessive wear. Any components that show
excessive wear or damage must be replaced with new components.
10. Disconnect rudder return spring by removing the FWD bolt. Retain hardware. See Figure 9-55.
VS-50-S16 RETAINING RING, PLAIN EXTERNAL, LIGHT DUTY, 316SS,
.500X.022
4
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