FLIGHT CONTROLS / ROLL CONTROLS 9-17
CHANGE C3 ICON A5 / MAINTENANCE MANUAL
RELATED INFORMATION:
"Condition and 100-Hour Inspection—Forward Fuselage and Hull" on page 3-16
"Rigging Roll Controls" on page 9-20
"Cockpit Floor Board Removal" on page 3-46
"Cockpit Floor Board Installation" on page 3-47
"Seat Back Removal" on page 3-50
"Seat Back Installation" on page 3-51
"Seat Pan Removal" on page 3-52
"Seat Pan Installation" on page 3-53
"Baggage Floor Removal" on page 3-41
"Baggage Floor Installation" on page 3-42
"Seat Belt Inertia Reel Removal" on page 3-39
"Seat Belt Inertia Reel Installation" on page 3-40
"Baggage Sidewall Panel Removal" on page 3-43
"Baggage Sidewall Panel Installation" on page 3-45
"Headliner Removal" on page 3-37
"Headliner Installation" on page 3-38
"Inspect Roll Rigging" on page 9-17
"Removal and Installation of Inspection Panels and Fairings" on page 3-34
"Cockpit Panels Removal and Installation" on page 3-36
9.4.3.2 Inspect Roll Rigging
The following section contains the information required to perform a rigging check on the roll control
system.
TASK INFORMATION:
Type of Maintenance
Line
Level of Certification
LSA-RM
Task Specific Training Required
No
Special Tools Required
Digital level with 0.1° resolution and Alt Ref function, calibrated to manufacturers instructions
A second person will be required during the inspection processes.
Parts Required
None
Aircraft System and Number
14—Wing
Consumables
None
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