FLIGHT CONTROLS / FLAP CONTROLS 9-69
CHANGE C3 ICON A5 / MAINTENANCE MANUAL
Aircraft System and Number
06—Flight Controls
Consumables
Powder-Free Nitrile Gloves
Powder-Free Latex Gloves
Isopropyl Alcohol
Anticorrosion/Lubricant/Tef-Gel
Torque Seal
1. Remove AFT baggage panel to gain access to the flap actuator. (See “Removal and Installation
of Inspection Panels and Fairings” on page 3-34.)
2. Clean the noted damage area as required in accordance with ICA010822, Section 10.1.
WARNING: Wear safety glasses when installing helicoils.Figure 9-43 shows
parts outside the aircraft, inside the aircraft installation orientation
might be different for accessibility.
3. Flap System Rigging Process. See Figure 9-43.
a. Set wings to the folded configuration per POH wing fold operation.
b. Adjust fuselage flap pin to achieve .200+.030/-.000 protrusion from the pin housing while
the actuator is extended to the 0° actuator stop.
NOTE: Push cable range of motion exceeds the required range of motion
of the push pins, but in some cases the push cable position must be
adjusted in the fuselage to avoid running out of push cable travel in
one direction. Push cable position can be changed by loosening all
jam nuts and running the bellcrank rod end and cable socket in or
out equally.
LOCTITE 243 THREAD LOCKER, LOCTITE
243, 10ml bottle
AS NEEDED
ICA012078 LUBRICANT, GENERAL
PURPOSE
AS NEEDED
ICA012079 INSPECTORS LACQUER,
ANTI-SABOTAGE, ORANGE
AS NEEDED
Part Number Part Name Quantity
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