ICON A5, Maintenance Manual

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LANDING GEAR / LANDING GEAR GENERAL MAINTENANCE 14-19
CHANGE C2 ICON A5 / MAINTENANCE MANUAL
CH
AP
TER 1
4
R
ELATED
I
NFORMATION
:
"Condition and 100-Hour Inspection—Landing Gear" on page 3-14
"Interval Maintenance—Calendar Intervals" on page 3-5
"Brake Line Replacement Procedure" on page 14-21
"Rudder Pedal Connector Lines Replacement" on page 14-21
"Forward Lines Replacement" on page 14-23
"Aft Lines Replacement" on page 14-25
"Parking Brake Valve Replacement Procedure" on page 14-32
14.4.2 Landing Gear Actuator Limit Switch Adjustment Procedure
There is one limit switch adjustment rod on each actuator that regulates the extension limit and the
retraction limit. Use this procedure to adjust the limit switch on the desired actuator.
T
ASK
I
NFORMATION
:
Type of Maintenance
Line
Level of Certification
LSA-RM
Task Specific Training Required
No
Special Tools Required
None
Parts Required
None
Aircraft System and Number
11—Landing Gear
Consumables
None
T
ASK
I
NSTRUCTIONS
:
1. Unless already performed, remove any interior panels needed to gain access to the actuator.
(See “Right Instrument Panel Top Panel Removal” on page 8-17.)(See “Removal and Installation
of Inspection Panels and Fairings” on page 3-34.)
2. Jack the aircraft so that the landing gear is clear of the ground. (See “Empty Weight and CG
Measurement While on Jackpoint Scales” on page 3-32.)
3. Use a 1/4” open-end wrench to loosen the jam nut tightened against the limit switch adjustment
saddle for the affected switch.
4. Use the thumb wheel to set the affected switch to the desired position.
5. Torque the jam nut to 36-40 in-lb
f
to secure the position of the limit switch.
6. Power up the aircraft, and actuate the landing gear to verify adjustment.