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Page 8-10 LMM for the Kodiak 100
190-02102-00 Rev.4
This procedure will only work correctly if both are selected. False readings
may be given otherwise. During the next two steps, the softkeys DIS CLCH
and STP SRVO should be showing - do not select them yet.
7. Override the servo actuator slip clutch for the engaged axis by moving the control
yoke through its range of motion. The controls should move, with some resis-
tance, through their range of motion.
It is not necessary to move each trim control through its full range of
motion; it should be moved sufficiently both directions to find the slip clutch
of the servo actuator is being overridden.
8. While moving the control yoke, be sure the servo motor does not turn by viewing
the SPEED (speed of motor) in the SERVO DATA box as you override the slip
clutch.
The motor of the servo actuator should remain stationary as the slip clutch
slips.
9. Disengage the servo actuator by selecting DIS CLCH and STP SRVO and check
for freedom of movement of controls. The resistance to movement from the
autopilot actuator slip clutch should not be present
10. Repeat for each control axis (roll, yaw, pitch and pitch trim).
8.16 GFC 700 Visual Inspection Procedure
Refer to the Kodiak 100 AMM.
8.17 Flight Stream 510 Wireless Transceiver Periodic Maintenance
There are no periodic maintenance requirements.
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