AIRCRAFT
Auto Flight
DA 42 NG AMM
Page 222
15 Mar 2018
22-10-00
Doc # 7.02.15
Rev. 4
14. Slip Clutch Override Procedure
Detail Steps/Work Items
Key Items/References
(1)
Lift the airplane on jacks.
Refer to Section 07-10.
(2)
With the autopilot disengaged, check freedom
of control movement in all control axes,
including pitch trim.
(3)
Power up the Garmin G1000 in Configuration
Mode.
Refer to G1000 System Maintenance
Manual, latest revision.
(4)
Navigate to the second of the GFC pages.
(5)
Engage the pitch servo:
S
Select the ENG CLCH soft-key.
S
Set the DRIVE SERVO speed to zero.
S
Select the DRV SRVO soft-key.
(6)
Manually override the servo actuator slip clutch
by moving the control stick forward and back
through its range of motion.
The control should move with some
resistance through its range of motion.
(7)
Verify the servo motor does not turn by viewing
the SPEED in the SERVO DATA area of the
screen.
The motor of the servo actuator should
remain stationary.
(8)
Disengage the pitch servo:
S
Select the STP SRVO soft-key.
S
Select the DIS CLCH soft-key.
Verify freedom of movement of the pitch
axis.
(9)
Repeat steps 5 to 8 for each axis including pitch
trim.
Summary of Contents for DA 42 NG
Page 933: ...AIRCRAFT DA 42 NG AMM Fuel Doc 7 02 15 Rev 4 28 TITLE Page 1 15 Mar 2018 CHAPTER 28 FUEL ...
Page 1459: ...AIRCRAFT DA 42 NG AMM Lights Doc 7 02 15 Rev 4 33 TITLE Page 1 15 Mar 2018 CHAPTER 33 LIGHTS ...
Page 1711: ...AIRCRAFT DA 42 NG AMM Doors Doc 7 02 15 Rev 4 52 TITLE Page 1 15 Mar 2018 CHAPTER 52 DOORS ...
Page 1853: ...AIRCRAFT DA 42 NG AMM Wings Doc 7 02 15 Rev 4 57 TITLE Page 1 15 Mar 2018 CHAPTER 57 WINGS ...
Page 2071: ...AIRCRAFT DA 42 NG AMM Engine Doc 7 02 15 Rev 4 72 TITLE Page 1 15 Mar 2018 CHAPTER 72 ENGINE ...
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