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(2) Remove the cable between the firewall and
the yoke:
− Remove the cotter pin and clevis pin that
attaches the cable to the bracket at the
firewall.
− Remove the bolt that attaches the cable
to the yoke.
− Cut the eye end from the old cable at the
firewall end.
− Remove the old cable.
Flight Controls
DA20-C1 AMM
Page 206
19 Dec 1997 27-20-00 Doc # DA201-C1
Rev. 0
C. Install the Rudder Control Cables (From the firewall to the yoke).
Detail Steps/Work Items Key Items
WARNING: ONLY TRAINED AND AUTHORIZED PERSONS SHOULD INSTALL
CABLE EYE-ENDS. IF THE EYE ENDS ARE NOT INSTALLED
CORRECTLY, THE RUDDER CONTROLS CAN FAIL. THIS CAN
CAUSE DEATH OR INJURY TO PERSONNEL.
Note: To make the work easier, swage an eye end on one end of the cable before
you install it in the airplane.
(1) Install a new eye end to the cable before you
install it in the airplane.
− Inspect the cable eye-end for correct
assembly.
− If necessary for your airworthiness
authority, send a sample for proof test.
Use Locoloc thimbles and oval sleeves for
3.2 mm diameter steel cables to
specification MS 51844.
(2) Push the control cable through the teflon
tubes from the rear.
Refer to Fig: 1.
(3) Make sure the cable is in the correct position
on the pulleys (for the outer cables only).
Refer to Fig: 1.
(4) Push the cable position through the “S” tube
on the rudder pedal assembly.
Refer to Fig: 1.
(5) Install a new eye end to the cable at the
firewall end.
− Inspect the cable eye end for correct
assembly.
− If necessary for your airworthiness
authority, send a sample for proof test.
Use Locoloc thimbles and oval sleeves for
3.2 mm diameter steel cables to
specification MS 51844.
(6) Install the cable to the yoke:
− Install the bolt that attaches the cable to
the yoke.
− Tighten the bolt.
Torque to 6.5 Nm (4.6 ft.lb).
DA20-C1 AMM
Flight Controls
Doc # DA201-C1
Rev. 0 27-20-00 Page 207
19 Dec 1997
Detail Steps/Work Items Key Items
(7) Install the cable to the bracket at the firewall:
− Install the clevis pin that attaches the
cable to the firewall bracket.
− Install the cotter pin.
Adjust the position of the clevis pin in the
multi-hole bracket to give the correct
rudder pedal position. The rudder pedal
lever must be vertical when the rudder is
neutral.
(8) Do a check of the rudder range of
movement.
Refer to the Rudder Control System Test
For Correct Range Of Movement.
(9) Do an inspection of all the controls that you
have adjusted.
− If necessary for your airworthiness
authority, do a second inspection of the
controls.
(10) Install these items:
− Pilots seats.
− Baggage compartment floor.
− Fuel Tank.
Refer to Chapters:
− 25-10
− 25-10
− 28-10
Flight Controls
DA20-C1 AMM
Page 208
29 Apr 2004 27-20-00 Doc # DA201-C1
Rev. 9
D. Remove The Aft Fuselage Rudder Control Cables (From the yoke to the rudder).
Detail Steps/Work Items Key Items
(1) Remove these items for access:
− Pilots seats.
− Baggage compartment floor.
− Fuel Tank.
− Rudder.
Refer to Chapters:
− 25-10.
− 25-10.
− 28-10.
− 55-40.
(2) Remove the cable between the rudder yoke
and the rudder:
− Remove the bolt that attaches the
turnbuckle to the rudder yoke.
− Remove the bolt that attaches the cable
to the rudder lower mounting bracket.
− Cut the eye end from the old cable at the
rudder lower bracket end.
− Remove the old cable.
− Cut the eye end from the turnbuckle.
E. Install The Aft Fuselage Rudder Control Cables (From the yoke to the rudder).
Detail Steps/Work Items Key Items
WARNING: ONLY TRAINED AND AUTHORIZED PERSONS SHOULD INSTALL
CABLE EYE-ENDS. IF THE EYE ENDS ARE NOT INSTALLED
CORRECTLY, THE RUDDER CONTROLS CAN FAIL. THIS CAN
CAUSE DEATH OR INJURY TO PERSONNEL.
Note: To make the work easier swage an eye end on one end of the cable before
you install it in the airplane.
(1) Install a new eye end to the cable through
the turnbuckle before you install the cable in
the airplane.
− Do a test of the cable eye end for correct
assembly.
− If necessary for your airworthiness
authority, send a sample for proof test.
　
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