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yoke.
S Remove the old cable aft.
S Cut the eye-end from the turnbuckle.
Refer to Figure 4.
(3) Remove the cable between the turnbuckle and
the rudder:
S Remove the nut, washer, bolt, bush and
spacer that attach the cable to the rudder
lower mounting-bracket.
S Cut the eye-end from the old cable at the
rudder end.
S Remove the old cable forward.
S Cut the eye-end from the turnbuckle.
AIRCRAFT
DA 40 Series
AMM
Flight Controls
Doc # 6.02.01
Rev. 5 27-20-00 Page 209
20 Sep 2007
E. Install the Fuselage Rudder Control Cables (from the Yoke to the Rudder)
Detail Steps/Work Items Key Items/References
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: Install eye-ends in accordance with FAA AC 43.13-1B, Chapter 7, Section 8.
Note: To make the work easier, install an eye-end on one end of each cable before
you install them in the airplane.
(1) Install a new eye-end to the front cable at the
yoke end before you install it in the airplane.
S Inspect the cable eye-end for correct
assembly.
S If necessary for your airworthiness authority,
send a sample for proof test.
Use Locoloc thimbles and Nico-Press
clamps for 3.2 mm (1/8 inch) diameter
steel cables to specification LN9374.
Inspect cable swage with go-no-go
gauge for 1/8 inch Nicopress oval
sleeve in accordance with FAA AC
43.13-1B, Chapter 7, Section 8.
(2) Push the control cable through the Teflon tube
from the front.
Refer to Figure 4.
Through the front and rear main
bulkheads.
(3) Install a new eye-end to the cable at the
turnbuckle end.
S Inspect the cable eye-end for correct
assembly.
S If necessary for your airworthiness authority,
send a sample for proof test.
Use Locoloc thimbles and Nico-Press
clamps for 3.2 mm (1/8 inch) diameter
steel cables to specification LN9374.
Inspect cable swage with go-no-go
gauge for 1/8 inch Nicopress oval
sleeve in accordance with FAA AC
43.13-1B, Chapter 7, Section 8.
(4) Install a new eye-end to the rear cable before you
install it in the airplane.
S Inspect the cable eye-end for correct
assembly.
S If necessary for your airworthiness authority,
send a sample for proof test.
Use Locoloc thimbles and Nico-Press
clamps for 3.2 mm (1/8 inch) diameter
steel cables to specification LN9374.
Inspect cable swage with go-no-go
gauge for 1/8 inch Nicopress oval
sleeve in accordance with FAA AC
43.13-1B, Chapter 7, Section 8.
AIRCRAFT
Flight Controls DA 40 Series
AMM
Detail Steps/Work Items Key Items/References
Page 210
20 Sep 2007 27-20-00 Doc # 6.02.01
Rev. 5
(5) Push the control cable through the Teflon tubes
from the front.
From the baggage frame to the rudder.
(6) Install a new eye-end to the cable at the rudder
end.
S Inspect the cable eye-end for correct
assembly.
S If necessary for your airworthiness authority,
send a sample for proof test.
Use Locoloc thimbles and Nico-Press
clamps for 3.2 mm (1/8 inch) diameter
steel cables to specification LN9374.
Inspect cable swage with go-no-go
gauge for 1/8 inch Nicopress oval
sleeve in accordance with FAA AC
43.13-1B, Chapter 7, Section 8.
(7) Install the cable to the rudder lower mountingbracket:
S Install the bolt, bush and spacer that attach
the cable to the rudder.
S Install a washer and self-locking nut.
Refer to Figure 4.
Torque to 6.4 Nm (4.7 ft.lb). Use a new
self-locking nut.
(8) Install the cable to the yoke:
S Install the bolt, bush and spacer that attach
the cable to the yoke.
S Install a washer and self-locking nut.
Refer to Figure 4.
Torque to 6.4 Nm (4.7 ft.lb). Use a new
self-locking nut.
(9) Adjust both left and right rudder cable
turnbuckles to give the correct tension.
Refer to Paragraph 3.
(10) Do a test for the correct range of rudder
movement.
Refer to Paragraph 2.
(11) Do an inspection of all the controls that you have
adjusted.
S If necessary for your airworthiness authority,
do a second inspection of the controls.
(12) Install these items:
S The pilots’ seats.
S The passenger seat.
Refer to Section 25-10.
AIRCRAFT
DA 40 Series
AMM
Flight Controls
Doc # 6.02.01
Rev. 5 27-20-00 Page 211
20 Sep 2007
5. Rudder Control Cable and Yoke Access
　
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