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AMM

D. Remove the Fuselage Rudder Control Cables (from the Yoke to the Rudder)
DA 40 Series

Detail Steps/Work Items  Key Items/References 
(1)  Remove these items for access: S The pilots’ seats. S The passenger seat.  Refer to Section 25-10. 
(2)  Remove the cable between the yoke and the turnbuckle: S Remove the nut, washer, bolt, bush and spacer that attach the cable to the yoke. S Cut the eye-end from the old cable at the 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. 

Page 208 Doc # 6.02.01 09 Jan 2003 Rev. 4
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Flight Controls
AMM

E. Install the Fuselage Rudder Control Cables (from the Yoke to the Rudder)
DA 40 Series

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. 

Doc # 6.02.01 Page 209
Rev. 4 09 Jan 2003

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AMM

DA 40 Series

Detail Steps/Work Items  Key Items/References 
(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 mounting-bracket: 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. 
　
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