DA 40 Series

Detail Steps/Work Items  Key Items/References 
(9)  Do an inspection of the controls that you have adjusted. S If necessary for your airworthiness authority, do a second inspection of the controls. 
(10)  Install these items: S Pilots’ seats. S Passenger seat. S Push-rod access panels under the center section. S Aileron bellcrank access panels under each wing.  Refer to Section: 25-10 52-40 

4. Aileron Push-Rod Access
Aileron Push-Rod  Remove/Install Access  References 
Between the control stick and the bellcrank at the control bulkhead.  Pilots’ seats.  Refer to Section 25-10. 
Between the bellcrank at the control bulkhead and the idler lever at the front main bulkhead.  Pilots’ seats.  Refer to Section 25-10. 
Between the idler lever at the front main bulkhead and the bellcrank at the rear main bulkhead.  Pilots’ seats. Passenger seat.  Refer to Section 25-10. 
Between the bellcrank at the rear main bulkhead. and the wing root rib.  Passenger seat. Center section access panels.  Refer to Section 25-10. Refer to Section 52-40. 
Between the wing root rib and the bellcrank in the left/right wing.  Center section access panels. Aileron bellcrank access panels under each wing.  Refer to Section 52-40. 
Between the bellcrank in the left/right wing and the aileron.  Aileron bellcrank access panels under each wing.  Refer to Section 52-40. 

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AMM

5. Aileron Bellcrank and Lever Access
Aileron Bellcrank/Lever  Remove/Install Access  References 
Bellcrank at the control bulkhead.  Pilots’ seats.  Refer to Section 25-10. 
Idler lever at the front main bulkhead.  Pilots’ seats.  Refer to Section 25-10. 
Bellcrank at the rear main bulkhead.  Passenger seat.  Refer to Section 25-10. 
Bellcrank in the wing.  Aileron bellcrank access panels under each wing.  Refer to Section 52-40. 

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Flight Controls
AMM

Section 27-20
Flight Controls - Rudder

1. General
The DA 40 has the usual rudder control system. Each pilot has a rudder pedal assembly. The pilot can adjust the pedal position. Control cables connect the pedal assembly to the rudder. A fixed trim tab gives a small amount of adjustment to the rudder trim. You can only adjust the fixed trim tab on the ground.
Doc # 6.02.01 Page 1
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AMM
AIRCRAFT
Rudder Lower Mounting-Bracket
Turnbuckles
Teflon Tubes which
Guide Cockpit Cables

Pulley
Fuselage Cables with Guide Tubes
Yoke
Control Bulkhead
Co-Pilot's Rudder Pedal Assembly Outboard Control Cable Inboard Control Cable
Figure 1: Rudder Control System
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Flight Controls
AMM

2. Description
The DA 40 has a set of rudder control pedals for each pilot. The pedal assembly can be adjusted. Figures 1, 3, and 4 show you the rudder control system. Figure 2 shows you the rudder pedal assembly. The system has these parts:
) A rudder pedal assembly for each pilot at the front of the cockpit. The forward part of each pedal connects to a brake master cylinder (refer to Section 32-40).
) An adjuster handle for each pilot, attached to the aft face of the rudder pedal assembly.
) A yoke (a “T”-shaped lever) assembly in the fuselage below the center console. The yoke attaches to the bottom of the control bulkhead and to the fuselage shell.
) A rudder pedestal at the rear of the fuselage. The rudder lower mounting-bracket is attached to the rudder leading edge. It connects the rudder to the rudder pedestal.
　
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