AIRCRAFT
DV 20 E AMM
Flight Controls
Doc # 4.02.25
Rev. 2
27-00-00
Page 1
15 Mar 2022
CHAPTER 27
FLIGHT CONTROLS
1. General
This chapter describes about the operation and the adjustment of the flight controls. It also describes
about the assembly of the flight controls. Refer to the related section for the data on a specified
system.
This chapter describes how standard parts are used to make the flight controls for each system.
2. Description
The DV 20 E airplane has the usual flight controls. An elevator attached to the horizontal stabilizer
gives longitudinal control. Ailerons attached to the trailing edge of each wing give lateral control. The
rudder attached to the Vertical Stabilizer gives yaw control. Flaps attached to the trailing edge of each
wing give extra lift for landing and for take-off.
The DV 20 E airplane has a control stick for each pilot. The pilot can set the elevator trim with a control
switch in the control stick.
Each pilot has a rudder pedal assembly. The assembly attaches to the cockpit floor. The pilot can
adjust the position of the rudder pedals with a T-grip selector on the rudder pedal assembly.
The pilot moves each primary control through a system of control rods and bellcranks. Cables operate
the rudder. An electric actuator operates the flaps.
3. Control Rods
The control rods used in the DV 20 E airplane have standard end fittings. Also most rods use a
standard diameter tube. Only the length of the rods is special.
Figure 1 shows an example of a standard control rod. The rod has adjustable end fittings. Each end
fitting has an eye end with a threaded shaft. The eye end has a bearing. A lock nut on the threaded
shaft locks the eye end in position. You can turn the eye end to adjust the length of the rod.
A steel tube connects the end fittings. Threaded inserts are welded into position in the end of each
steel tube. A safety hole is drilled in each end of the steel tube. The safety hole shows you if the
installation of the eye end to the insert in the steel tube is correct. If you can push the safety wire
through the hole to the other side, the eye end installation is not correct. If you cannot push the safety
wire through the hole, the eye end installation is correct.
Summary of Contents for DV 20 E 2022
Page 50: ...AIRCRAFT Airworthiness Limitations DV 20 E AMM Page 4 15 Mar 2022 04 00 00 Doc 4 02 25 Rev 2...
Page 405: ...AIRCRAFT DV 20 E AMM Fuel Doc 4 02 25 Rev 2 28 TITLE Page 1 15 Mar 2022 CHAPTER 28 FUEL...
Page 561: ...AIRCRAFT DV 20 E AMM Lights Doc 4 02 25 Rev 2 33 TITLE Page 1 15 Mar 2022 CHAPTER 33 LIGHTS...
Page 679: ...AIRCRAFT DV 20 E AMM Doors Doc 4 02 25 Rev 2 52 TITLE Page 1 15 Mar 2022 CHAPTER 52 DOORS...
Page 686: ...AIRCRAFT Doors DV 20 E AMM Page 2 15 Mar 2022 52 10 00 Doc 4 02 25 Rev 2 Figure 1 Canopy...
Page 741: ...AIRCRAFT DV 20 E AMM Windows Doc 4 02 25 Rev 2 56 TITLE Page 1 15 Mar 2022 CHAPTER 56 WINDOWS...
Page 757: ...AIRCRAFT DV 20 E AMM Wings Doc 4 02 25 Rev 2 57 TITLE Page 1 15 Mar 2022 CHAPTER 57 WINGS...
Page 857: ...AIRCRAFT DV 20 E AMM Exhaust Doc 4 02 25 Rev 2 78 TITLE Page 1 15 Mar 2022 CHAPTER 78 EXHAUST...
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