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The aileron hinge axis is near the lower wing stem.
2. Description
Each aileron has these components:
A. Top Shell
The top shell has inner and outer GFRP skins. The skins bond to a rigid plastic foam core.
Carbon cloth gives extra strength and stiffness in the outer skin.
B. Bottom Shell
The bottom shell has inner and outer GFRP skins. The skins bond to a rigid plastic foam core.
Carbon cloth gives extra strength and stiffness in the outer skin.
C. End Ribs
The end ribs are rigid carbon moldings. They bond to the top and bottom shells. The outer end
rib has the mounting for the aileron mass-balance.
D. Aileron Horn
The aileron horn is aluminum alloy. Bolts and nuts attach the aileron horn to the bottom shell of
the aileron. The horn also makes the middle hinge for the aileron.
E. Aileron Hinges
Each aileron has 3 hinges (and the aileron horn). The aileron hinges are small blocks of
aluminum alloy. Bolts attach the aileron hinges to the aileron.
Wings
DA20-C1 AMM
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Figure 1: Aileron Structure
DA20-C1 AMM
Wings
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Rev. 1 57-60-00 Page 201
24 Mar 1999
MAINTENANCE PRACTICES
1. General
These maintenance practices tell you how to remove and install the ailerons. Refer to Chapter 27-
10 for data on adjusting the aileron controls.
2. Remove/Install A Aileron
A. Remove An Aileron
Detail Steps/Work Items Key Items
(1) Remove the bolt which attaches the control
rod to the aileron horn.
Hold the aileron.
(2) Remove the pivot bolts from the hinges and
the aileron horn.
Hold the aileron.
(3) Remove the aileron from the airplane.
B. Install An Aileron
Detail Steps/Work Items Key Items
(1) Put the aileron in position on the airplane. Hold the aileron.
(2) Install the pivot bolts in the hinges and the
aileron horn.
Hold the aileron.
Make sure that there is a gap of 3mm
(0.12 in) between the flap and the aileron
(3) Install the bolt which attaches the control rod
to the aileron horn.
(4) Do a test for correct adjustment of the
ailerons.
Refer to Chapter 27-10
(5) Do an inspection of the aileron controls
which you disconnected or adjusted.
(6) If necessary for your airworthiness authority,
do a second inspection of the aileron
controls.
Wings
DA20-C1 AMM
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19 Dec 1997 57-60-00 Doc # DA201-C1
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Figure 2: Aileron Connections
DA20-C1 AMM
Propeller
Doc # DA201-C1
Rev. 0 61-TITLE Page 1
19 Dec 1997
CHAPTER 61
PROPELLER
Propeller
DA20-C1 AMM
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Propeller
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Rev. 7 61-CONTENTS Page 1
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TABLE OF CONTENTS
CHAPTER 61-00 PROPELLER.............................................................................................................1
1.General ..............................................................................................................................1
CHAPTER 61-10 PROPELLER ASSEMBLY............................................................................................1
1.General ..............................................................................................................................1
2.Description .........................................................................................................................1
Trouble-Shooting........................................................................................................................101
1.General ..........................................................................................................................101
Maintenance Practices................................................................................................................201
1.General ..........................................................................................................................201
Remove/Install the Hoffmann HO-14HM-175-157 Propeller ............................................201
3.Remove/Install the Sensenich Propeller........................................................................204
Propeller
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Propeller
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CHAPTER 61-00
PROPELLER
1. General
This Chapter tells you about the propeller installed on the DA20-C1.
For data on the propeller refer to the manufacturer Owner’s Manual.
　
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