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6 1 8.4525.60 Glass uni-directional ±45º, 265 mm x 100 mm
9 1 H 60 3 mm Rigid foam
11 1 8.4548.60 Glass twill 2/2 ±45º
% Figure 4: Layers of Cloth in the Rudder Shells
AIRCRAFT
Stabilizers
DA 40 Series
AMM
Page 204
20 Sep 2007 55-40-00 Doc # 6.02.01
Rev. 5
3. Repair Data for the Rudder Shells
% Figure 4 shows the layers of glass fiber cloth in the rudder shells. Use this data when you need to
repair the rudder.
The Figures show the main layers of cloth. The cross-hatching on the Figure shows the orientation of
the fibers. The orientation is also given in the related table. When you repair the rudder, you must use
the same type of cloth with the same fiber orientation.
The numbers in circles beside each drawing give the order in which the layers are applied (‘Stages’).
The first stage is a layer of filler and is not shown. Stage 1 is the outer face of the shell.
Always do a burn test on a piece of composite from the damaged area before you do a repair. Refer
to Section 51-20 for the burn test.
AIRCRAFT
DA 40 Series
AMM
Windows
Doc # 6.02.01
Rev. 5 56-TITLE Page 1
20 Sep 2007
CHAPTER 56
WINDOWS
AIRCRAFT
Windows DA 40 Series
AMM
Page 2
20 Sep 2007 56-TITLE Doc # 6.02.01
Rev. 5
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AIRCRAFT
DA 40 Series
AMM
Windows
Doc # 6.02.01
Rev. 5 56-CONTENTS Page 1
20 Sep 2007
TABLE OF CONTENTS
CHAPTER 56
WINDOWS
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
Section 56-10
Flight Compartment Windows
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
2. Description and Operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3
Maintenance Practices
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 201
2. Replace a Window . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 201
3. Window Repairs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 203
AIRCRAFT
Windows DA 40 Series
AMM
Page 2
20 Sep 2007 56-CONTENTS Doc # 6.02.01
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AIRCRAFT
DA 40 Series
AMM
Windows
Doc # 6.02.01
Rev. 5 56-00-00 Page 1
20 Sep 2007
CHAPTER 56
WINDOWS
1. General
The DA 40 has 3 windows. All of the windows are molded acrylic glass (plexiglass). The one-piece
canopy window covers the pilots’ cockpit. It is also the windscreen. The passenger door has a window.
The right side of the fuselage has a window for the passenger compartment.
A high-performance elastic adhesive bonds each window to the structure.
Section 56-10 gives the data for all of the windows. Refer to Section 52-10 for data about the canopy
and door structure.
AIRCRAFT
Windows DA 40 Series
AMM
Page 2
20 Sep 2007 56-00-00 Doc # 6.02.01
Rev. 5
Intentionally left blank
AIRCRAFT
DA 40 Series
AMM
Windows
Doc # 6.02.01
Rev. 5 56-10-00 Page 1
20 Sep 2007
Section 56-10
Flight Compartment Windows
1. General
This Section tells you about the windows in the canopy, passenger door and fuselage. Refer to Section
52-10 for data about the canopy and door structure.
AIRCRAFT
Windows DA 40 Series
AMM
Page 2
20 Sep 2007 56-10-00 Doc # 6.02.01
Rev. 5
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Figure 1: Windows
AIRCRAFT
DA 40 Series
AMM
Windows
Doc # 6.02.01
Rev. 5 56-10-00 Page 3
20 Sep 2007
2. Description and Operation
Figure 1 shows the windows.
A. General
The DA 40 has 3 windows. Each window is polycast molded acrylic glass (plexiglass). This material
gives good optical characteristics. It is also strong. It can be accurately formed into 3-dimensional
shapes. A high-performance elastic adhesive bonds each window to the structure. A flexible white
sealant fills the small gap between the edge of the window and the structure.
Each window has a band of white paint over the area where it bonds to the structure. The canopy
window also has a screened area above the pilots’ heads. This is a sun-shade. New windows are
　
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