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AIRCRAFT
Fuselage
DA 40 Series
AMM
Page 204
20 Sep 2007 53-10-00 Doc # 6.02.01
Rev. 5
16 14
15
17
14 16
19
LEFT FUSELAGE SHELL
20 21 22
25 24 23
LEFT FUSELAGE SHELL
RIGHT FUSELAGE SHELL
22 21 20
23 24 25
RIGHT FUSELAGE SHELL
9
10
Item No. Layers Reference No. Type Remarks
14 3 KDU 1034 Carbon 100 mm uni-directional 1000 mm
15 3 KDU 1034 Carbon 100 mm uni-directional 1400 mm
16 3 KDU 1034 Carbon 100 mm uni-directional 850 mm
17 3 KDU 1034 Carbon 100 mm uni-directional 1200 mm
19 3 KDU 1034 Carbon 100 mm uni-directional 1200 mm
20-22 1 each KDU 1034 Carbon 100 mm uni-directional 600 mm, 700 mm, 800 mm
23-25 1 each KDU 1034 Carbon 100 mm uni-directional 600 mm, 700 mm, 800 mm
Figure 7: Layers of Cloth in the Fuselage Shells - Stages 9 & 10
AIRCRAFT
DA 40 Series
AMM
Fuselage
Doc # 6.02.01
Rev. 5 53-10-00 Page 205
20 Sep 2007
27
34
32 31 30 29
28
34
36
35
42
37 38 39 40
VIEW FROM BELOW
LEFT FUSELAGE SHELL
VIEW FROM ABOVE
RIGHT FUSELAGE SHELL
11
Item No. Reference No. Type Remarks
27-32 H 60 8 mm Rigid foam
34-36 H 60 3 mm Rigid foam
37-42 H 60 8 mm Rigid foam
Figure 8: Rigid Foam Inserts in the Fuselage Shells - Stage 11
AIRCRAFT
Fuselage
DA 40 Series
AMM
Page 206
20 Sep 2007 53-10-00 Doc # 6.02.01
Rev. 5
43
44, 45
44, 45
12
13
Item
No.
Layers Reference No. Type Remarks
43 2 8.4551.60 Glass 92125 twill 2/2 ±45º
44 2 8.4554.60 Glass 92140 twill 2/2 ±45º
45 1 8.4554.60 Glass 92140 twill 2/2 0º/90º
Figure 9: Layers of Cloth in the Fuselage Shells - Stages 12 & 13
AIRCRAFT
DA 40 Series
AMM
Fuselage
Doc # 6.02.01
Rev. 5 53-10-00 Page 207
20 Sep 2007
2 3
4
5 6
8 9
2 3
5
4
6 7
7
Item
No.
Layers Reference No. Type Remarks
2 1 8.4548.60 Glass 92110 twill 2/2 0º/90º
3 1 8.4551.60 Glass 92125 twill 2/2 ±45º
4 2 8.4551.60 Glass 92125 twill 2/2 0º/90º
5 3 8.4525.60 Glass 92146 uni-directional 0º, 900 mm
6 2 8.4551.60 Glass 92125 twill 2/2 200 mm * 200 mm
7 & 8 H 60 8 mm Rigid foam
9 3 8.4548.60 Glass 92110 twill 2/2 ±45º
Figure 10: Layers of Cloth in the Center Section Bottom Shell
AIRCRAFT
Fuselage
DA 40 Series
AMM
Page 208
20 Sep 2007 53-10-00 Doc # 6.02.01
Rev. 5
2 3
5
4
6 7
2 3 4
5
6
8 7
10 9
11
Item
No.
Layers Reference No. Type Remarks
2 1 8.4548.60 Glass 92110 twill 2/2 0º/90º
3 2 8.4551.60 Glass 92125 twill 2/2 0º/90º
4 2 8.4551.60 Glass 92125 twill 2/2 ±45º
5 3 8.4525.60 Glass 92146 uni-directional 0º
6 - 10 H 60 8 mm rigid foam
11 2 8.4551.60 Glass 92125 twill 2/2 0º/90º
Figure 11: Layers of Cloth in the Center Section Top Shells
AIRCRAFT
DA 40 Series
AMM
Stabilizers
Doc # 6.02.01
Rev. 5 55-TITLE Page 1
20 Sep 2007
CHAPTER 55
STABILIZERS
AIRCRAFT
Stabilizers
DA 40 Series
AMM
Page 2
20 Sep 2007 55-TITLE Doc # 6.02.01
Rev. 5
Intentionally left blank
AIRCRAFT
DA 40 Series
AMM
Stabilizers
Doc # 6.02.01
Rev. 5 55-CONTENTS Page 1
20 Sep 2007
TABLE OF CONTENTS
CHAPTER 55
STABILIZERS
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
Section 55-10
Horizontal Stabilizer
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
2. Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
Maintenance Practices
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 201
2. Remove/Install the Horizontal Stabilizer . . . . . . . . . . . . . . . . . . . . 201
3. Repair Data for the Horizontal Stabilizer Shells . . . . . . . . . . . . . . 205
Section 55-20
Elevator
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
2. Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3
Maintenance Practices
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 201
　
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