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Support the aileron assembly!
(3) Carefully move the aileron aft, and clear of the
airplane.
AIRCRAFT
Wings DA 40 Series
AMM
Page 202
20 Sep 2007 57-60-00 Doc # 6.02.01
Rev. 5
B. Install an Aileron
Detail Steps/Work Items Key Items/References
(1) Make sure that the hinge pins are clean and not
damaged.
(2) Put the aileron into position on the airplane.
(3) Install the 4 hinge pins in the hinges and aileron
horn:
S Push the hinge pins into position from the
inboard side.
S Align the holes in the hinges with the holes in
the hinge pins and install the roll pins.
Make sure that there is a gap of 0.5 -
2.5 mm (0.002 - 0.010 in) between the
faces of the hinge at the horn and a gap
of 1 - 3mm (0.004 - 0.012 in) between
the faces at the other hinges. hinges.
(4) Install the bolt which attaches the aileron push
rod to the aileron horn:
S Install a washer on the bolt.
S Push the bolt through the horn and the push
rod.
S Install the washer and the nut on the bolt.
(5) Do a test for correct adjustment of the aileron. Refer to Section 27-60.
(6) If necessary for your Airworthiness Authority, do
a second inspection of the aileron controls.
AIRCRAFT
DA 40 Series
AMM
Wings
Doc # 6.02.01
Rev. 5 57-60-00 Page 203
20 Sep 2007
3. Repair Data for the Aileron Shells
Figures 2 and 3 show the layers of glass/carbon fiber cloth in the aileron shells. Use this data when
you need to repair the aileron.
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 aileron, 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
Wings DA 40 Series
AMM
Page 204
20 Sep 2007 57-60-00 Doc # 6.02.01
Rev. 5
2 6
3 7
4 8
5
2 8
15
3 11 12 13 14
6
4 5
9 10
Item No. Layers Reference No. Type Remarks
2 2 8.4548.60 glass twill 2/2 ±45º
3 1 8.3520.8 carbon ±45º, 270 mm x 1220 mm.
4 1 8.4548.60 glass twill 2/2 ±45º, 270 mm x 520 mm.
5 3 8.3520.8 carbon ±45º, 80 mm x 270 mm.
6 1 H 60 3 mm rigid foam
8 1 8.3520.8 carbon ±45º, 90 mm x 1670 mm.
9 2 8.4548.60 glass twill 2/2 ±45º, 80 mm x 270 mm.
10 8 8.3520.8 carbon ±45º, 80 mm x 270 mm.
11 - 14 8 each 8.3520.8 carbon ±45º, 20 mm x 70 mm.
15 1 8.4548.60 glass twill 2/2 ±45º
Figure 2: Layers of Cloth in the Aileron Bottom Shell
AIRCRAFT
DA 40 Series
AMM
Wings
Doc # 6.02.01
Rev. 5 57-60-00 Page 205
20 Sep 2007
2
3 6
4 7
2 5 5
8
3
4
7
Item
No.
Layers Reference No. Type Remarks
2 2 8.4548.60 glass twill 2/2 ±45º
3 1 8.3520.8 carbon ±45º 300 mm x 1220 mm.
4 1 8.4548.60 glass twill 2/2 ±45º 300 mm x 480 mm.
5 1 H 60 3 mm rigid foam
7 2 8.3520.8 carbon ±45º 40 mm x 80 mm.
8 1 8.4548.60 glass twill 2/2 ±45º
Figure 3: Layers of Cloth in the Aileron Top Shell
AIRCRAFT
Wings DA 40 Series
AMM
Page 206
20 Sep 2007 57-60-00 Doc # 6.02.01
Rev. 5
Intentionally left blank
AIRCRAFT
DA 40 Series
AMM
Propeller
Doc # 6.02.01
Rev. 5 61-TITLE Page 1
20 Sep 2007
CHAPTER 61
PROPELLER
AIRCRAFT
Propeller
DA 40 Series
AMM
Page 2
20 Sep 2007 61-TITLE Doc # 6.02.01
Rev. 5
Intentionally left blank

　
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