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Dimensions and Areas
DA 40 Series
AMM
Page 2
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AIRCRAFT
DA 40 Series
AMM
Dimensions and Areas
Doc # 6.02.01
Rev. 5 06-CONTENTS Page 1
20 Sep 2007
TABLE OF CONTENTS
CHAPTER 06
DIMENSIONS AND AREAS
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
% 2. Dimensions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2
% 3. Adjustment Values . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5
% 4. Weight and Static Moments of Control Surfaces . . . . . . . . . . . . . . 11
AIRCRAFT
Dimensions and Areas
DA 40 Series
AMM
Page 2
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AIRCRAFT
DA 40 Series
AMM
Dimensions and Areas
Doc # 6.02.01
Rev. 5 06-00-00 Page 1
20 Sep 2007
CHAPTER 06
DIMENSIONS AND AREAS
1. General
The DA 40 uses the System Internationale (SI) for dimensions and areas. Imperial dimensions are also
given in brackets. For example: Wing span 11.94 m (39.2 ft).
Conversions between SI units and imperial units are given in Chapter 02.
AIRCRAFT
Dimensions and Areas
DA 40 Series
AMM
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20 Sep 2007 06-00-00 Doc # 6.02.01
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2.97 m (9.7 ft)
11.94 m (39.2 ft)
8.01 m (26.3 ft)
1.97 m (6.5 ft)
3.29 m (10.8 ft)
Propeller (∅ 1.8 m (70.9 in))
Ground Line, Static
% 2. Dimensions
Figure 1: DA 40 with Lycoming Engine, Overall Dimensions (Approximate Values)
AIRCRAFT
DA 40 Series
AMM
Dimensions and Areas
Doc # 6.02.01
Rev. 5 06-00-00 Page 3
20 Sep 2007
2.97 m (9.7 ft)
11.94 m (39.2 ft)
8.06 m (26.4 ft)
1.97 m (6.5 ft)
3.29 m (10.8 ft)
Propeller (∅ 1.87 m (73.6 in))
Ground Line, Static
% Figure 2: DA 40 D with TAE Engine, Overall Dimensions (Approximate Values)
AIRCRAFT
Dimensions and Areas
DA 40 Series
AMM
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20 Sep 2007 06-00-00 Doc # 6.02.01
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DA 40
Overall Dimensions
Wing span 11.94 m (39.2 ft)
% Length Lycoming version 8.01 m (26.3 ft)
TAE version 8.06 m (26.4 ft)
Height (Nominal) 1.97 m (6.5 ft)
Wing
Airfoil Wortmann FX 63-137/20-W4
Wing area 13.54 m² (145.7 ft²)
Dihedral (Nominal) 5°
Angle of incidence (Nominal) 3º
Horizontal Tail Surfaces
Span 3.29 m (10.8 ft)
Angle of incidence -3.0º
Landing gear (Typical static, normal load)
Wheel Track 2.97 m (9.74 ft)
Wheel base 1.68 m (5.51 ft)
Nose wheel 5.00-5; 6 PR, 120 mph
% Main wheel (a) 6.00-6; 6PR, 120 mph
% Only in combination with the standard
% MLG strut or the “thin” MLG strut
% (MÄM 40-123/e)
% (b) 15x6.0-6; 6PR, 120 mph (OÄM 40-124)
% only in combination with the “thin”
% (MÄM 40-123/e) or the “tall”
% (OÄM 40-283) MLG strut
AIRCRAFT
DA 40 Series
AMM
Dimensions and Areas
Doc # 6.02.01
Rev. 5 06-00-00 Page 5
20 Sep 2007
3. Adjustment Values
The measurements of the DA 40 are recorded on an Adjustment Report at the factory when the
% airplane is built. See Figures 4 and 5 (depends on DA 40 version) and 6. This Report becomes part
of the airplane records.
When you measure the dimensions, use the Adjustment Report as a reference for deviations.
Control Surface Deflections and Adjustment Reports:
% DA 40 with Lycoming IO 360 M1A
% Control Surface Deflections Adjustment Report
% Standard Version see figure 3 see figure 4
% OÄM 40-071 (Longe Range Tank)
% incorporated
see figure 3 see figure 5
% MÄM 40-113 (LRT Rudder for
% Standard Version) incorporated
see figure 3 see figure 5
% DA 40 D with TAE 125
% Control Surface Deflections Adjustment Report
% Standard Version (OÄM 40-100) see figure 3 see figure 4
% OÄM 40-130 (Longe Range Tank)
% incorporated
see figure 3 see figure 5
% MÄM 40-113 (LRT Rudder for
% Standard Version) incorporated
see figure 3 see figure5
AIRCRAFT
Dimensions and Areas
DA 40 Series
AMM
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