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Nominal
Actual
Actual
(mm)
Actual
(mm)
Actual
(mm)
Nominal
(°)
Nominal
(°)
Nominal
(°)
Actual
(°)
Actual
(°)
Actual
(°)
Cruise
(UP)
Take-
Off
(T/O)
Landing
(LDG)
0° 0°
±1°
0
±4
81
±8
167
±4
167
±4
81
±8
0
±4
±1°
+20°
+42° +42°
+20°
±2°
±1° ±1°
±2°
Pre-
Load
3 - 5 kp
6.6 - 11 lbf
3 - 5 kp
6.6 - 11 lbf
233 233 200 200 200 200 200 200 477 477 240 240
AIRCRAFT
Dimensions and Areas
DA 40 Series
AMM
Page 10
20 Sep 2007 06-00-00 Doc # 6.02.01
Rev. 5
Adjustment Report
Wings
Leading Edge
Sweep Back
Dihedral (Wing
Supported)
Left Right Left Right Left Right Left Right
Nominal
Actual
Horizontal
Stabilizer
Angle of
Incidence
Rudder
Controls
Cable
Tension
Angle of
Incidence
(Wings supported with no load on the wing mounting bolts).
Wing Dihedral
±0.2°
1.0° 1.0°
±0.2°
5.0 °
±0.25° ±1° ±1°
5.0°
±0.25°
3.0°
+0.0° / -0.2°
15 daN (33.7 lb)
± 2 daN(± 4.5 lb)
Date
Registration
Main Landing Gear (at Empty
Weight, on Glide Sheets)
Camber Toe
1° to 1° to 0° 0° max.
4° 4° 1°
difference
% Figure 6: Adjustment Report, General Items
(valid for Lycoming and TAE versions)
AIRCRAFT
DA 40 Series
AMM
Dimensions and Areas
Doc # 6.02.01
Rev. 5 06-00-00 Page 11
20 Sep 2007
4. Weight and Static Moments of Control Surfaces
WARNING: IF YOU REPAINT (OR DO REPAIRS TO) THE CONTROL SURFACES,
YOU MUST MAKE SURE THAT THE WEIGHTS AND STATIC MOMENTS
OF THE CONTROL SURFACES ARE IN THE LIMITS IN THE CONTROL
SURFACE BALANCING REPORT. THIS WILL PREVENT CONTROL
SURFACE FLUTTER.
To measure the static moments you must remove the control surface from the airplane. Refer to
Section 51-60 for the measuring procedures.
If the values are not within the limits in the Control Surface Balancing Report, you must ask the
manufacturer for advice before you adjust the balancing weight.
AIRCRAFT
Dimensions and Areas
DA 40 Series
AMM
Page 12
20 Sep 2007 06-00-00 Doc # 6.02.01
Rev. 5
Intentionally left blank
AIRCRAFT
DA 40 Series
AMM
Lifting and Shoring
Doc # 6.02.01
Rev. 5 07-TITLE Page 1
20 Sep 2007
CHAPTER 07
LIFTING AND SHORING
AIRCRAFT
Lifting and Shoring DA 40 Series
AMM
Page 2
20 Sep 2007 07-TITLE Doc # 6.02.01
Rev. 5
Intentionally left blank
AIRCRAFT
DA 40 Series
AMM
Lifting and Shoring
Doc # 6.02.01
Rev. 5 07-CONTENTS Page 1
20 Sep 2007
TABLE OF CONTENTS
CHAPTER 07
LIFTING AND SHORING
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
Section 07-10
Jacking
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
2. Lifting the Airplane on Jacks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
AIRCRAFT
Lifting and Shoring DA 40 Series
AMM
Page 2
20 Sep 2007 07-CONTENTS Doc # 6.02.01
Rev. 5
Intentionally left blank
AIRCRAFT
DA 40 Series
AMM
Lifting and Shoring
Doc # 6.02.01
Rev. 5 07-00-00 Page 1
20 Sep 2007
CHAPTER 07
LIFTING AND SHORING
1. General
The DA 40 has no hoisting points. Use straps to lift the airplane.
You can use your hands to lift the wings and the horizontal stabilizer.
Section 07-10 tells you how to lift the airplane with jacks.
AIRCRAFT
Lifting and Shoring DA 40 Series
AMM
Page 2
20 Sep 2007 07-00-00 Doc # 6.02.01
Rev. 5
Intentionally left blank
AIRCRAFT
DA 40 Series
AMM
Lifting and Shoring
Doc # 6.02.01
Rev. 5 07-10-00 Page 1
20 Sep 2007
Section 07-10
Jacking
1. General
The DA 40 has 3 jacking points. There are main jacking points under each stub-wing. The tie-down
hole in the lower fin makes the tail jacking point. For maintenance lift the fuselage with the 3 hydraulic
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