Wing Dihedral
(Wings supported with no load on the wing mounting bolts).
% Figure 7: Adjustment Report, General Items % (valid for Lycoming and TAE versions)
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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 3 and 4. This Report becomes part of the airplane records.
When you measure the dimensions, use the Adjustment Report as a reference for deviations.
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.
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CHAPTER 07
LIFTING AND SHORING
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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
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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.
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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 jacks. Use a trestle with a special former to hold the front of the fuselage. Use standard trestles under the wings at the position where the tips connect to the wing. Refer to Figure 1.
WARNING: IF THE WIND SPEED IS MORE THAN 10 KM/H (6 KNOTS), DO NOT LIFT THE AIRPLANE ON JACKS IN THE OPEN.
2. Lifting the Airplane on Jacks
A. Equipment
Item Quantity Part Number
Airplane jacks (600 kg / 1320 lb minimum lifting capacity). 3 Commercial
Nose trestle. 1 Commercial
Wing trestles. 2 Commercial
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