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Wings
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CHAPTER 57
WINGS
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Wings
AMM
TABLE OF CONTENTS
CHAPTER 57
WINGS
1. General ..............................................1
Section 57-10
Wing Structure
1.
General ..............................................1
2.
Description............................................3
Maintenance Practices
1.
General ............................................201
2.
Remove/Install the Wings ..............................201
3.
Remove/Install the A or B-Bolts..........................212
4.
Remove/Install Control Surface Hinge Brackets..............215
5.
Repair Data for the Wing Shells..........................217
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Section 57-50
Flaps
1.
General ..............................................1
2.
Description............................................3
Maintenance Practices
1.
General ............................................201
2.
Remove/Install a Flap .................................201
3.
Repair Data for the Flap Shells...........................203
Section 57-60
Aileron
1.
General ..............................................1
2.
Description............................................3
Maintenance Practices
1.
General ............................................201
2.
Remove/Install an Aileron ..............................201
3.
Repair Data for the Aileron Shells ........................203
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Wings
AMM
CHAPTER 57
WINGS
1. General
The DA 40 has cantilever wings. The wings are set low on the fuselage. Each wing has a flap attached to the inboard trailing edge. An aileron attaches to the outboard trailing edge.
The wings have a monocoque structure. Each wing has top and bottom shells. The shells have CFRP outer skins, a rigid foam core and GFRP inner skins. Each wing has two I-section spars. Uni-directional carbon fiber cloth makes the spar caps. Each wing also has GFRP ribs and webs.
The flaps and ailerons have a mixture of CFRP and GFRP cloth in the shells. The shells have rigid foam cores.
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