AIRCRAFT
DA 42 NG AMM
Wings
Doc # 7.02.15
Rev. 4
57-00-00
Page 1
15 Mar 2018
CHAPTER 57
WINGS
1. General
The DA 42 NG is a low wing monoplane with cantilever wings. A wing center section with stub wings
and the engine nacelles attaches to the fuselage. Refer to Section 53-10 for more data about the
fuselage center section.
The outer wings attach to the wing center section stub wings. Each wing has a flap attached to the
inboard trailing edge of the outer wing and to the trailing edge of the stub wing. An aileron attaches
to the outboard trailing edge of each outer wing.
The wings have a semi-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.
Refer to Chapter 51 for general composite repair data. Refer to Chapter 27 for data about the control
systems which operate the flaps and ailerons.
Summary of Contents for DA 42 NG
Page 933: ...AIRCRAFT DA 42 NG AMM Fuel Doc 7 02 15 Rev 4 28 TITLE Page 1 15 Mar 2018 CHAPTER 28 FUEL ...
Page 1459: ...AIRCRAFT DA 42 NG AMM Lights Doc 7 02 15 Rev 4 33 TITLE Page 1 15 Mar 2018 CHAPTER 33 LIGHTS ...
Page 1711: ...AIRCRAFT DA 42 NG AMM Doors Doc 7 02 15 Rev 4 52 TITLE Page 1 15 Mar 2018 CHAPTER 52 DOORS ...
Page 1853: ...AIRCRAFT DA 42 NG AMM Wings Doc 7 02 15 Rev 4 57 TITLE Page 1 15 Mar 2018 CHAPTER 57 WINGS ...
Page 2071: ...AIRCRAFT DA 42 NG AMM Engine Doc 7 02 15 Rev 4 72 TITLE Page 1 15 Mar 2018 CHAPTER 72 ENGINE ...
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