DA20-C1 AMM
1.
General
The DA20-C1 aircraft has cantilever wings. The wings are set low on the fuselage. Each wing has a flap
inboard on the trailing edge. There is an aileron on the outboard trailing edge.
The wings are monocoque structure. Each wing has top and bottom shells. The shells have GFRP
skins and a rigid foam core. Each wing has an I-section spar. Carbon fiber rovings make the spar caps.
Each wing also has rigid GFRP ribs and webs.
Refer to Chapter 27 for data on the control systems for the flaps and ailerons. Refer to Chapter 51 for
general repair data.
DA201-C1
Rev 21
WINGS
57-00-00
Wings
Page 1
14 Jan 13
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