Each wing contains an integral fuel tank, aileron, flaps, de-ice boot, and main landing gear.
The fuel tanks are located between ribs 3 and 16, forward of the main spar to the nose rib and
between ribs 6 and 16 behind the main spar to the rear spar.
The ailerons are conventional construction with a single spar and ribs. The aileron access
panels are a carbon/nomex honeycomb construction. The ailerons are mass balanced and the
aileron/wing gap is sealed.
Each wing incorporates a single piece Fowler flap of conventional construction, with three
support arms and associated linkages. The wing trailing edges above the flaps are foam core
covered with carbon laminate while the flap fairings are a carbon laminate with nomex
honeycomb reinforcement strips.
A surface mounted de-ice boot is attached to the nose skin of each wing. Each wing has a
main landing gear attached to the front and rear spar, with a carbon fiber/nomex honeycomb
gear door attached to the leg. The wing tips are constructed of carbon fiber/honeycomb with a
top layer of copper foil for lightning protection.
Section 7 - Airplane and Systems Description
Wings
Pilot's Operating Handbook
Report No: 02406
Issue date: Mar 06, 2020
Page 7-2-2
12-C-A15-00-0702-00A-043A-A
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